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PUGET SOUND, Wash. (April 2, 2018) The Blue crew of the Ohio-class ballistic missile submarine USS Nebraska (SSBN 739) transits the Hood Canal as it returns to its homeport following a test launch of two unarmed Trident II D5 missiles off the coast of California. The test launch was part of the U.S. Navy Strategic Systems Program’s demonstration and shakedown operation certification process. The successful launch certified the readiness of an SSBN crew and the operational performance of the submarine’s strategic weapons system before returning to operational availability. Nebraska is one of eight ballistic missile submarines stationed at Naval Base Kitsap-Bangor providing the most survivable leg of the strategic deterrence triad for the United States. (U.S. Navy photo by Lt. Cmdr. Michael L. Smith)

This visualization shows the extent of Arctic sea ice on Aug. 26, 2012, the day the sea ice dipped to its smallest extent ever recorded in more than three decades of satellite measurements, according to scientists from NASA and the National Snow and Ice Data Center. The data is from the U.S. Defense Meteorological Satellite Program’s Special Sensor Microwave/Imager. The line on the image shows the average minimum extent from the period covering 1979-2010, as measured by satellites. Every summer the Arctic ice cap melts down to what scientists call its “minimum” before colder weather builds the ice cover back up. The size of this minimum remains in a long-term decline. The extent on Aug. 26. 2012 broke the previous record set on Sept. 18, 2007. But the 2012 melt season could still continue for several weeks.

 

To read more go to: 1.usa.gov/PkgRuq

 

Image credit: Scientific Visualization Studio, NASA Goddard Space Flight Center

 

NASA and the National Snow and Ice Data Center (NSIDC) announced on Aug. 27, 2012, that the ice cap covering the Arctic Ocean is now smaller than ever recorded since consistent satellite measurements of the ice began more than three decades ago. Each year, the ice cap goes through a shrink-and-swell cycle, melting throughout the summer months before expanding through fall and winter. In the past decade in particular the minimum summertime extent of the ice cap has shown a consistent decline in size – a trend closely linked with the Arctic's warming climate. NASA and NSIDC scientists said the extent of Arctic sea ice on Aug. 26 surpassed the previous record minimum extent set in the summer of 2007. The ice cap will continue to melt and get smaller in the coming weeks before temperatures get colder and ice begins to refreeze as fall approaches.

 

NASA and the National Snow and Ice Data Center (NSIDC) announced on Aug. 27, 2012, that the ice cap covering the Arctic Ocean is now smaller than ever recorded since consistent satellite measurements of the ice began more than three decades ago. Each year, the ice cap goes through a shrink-and-swell cycle, melting throughout the summer months before expanding through fall and winter. In the past decade in particular the minimum summertime extent of the ice cap has shown a consistent decline in size – a trend closely linked with the Arctic's warming climate. NASA and NSIDC scientists said the extent of Arctic sea ice on Aug. 26 surpassed the previous record minimum extent set in the summer of 2007. The ice cap will continue to melt and get smaller in the coming weeks before temperatures get colder and ice begins to refreeze as fall approaches.

 

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NASA Goddard Space Flight Center enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission.

 

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+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The OV-10 Bronco was initially conceived in the early 1960s through an informal collaboration between W. H. Beckett and Colonel K. P. Rice, U.S. Marine Corps, who met at Naval Air Weapons Station China Lake, California, and who also happened to live near each other. The original concept was for a rugged, simple, close air support aircraft integrated with forward ground operations. At the time, the U.S. Army was still experimenting with armed helicopters, and the U.S. Air Force was not interested in close air support.

The concept aircraft was to operate from expedient forward air bases using roads as runways. Speed was to be from very slow to medium subsonic, with much longer loiter times than a pure jet. Efficient turboprop engines would give better performance than piston engines. Weapons were to be mounted on the centerline to get efficient aiming. The inventors favored strafing weapons such as self-loading recoilless rifles, which could deliver aimed explosive shells with less recoil than cannons, and a lower per-round weight than rockets. The airframe was to be designed to avoid the back blast.

 

Beckett and Rice developed a basic platform meeting these requirements, then attempted to build a fiberglass prototype in a garage. The effort produced enthusiastic supporters and an informal pamphlet describing the concept. W. H. Beckett, who had retired from the Marine Corps, went to work at North American Aviation to sell the aircraft.

The aircraft's design supported effective operations from forward bases. The OV-10 had a central nacelle containing a crew of two in tandem and space for cargo, and twin booms containing twin turboprop engines. The visually distinctive feature of the aircraft is the combination of the twin booms, with the horizontal stabilizer that connected them at the fin tips. The OV-10 could perform short takeoffs and landings, including on aircraft carriers and large-deck amphibious assault ships without using catapults or arresting wires. Further, the OV-10 was designed to take off and land on unimproved sites. Repairs could be made with ordinary tools. No ground equipment was required to start the engines. And, if necessary, the engines would operate on high-octane automobile fuel with only a slight loss of power.

 

The aircraft had responsive handling and could fly for up to 5½ hours with external fuel tanks. The cockpit had extremely good visibility for both pilot and co-pilot, provided by a wrap-around "greenhouse" that was wider than the fuselage. North American Rockwell custom ejection seats were standard, with many successful ejections during service. With the second seat removed, the OV-10 could carry 3,200 pounds (1,500 kg) of cargo, five paratroopers, or two litter patients and an attendant. Empty weight was 6,969 pounds (3,161 kg). Normal operating fueled weight with two crew was 9,908 pounds (4,494 kg). Maximum takeoff weight was 14,446 pounds (6,553 kg).

The bottom of the fuselage bore sponsons or "stub wings" that improved flight performance by decreasing aerodynamic drag underneath the fuselage. Normally, four 7.62 mm (.308 in) M60C machine guns were carried on the sponsons, accessed through large forward-opening hatches. The sponsons also had four racks to carry bombs, pods, or fuel. The wings outboard of the engines contained two additional hardpoints, one per side. Racked armament in the Vietnam War was usually seven-shot 2.75 in (70 mm) rocket pods with white phosphorus marker rounds or high-explosive rockets, or 5" (127 mm) four-shot Zuni rocket pods. Bombs, ADSIDS air-delivered/para-dropped unattended seismic sensors, Mk-6 battlefield illumination flares, and other stores were also carried.

Operational experience showed some weaknesses in the OV-10's design. It was significantly underpowered, which contributed to crashes in Vietnam in sloping terrain because the pilots could not climb fast enough. While specifications stated that the aircraft could reach 26,000 feet (7,900 m), in Vietnam the aircraft could reach only 18,000 feet (5,500 m). Also, no OV-10 pilot survived ditching the aircraft.

 

The OV-10 served in the U.S. Air Force, U.S. Marine Corps, and U.S. Navy, as well as in the service of a number of other countries. In U.S. military service, the Bronco was operated until the early Nineties, and obsoleted USAF OV-10s were passed on to the Bureau of Alcohol, Tobacco, and Firearms for anti-drug operations. A number of OV-10As furthermore ended up in the hands of the California Department of Forestry (CDF) and were used for spotting fires and directing fire bombers onto hot spots.

 

This was not the end of the OV-10 in American military service, though: In 2012, the type gained new attention because of its unique qualities. A $20 million budget was allocated to activate an experimental USAF unit of two airworthy OV-10Gs, acquired from NASA and the State Department. These machines were retrofitted with military equipment and were, starting in May 2015, deployed overseas to support Operation “Inherent Resolve”, flying more than 120 combat sorties over 82 days over Iraq and Syria. Their concrete missions remained unclear, and it is speculated they provided close air support for Special Forces missions, esp. in confined urban environments where the Broncos’ loitering time and high agility at low speed and altitude made them highly effective and less vulnerable than helicopters.

Furthermore, these Broncos reputedly performed strikes with the experimental AGR-20A “Advanced Precision Kill Weapons System (APKWS)”, a Hydra 70-millimeter rocket with a laser-seeking head as guidance - developed for precision strikes against small urban targets with little collateral damage. The experiment ended satisfactorily, but the machines were retired again, and the small unit was dissolved.

 

However, the machines had shown their worth in asymmetric warfare, and the U.S. Air Force decided to invest in reactivating the OV-10 on a regular basis, despite the overhead cost of operating an additional aircraft type in relatively small numbers – but development and production of a similar new type would have caused much higher costs, with an uncertain time until an operational aircraft would be ready for service. Re-activating a proven design and updating an existing airframe appeared more efficient.

The result became the MV-10H, suitably christened “Super Bronco” but also known as “Black Pony”, after the program's internal name. This aircraft was derived from the official OV-10X proposal by Boeing from 2009 for the USAF's Light Attack/Armed Reconnaissance requirement. Initially, Boeing proposed to re-start OV-10 manufacture, but this was deemed uneconomical, due to the expected small production number of new serial aircraft, so the “Black Pony” program became a modernization project. In consequence, all airframes for the "new" MV-10Hs were recovered OV-10s of various types from the "boneyard" at Davis-Monthan Air Force Base in Arizona.

 

While the revamped aircraft would maintain much of its 1960s-vintage rugged external design, modernizations included a completely new, armored central fuselage with a highly modified cockpit section, ejection seats and a computerized glass cockpit. The “Black Pony” OV-10 had full dual controls, so that either crewmen could steer the aircraft while the other operated sensors and/or weapons. This feature would also improve survivability in case of incapacitation of a crew member as the result from a hit.

The cockpit armor protected the crew and many vital systems from 23mm shells and shrapnel (e. g. from MANPADS). The crew still sat in tandem under a common, generously glazed canopy with flat, bulletproof panels for reduced sun reflections, with the pilot in the front seat and an observer/WSO behind. The Bronco’s original cargo capacity and the rear door were retained, even though the extra armor and defensive measures like chaff/flare dispensers as well as an additional fuel cell in the central fuselage limited the capacity. However, it was still possible to carry and deploy personnel, e. g. small special ops teams of up to four when the aircraft flew in clean configuration.

Additional updates for the MV-10H included structural reinforcements for a higher AUW and higher g load maneuvers, similar to OV-10D+ standards. The landing gear was also reinforced, and the aircraft kept its ability to operate from short, improvised airstrips. A fixed refueling probe was added to improve range and loiter time.

 

Intelligence sensors and smart weapon capabilities included a FLIR sensor and a laser range finder/target designator, both mounted in a small turret on the aircraft’s nose. The MV-10H was also outfitted with a data link and the ability to carry an integrated targeting pod such as the Northrop Grumman LITENING or the Lockheed Martin Sniper Advanced Targeting Pod (ATP). Also included was the Remotely Operated Video Enhanced Receiver (ROVER) to provide live sensor data and video recordings to personnel on the ground.

 

To improve overall performance and to better cope with the higher empty weight of the modified aircraft as well as with operations under hot-and-high conditions, the engines were beefed up. The new General Electric CT7-9D turboprop engines improved the Bronco's performance considerably: top speed increased by 100 mph (160 km/h), the climb rate was tripled (a weak point of early OV-10s despite the type’s good STOL capability) and both take-off as well as landing run were almost halved. The new engines called for longer nacelles, and their circular diameter markedly differed from the former Garrett T76-G-420/421 turboprop engines. To better exploit the additional power and reduce the aircraft’s audio signature, reversible contraprops, each with eight fiberglass blades, were fitted. These allowed a reduced number of revolutions per minute, resulting in less noise from the blades and their tips, while the engine responsiveness was greatly improved. The CT7-9Ds’ exhausts were fitted with muzzlers/air mixers to further reduce the aircraft's noise and heat signature.

Another novel and striking feature was the addition of so-called “tip sails” to the wings: each wingtip was elongated with a small, cigar-shaped fairing, each carrying three staggered, small “feather blade” winglets. Reputedly, this installation contributed ~10% to the higher climb rate and improved lift/drag ratio by ~6%, improving range and loiter time, too.

Drawing from the Iraq experience as well as from the USMC’s NOGS test program with a converted OV-10D as a night/all-weather gunship/reconnaissance platform, the MV-10H received a heavier gun armament: the original four light machine guns that were only good for strafing unarmored targets were deleted and their space in the sponsons replaced by avionics. Instead, the aircraft was outfitted with a lightweight M197 three-barrel 20mm gatling gun in a chin turret. This could be fixed in a forward position at high speed or when carrying forward-firing ordnance under the stub wings, or it could be deployed to cover a wide field of fire under the aircraft when it was flying slower, being either slaved to the FLIR or to a helmet sighting auto targeting system.

The original seven hardpoints were retained (1x ventral, 2x under each sponson, and another pair under the outer wings), but the total ordnance load was slightly increased and an additional pair of launch rails for AIM-9 Sidewinders or other light AAMs under the wing tips were added – not only as a defensive measure, but also with an anti-helicopter role in mind; four more Sidewinders could be carried on twin launchers under the outer wings against aerial targets. Other guided weapons cleared for the MV-10H were the light laser-guided AGR-20A and AGM-119 Hellfire missiles, the Advanced Precision Kill Weapon System upgrade to the light Hydra 70 rockets, the new Laser Guided Zuni Rocket which had been cleared for service in 2010, TV-/IR-/laser-guided AGM-65 Maverick AGMs and AGM-122 Sidearm anti-radar missiles, plus a wide range of gun and missile pods, iron and cluster bombs, as well as ECM and flare/chaff pods, which were not only carried defensively, but also in order to disrupt enemy ground communication.

 

In this configuration, a contract for the conversion of twelve mothballed American Broncos to the new MV-10H standard was signed with Boeing in 2016, and the first MV-10H was handed over to the USAF in early 2018, with further deliveries lasting into early 2020. All machines were allocated to the newly founded 919th Special Operations Support Squadron at Duke Field (Florida). This unit was part of the 919th Special Operations Wing, an Air Reserve Component (ARC) of the United States Air Force. It was assigned to the Tenth Air Force of Air Force Reserve Command and an associate unit of the 1st Special Operations Wing, Air Force Special Operations Command (AFSOC). If mobilized the wing was gained by AFSOC (Air Force Special Operations Command) to support Special Tactics, the U.S. Air Force's special operations ground force. Similar in ability and employment to Marine Special Operations Command (MARSOC), U.S. Army Special Forces and U.S. Navy SEALs, Air Force Special Tactics personnel were typically the first to enter combat and often found themselves deep behind enemy lines in demanding, austere conditions, usually with little or no support.

 

The MV-10Hs are expected to provide support for these ground units in the form of all-weather reconnaissance and observation, close air support and also forward air control duties for supporting ground units. Precision ground strikes and protection from enemy helicopters and low-flying aircraft were other, secondary missions for the modernized Broncos, which are expected to serve well into the 2040s. Exports or conversions of foreign OV-10s to the Black Pony standard are not planned, though.

  

General characteristics:

Crew: 2

Length: 42 ft 2½ in (12,88 m) incl. pitot

Wingspan: 45 ft 10½ in(14 m) incl. tip sails

Height: 15 ft 2 in (4.62 m)

Wing area: 290.95 sq ft (27.03 m²)

Airfoil: NACA 64A315

Empty weight: 9,090 lb (4,127 kg)

Gross weight: 13,068 lb (5,931 kg)

Max. takeoff weight: 17,318 lb (7,862 kg)

 

Powerplant:

2× General Electric CT7-9D turboprop engines, 1,305 kW (1,750 hp) each,

driving 8-bladed Hamilton Standard 8 ft 6 in (2.59 m) diameter constant-speed,

fully feathering, reversible contra-rotating propellers with metal hub and composite blades

 

Performance:

Maximum speed: 390 mph (340 kn, 625 km/h)

Combat range: 198 nmi (228 mi, 367 km)

Ferry range: 1,200 nmi (1,400 mi, 2,200 km) with auxiliary fuel

Maximum loiter time: 5.5 h with auxiliary fuel

Service ceiling: 32.750 ft (10,000 m)

13,500 ft (4.210 m) on one engine

Rate of climb: 17.400 ft/min (48 m/s) at sea level

Take-off run: 480 ft (150 m)

740 ft (227 m) to 50 ft (15 m)

1,870 ft (570 m) to 50 ft (15 m) at MTOW

Landing run: 490 ft (150 m)

785 ft (240 m) at MTOW

1,015 ft (310 m) from 50 ft (15 m)

 

Armament:

1x M197 3-barreled 20 mm Gatling cannon in a chin turret with 750 rounds ammo capacity

7x hardpoints for a total load of 5.000 lb (2,270 kg)

2x wingtip launch rails for AIM-9 Sidewinder AAMs

  

The kit and its assembly:

This fictional Bronco update/conversion was simply spawned by the idea: could it be possible to replace the original cockpit section with one from an AH-1 Cobra, for a kind of gunship version?

 

The basis is the Academy OV-10D kit, mated with the cockpit section from a Fujimi AH-1S TOW Cobra (Revell re-boxing, though), chosen because of its “boxy” cockpit section with flat glass panels – I think that it conveys the idea of an armored cockpit section best. Combining these parts was not easy, though, even though the plan sound simple. Initially, the Bronco’s twin booms, wings and stabilizer were built separately, because this made PSR on these sections easier than trying the same on a completed airframe. One of the initial challenges: the different engines. I wanted something uprated, and a different look, and I had a pair of (excellent!) 1:144 resin engines from the Russian company Kompakt Zip for a Tu-95 bomber at hand, which come together with movable(!) eight-blade contraprops that were an almost perfect size match for the original three-blade props. Biggest problem: the Tu-95 nacelles have a perfectly circular diameter, while the OV-10’s booms are square and rectangular. Combining these parts and shapes was already a messy PST affair, but it worked out quite well – even though the result rather reminds of some Chinese upgrade measure (anyone know the Tu-4 copies with turboprops? This here looks similar!). But while not pretty, I think that the beafier look works well and adds to the idea of a “revived” aircraft. And you can hardly beat the menacing look of contraprops on anything...

The exotic, so-called “tip sails” on the wings, mounted on short booms, are a detail borrowed from the Shijiazhuang Y-5B-100, an updated Chinese variant/copy of the Antonov An-2 biplane transporter. The booms are simple pieces of sprue from the Bronco kit, the winglets were cut from 0.5mm styrene sheet.

 

For the cockpit donor, the AH-1’s front section was roughly built, including the engine section (which is a separate module, so that the basic kit can be sold with different engine sections), and then the helicopter hull was cut and trimmed down to match the original Bronco pod and to fit under the wing. This became more complicated than expected, because a) the AH-1 cockpit and the nose are considerably shorter than the OV-10s, b) the AH-1 fuselage is markedly taller than the Bronco’s and c) the engine section, which would end up in the area of the wing, features major recesses, making the surface very uneven – calling for massive PSR to even this out. PSR was also necessary to hide the openings for the Fujimi AH-1’s stub wings. Other issues: the front landing gear (and its well) had to be added, as well as the OV-10 wing stubs. Furthermore, the new cockpit pod’s rear section needed an aerodynamical end/fairing, but I found a leftover Academy OV-10 section from a build/kitbashing many moons ago. Perfect match!

All these challenges could be tackled, even though the AH-1 cockpit looks surprisingly stout and massive on the Bronco’s airframe - the result looks stockier than expected, but it works well for the "Gunship" theme. Lots of PSR went into the new central fuselage section, though, even before it was mated with the OV-10 wing and the rest of the model.

Once cockpit and wing were finally mated, the seams had to disappear under even more PSR and a spinal extension of the canopy had to be sculpted across the upper wing surface, which would meld with the pod’s tail in a (more or less) harmonious shape. Not an easy task, and the fairing was eventually sculpted with 2C putty, plus even more PSR… Looks quite homogenous, though.

 

After this massive body work, other hardware challenges appeared like small distractions. The landing gear was another major issue because the deeper AH-1 section lowered the ground clearance, also because of the chin turret. To counter this, I raised the OV-10’s main landing gear by ~2mm – not much, but it was enough to create a credible stance, together with the front landing gear transplant under the cockpit, which received an internal console to match the main landing gear’s length. Due to the chin turret and the shorter nose, the front wheel retracts backwards now. But this looks quite plausible, thanks to the additional space under the cockpit tub, which also made a belt feed for the gun’s ammunition supply believable.

To enhance the menacing look I gave the model a fixed refueling boom, made from 1mm steel wire and a receptor adapter sculpted with white glue. The latter stuff was also used add some antenna fairings around the hull. Some antennae, chaff dispensers and an IR decoy were taken from the Academy kit.

 

The ordnance came from various sources. The Sidewinders under the wing tips were taken from an Italeri F-16C/D kit, they look better than the missiles from the Academy Bronco kit. Their launch rails came from an Italeri Bae Hawk 200. The quadruple Hellfire launchers on the underwing hardpoints were left over from an Italeri AH-1W, and they are a perfect load for this aircraft and its role. The LAU-10 and -19 missile pods on the stub wings were taken from the OV-10 kit.

  

Painting and markings:

Finding a suitable and somewhat interesting – but still plausible – paint scheme was not easy. Taking the A-10 as benchmark, an overall light grey livery (with focus on low contrast against the sky as protection against ground fire) would have been a likely choice – and in fact the last operational American OV-10s were painted in this fashion. But in order to provide a different look I used the contemporary USAF V-22Bs and Special Operations MC-130s as benchmark, which typically carry a darker paint scheme consisting of FS 36118 (suitably “Gunship Gray” :D) from above, FS 36375 underneath, with a low, wavy waterline, plus low-viz markings. Not spectacular, but plausible – and very similar to the late r/w Colombian OV-10s.

The cockpit tub became Dark Gull Grey (FS 36231, Humbrol 140) and the landing gear white (Revell 301).

 

The model received an overall black ink washing and some post-panel-shading, to liven up the dull all-grey livery. The decals were gathered from various sources, and I settled for black USAF low-viz markings. The “stars and bars” come from a late USAF F-4, the “IP” tail code was tailored from F-16 markings and the shark mouth was taken from an Academy AH-64. Most stencils came from another Academy OV-10 sheet and some other sources.

Decals were also used to create the trim on the propeller blades and markings on the ordnance.

 

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri) and some exhaust soot stains were added with graphite along the tail boom flanks.

  

A successful transplantation – but is this still a modified Bronco or already a kitbashing? The result looks quite plausible and menacing, even though the TOW Cobra front section appears relatively massive. But thanks to the bigger engines and extended wing tips the proportions still work. The large low-pressure tires look a bit goofy under the aircraft, but they are original. The grey livery works IMHO well, too – a more colorful or garish scheme would certainly have distracted from the modified technical basis.

A manta trawl skims the surface of the Chesapeake Bay in Maryland on Sept. 4, 2015. Julie Lawson of Trash Free Maryland and Stiv Wilson of The Story of Stuff Project invited advocates, educators, journalists, officials and others onboard for 13 days of sampling for microplastic, which animals can accidentally consume and which can release chemical pollutants. (Photo by Will Parson/Chesapeake Bay Program)

 

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A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

We are less than one month away from 611's return to the high iron for Norfolk Southern's 2016 excursion season. With the steam program's uncertain fate, I would get out and see this streamlined beauty while you can.

 

In this black and white photo, N&W 611 accelerates past the position light at Bowler, Virginia with 'The Cavalier' after a severe thunderstorm. Even at 40 mph, the rain and dark storm clouds took away enough light to blur the nose of the famous locomotive.

Florence Shelly Preserve in Susquehanna County, Pa., on Aug. 2, 2016. The 357-acre preserve is owned by the Nature Conservancy and features forest, fields, a stream, and glacial pond surrounded by a floating bog. (Photo by Will Parson/Chesapeake Bay Program)

 

USAGE REQUEST INFORMATION

The Chesapeake Bay Program's photographic archive is available for media and non-commercial use at no charge. To request permission, send an email briefly describing the proposed use to requests@chesapeakebay.net. Please do not attach jpegs. Instead, reference the corresponding Flickr URL of the image.

 

A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

F-35A aircraft AL-1 and an Italian Air Force KC-767 tanker come in for a landing at Naval Air Station Patuxent River, Maryland to complete the F-35 program’s first trans-Atlantic flight on Feb. 5, 2016. Learn more: bit.ly/1S Ecue0

In the biblical story of Jacob, from Genesis 28, Jacob witnesses angels ascending and descending a ladder from heaven. But in the painting the ladder doesn't come from heaven, but from a dark, round object emitting multi-colored lights. Though Jacob's Ladder is a popular symbol in freemasonry, is this rendering pointing to something more of an extraterrestrial nature? According to ancient astronaut theorists, Jacob's Ladder was nothing more than a ramp or a device with which to reach the realm of the gods, and the 'gods' were extraterrestrials.Traditional Christianity (most notably, CS Lewis) believes that extraterrestrial beings are simply angels, whether fallen or holy. The relatively new Indiana Jones movie, The Kingdom of the Skulls, say that aliens are not really extraterrestrial, but extradimensional. That describes what the Bible says about spiritual powers. According to the Air Force Project Blue Book, the unexplained percentage of encounters fit a spiritual, occult phenomenon. Some go on to say that alien beings are ultraterrestrial, meaning to say that these beings live among us and are what humans are to bears; both live on Earth, but don't interact; it'd be a stretch to say that a bear would comprehend being abducted in a human airplane. In a way, He is not a human (except through the Person of the Lord Jesus Christ). to us that He is a different Being altogether. But He is not a Grey or a Reptilian or Annunaki or biological or even matter; He is Spirit. Angels obviously ride on disc vehicles according to the Bible, and mainstream Christianity classifies aliens as spiritual beings of angels, not a science fiction astrobiological derivative. The medieval Dante notions of angels and demons of harping cherubs and horned devils must be overthrown.Assume there are beings besides humans, hailing from other worlds (universes?). This does not say anything about G-d, just the way some people stumbled upon backward tribes who thought the white men were gods, has nothing to do with the reality of G-d. It's agree that Ezekiel (and Jacob's ladder) speak of some form of aliens, from space. But their meaning does not change the reality of G-d. It does throw into question what people back then thought about angels. Still, their understanding of "UFO's" do not need to influence ours. In conclusion, it doesn't interfere with my beliefs. The ancient alien theory fails in that it classifies the aliens and UFOs as biological and materialistic, not spiritual. One of the more convoluted priest-written myths that make up the Old Testament book of Genesis is that of Jacob, the younger of twin boys who, nonetheless, received through fraud and deceit the blessings of first-born. This is the much revered ancestor of the “chosen” ones. There is hidden meaning in all of this, of course, but the focus for this blog is why this character’s name was changed to Israel. It is all inexplicably mixed in with an alleged wrestling match with an angel and a “dream” about a ladder upon which angels were seen to move up and down between heaven and Earth. The story of Jacob and his name change to Israel is found in the opening of biblical lore, Genesis–the book of beginnings. The focus here on this devious character is spurred by a recent television series called Ancient Aliens, which speculated that various unknowns in Earth’s ancient past hinge upon the aspect that extraterrestrials were responsible for those unknowns. This evaluation of the program’s biblical interpretations does not necessarily rule out that such visitations may have occurred. Like hard-line religionists, however, this theory overlooks or deliberately ignores many of the various clues that the priest-authors used to season the tale—clues that were drawn from prehistory lessons that once used groups of stars (constellations) to illustrate Creation principles of energy progression into visible forms. For example, Jacob’s grandfather also had his name changed from Abram to Abraham–and for the same reason, which is also not effectively explained. Jacob’s ladder is regarded as a religious “mystery,” which is referred to as the scala coeli (stairway). This “mystery” is no genuine mystery at all when one follows all the clues that are dropped throughout the story. In the book The Celestial Scripures (by this author), it is pointed out that symbols are employed which are easily recognized by initiates. Jacob is said to have gone out from Beer-sheba (Genesis 28:10), his course being toward Haran. The Beer part of the name means “well,” and the word sheba means “seven”, which indicates that the Life Principle advances through seven stages (symbolized as wells) of primordial development toward visible amassment, and the earliest phenomenon of this activity is seen as light. Thus we read that Jacob “…lighted upon a certain place and he tarried there all night (through that primordial energy plane) because the Sun was set…” (Genesis 28:11). In other words, energy is in the process of manifesting toward denser form–or definable matter form is “set“. At this point Jacob then had to take “…of the stones of that place…” and use them for his pillow. Now this is strange: Jacob is characterized as being a forward planning individual, so wouldn’t such a person have taken with him something to sleep upon during an overnight journey?The prophesy of Ezekiel was explained in the Talmud by Jewish sages that received the explanation from Ezekiel’s own students. The Jews in the times of the Mishna and Talmud where only a few generations after Ezekiel lived. There are many many books of Jewish thought and mysticism based on the visions of Ezekiel and none of them have any mention of Aliens. That prophecy is described as “The workings of the chariot” in Jewish literature. The Workings of the chariot are teachings that were originally only taught in parables, and only to the highest ranking scholars. The vision of the chariot is an elusion to very lofty esoteric concepts. Nobody in his time period believed he was speaking of aliens, or even actual physical beings of any sort. To clarify, this was a prophesy (one of 26 in the book of Ezekiel), which by definition is not a record of an event. No explanation is forthcoming for this lack of preparedness. Instead, he must lay his head upon a pile of stones, and then he has his famous mystifying dream of angel activity on a ladder that linked Heaven with Earth. (Genesis 28:12-17). To repeat, the Genesis story relates that the ladder was seen by Jacob in a dream, not as some actual physical encounter. The ladder that Jacob allegedly beheld, upon which angels or divine messengers were moving up and down, is coded reference to elementary particles that are becoming actively involved in the coalescing phase into biological life; thus it is the ladder-like DNA sequence that is referred to as the ladder which connects all life with the Source. It is at this point in the story that Jacob was then allegedly promised by God (the Life Principle personified) that he and his multitudes of descendants would be given possession of Canaan: but this “land” is not in regard to any Near East area on planet Earth, but symbolizes the advanced energy involvement as matter. This holy account is therefore not history of a specific “chosen” people, but is about how all life forms move through elemental energy phases into temporary matter form where self-aware consciousness is achieved. Nonetheless, this is all implied by the priest-authors to have occurred around the timeframe of 1760 BCE.

When Jacob awakened from this “dream,” he is quoted as saying, “How dreadful is this place!–this is none other than the house of God, and this is the gate of heaven.” (28:17). Huh? “This place” therefore refers to the pre-physical energy conditions or prototype circumstances which initiate matter manifestation. This is “dreadful” only because elementary consciousness is amassing to descend and pass over into visible dense matter identity. It is in this in-between development stage where Jacob “tarried” (it is not until chapter 32 that Jacob is actually transformed into self-aware matter-life as Israel). The stone that Jacob had used for his pillow he then set up as a pillar. Strangely, Jacob had not carried any sleeping gear for the overnight journey, but he had carried along a supply of oil which he poured upon the pillar. And he called that place of intensifying energy Beth-el (House of God).

 

Jacob is said to “tarry” in this prototype situation for fourteen years, and it is here that Rachel and her elder sister Leah enter the story, and both became his wives. Female figures represent energy substance. (So when other scriptural women, some called sisters, marries the lead character they are, being an interacting part of the energy spectrum, not committing incest.) Jacob also frolicked with the female servants of his wives–all with God’s blessing. From these unions Jacob allegedly fathered twelve sons, each to become the ancestors of the twelve tribes of Israel. When at last Jacob and his evolving family stole away from his father-in-law’s locale, they also left with stolen rudiments from the father-in-law before they passed over the river toward the mount Gilead (Genesis 31:21).

 

Later on (Genesis 32:28 and 35:10) Jacob is described as having to indulge in a wrestling match with an angel (some interpret it as a struggle with God). This peculiar wrestling match is said to have lasted “…until the breaking of day,” meaning until energy-form was becoming defined. In the brief description of the wrestling match it is impossible to follow which one of the combatants is Jacob and which one is the “man” during the combat. The reason for this seemingly garbled account is that both participants represent the same energy involvement which is in the process of transforming–or passing over–from primal energy conditions into defined form–or “until the breaking of the day.” When Jacob later asks the name of his opponent, Jacob is rebuffed. The question is never answered, but nonetheless “…he blessed him there.” Who blessed whom? The wrestling match is a parable for energy transformation, so the Life Principle blesses itself by the exertion of transformation! Thus the creative principle has advanced into defined matter form and so we read, “Thy name shall be called no more Jacob, but Israel; for as a prince hast thou power with God and with men, and has prevailed.” Jacob then named the place of combat as Peniel, which is said to mean, “I have seen God face to face, and my life is preserved.” Then in 32:31 it relates, “And as he (Jacob) passed over Peniel the sun rose upon him, and he halted upon his thigh”–upon his organ of generation.

So the teasing suggestion in the television series Ancient Aliens that perhaps the ladder in the Jacob fable represents extraterrestrials coming to Earth is another misinterpretation of prehistory lessons concerning the energies of Creation. But in various illustrations which show a ladder descending from a darkish oval area,* that does not signify a UFO; it represents the tunnel mouth out of primordial energy conditions from which energy as visible matter-forms descend. On the other hand the relationship with space and heavenly activity is not exactly alien to scriptures: each of the twelve sons of Jacob/Israel represents one of the signs from the Zodiac. In this dream, Jacob saw a ladder (or in some translations, a stairway) that connected heaven to earth. Additionally, Jacob is said to have seen God at the top of the ladder, and also angels, who were ascending and descending this structure. The story of Jacob’s Ladder may be found in the Book of Genesis.Jacob's Ladder (Hebrew: Sulam Yaakov סולם יעקב) is the colloquial name for a connection between the earth and heaven that the biblical Patriarch Jacob dreams about during his flight from his brother Esau, as described in the Book of Genesis. The significance of the dream has been somewhat debated, but most interpretations agree that it identified Jacob with the obligations and inheritance of the ethnic people chosen by God, as understood in Abrahamic religions. It has since been used as a symbolic reference in various other contexts.Jacob (Arabic: يَعْقُوب‎, translit. Yaʿqūb) is revered in Islam as a prophet and patriarch. Muslim scholars, especially of the perennialist tradition,drew a parallel with Jacob's vision of the ladder[11] and Muhammad's event of the Mi'raj.The ladder of Jacob was interpreted by Muslims to be one of the many symbols of God, and many saw Jacob's ladder as representing in its form the essence of Islam, which emphasizes following the "straight path". The twentieth-century scholar Martin Lings described the significance of the ladder in the Islamic mystic perspective: The ladder of the created Universe is the ladder which appeared in a dream to Jacob, who saw it stretching from Heaven to earth, with Angels going up and down upon it; and it is also the "straight path", for indeed the way of religion is none other than the way of creation itself retraced from its end back to its Beginning.esus said in John 1:51 "And he saith unto him, Verily, verily, I say unto you, Hereafter ye shall see heaven open, and the angels of God ascending and descending upon the Son of man." This statement has been interpreted as associating or implicating Jesus with the mythical ladder, in that Christ bridges the gap between Heaven and Earth. Jesus presents himself as the reality to which the ladder points; as Jacob saw in a dream the reunion of Heaven and Earth, Jesus brought this reunion, metaphorically the ladder, into reality. Adam Clarke, an early 19th-century Methodist theologian and Bible scholar, elaborates: That by the angels of God ascending and descending, is to be understood, that a perpetual intercourse should now be opened between heaven and earth, through the medium of Christ, who was God manifested in the flesh. Our blessed Lord is represented in his mediatorial capacity as the ambassador of God to men; and the angels ascending and descending upon the Son of Man, is a metaphor taken from the custom of dispatching couriers or messengers from the prince to his ambassador in a foreign court, and from the ambassador back to the prince. The theme of a ladder to heaven is often used by the Church Fathers. Irenaeus in the second century describes the Christian Church as the "ladder of ascent to God".In the third century, Origen explains that there are two ladders in the life of a Christian, the ascetic ladder that the soul climbs on the earth, by way of—and resulting in—an increase in virtue, and the soul's travel after death, climbing up the heavens towards the light of God. In the fourth century, Gregory of Nazianzus[8] speaks of ascending Jacob's Ladder by successive steps towards excellence, interpreting the ladder as an ascetic path, while Saint Gregory of Nyssa narrates, that Moses climbed on Jacob's Ladder to reach the heavens where he entered the tabernacle not made with hands, thus giving the Ladder a clear mystical meaning. The ascetic interpretation is found also in Saint John Chrysostom, who writes: "And so mounting as it were by steps, let us get to heaven by a Jacob’s ladder. For the ladder seems to me to signify in a riddle by that vision the gradual ascent by means of virtue, by which it is possible for us to ascend from earth to heaven, not using material steps, but improvement and correction of manners." Jacob's Ladder as an analogy for the spiritual ascetic of life enjoyed wide influence thanks to the classical work The Ladder of Divine Ascent by John Climacus.he classic Torah commentaries offer several interpretations of Jacob's ladder. According to the Midrash Genesis Rabbah, the ladder signified the exiles which the Jewish people would suffer before the coming of the Messiah. First the angel representing the 70-year exile of Babylonia climbed "up" 70 rungs, and then fell "down". Then the angel representing the exile of Persia went up a number of steps, and fell, as did the angel representing the exile of Greece. Only the fourth angel, which represented the final exile of Rome/Edom (whose guardian angel was Esau himself), kept climbing higher and higher into the clouds. Jacob feared that his children would never be free of Esau's domination, but God assured him that at the End of Days, Edom too would come falling down. Another interpretation of the ladder keys into the fact that the angels first "ascended" and then "descended". The Midrash explains that Jacob, as a holy man, was always accompanied by angels. When he reached the border of the land of Canaan (the future land of Israel), the angels who were assigned to the Holy Land went back up to Heaven and the angels assigned to other lands came down to meet Jacob. When Jacob returned to Canaan he was greeted by the angels who were assigned to the Holy Land. Yet another interpretation is this: The place at which Jacob stopped for the night was in reality Mount Moriah, the future home of the Temple in Jerusalem. The ladder therefore signifies the "bridge" between Heaven and earth, as prayers and sacrifices offered in the Holy Temple soldered a connection between God and the Jewish people. Moreover, the ladder alludes to the giving of the Torah as another connection between heaven and earth. In this interpretation, it is also significant that the Hebrew word for ladder, sulam (סלם) and the name for the mountain on which the Torah was given, Sinai (סיני) have the same gematria (numerical value of the letters). The Hellenistic Jewish philosopher Philo, born in Alexandria, (d. ca. 50 CE) presents his allegorical interpretation of the ladder in the first book of his De somniis. There he gives four interpretations, which are not mutually exclusive: The angels represent souls descending to and ascending from bodies (some consider this to be Philo's clearest reference to the doctrine of reincarnation). In the second interpretation the ladder is the human soul and the angels are God's logoi, pulling the soul up in distress and descending in compassion. In the third view the dream depicts the ups and downs of the life of the "practiser" (of virtue vs. sin). Finally the angels represent the continually changing affairs of men. A hilltop overlooking the Israeli settlement of Beit El north of Jerusalem that is believed by some to be the site of Jacob's dream is a tourist destination during the holiday of Sukkot.Is it the case that Ezekiel saw an alien-operated flying machine from outer space? No, Ezekiel did not see an alien spaceship. How, then, are his visions to be explained? When one looks into Ezekiel’s prophetic book, it becomes clear that Ezekiel did see some strange things. From a quick reading of chapter one, it becomes apparent that Ezekiel saw a “great cloud with raging fire engulfing itself ” (vs. 4), four living creatures from within the cloud (vs. 5), a wheel beside each living creature (vs. 15), and the rims of the wheels full of eyes (vs. 18), among many other things. Indeed, the things seen by Ezekiel were amazing and unusual to say the least.

But with a little research into the biblical message, it becomes clear that Ezekiel’s writing and visions were apocalyptic in nature—very similar to the writings found in both Daniel and Revelation. The visions Ezekiel described are of heavenly, spiritual beings, not “alien life forms.” By comparing the description of the living creatures in Ezekiel to that of the living creatures that surround the throne of God in Revelation 4, one quickly realizes that the scenes witnessed by Ezekiel, John, Daniel, and other inspired writers were visions of God and His spiritual host of heaven. As further evidence of this fact, at the end of Ezekiel 1, after describing “a likeness with the appearance of a man” on a throne, Ezekiel wrote: “This was the appearance of the likeness of the glory of the Lord” (1:28). Then, a few verses later in chapter 2, this same person said to Ezekiel, “Son of man, I am sending you to the children of Israel, to a rebellious nation that has rebelled against Me” (2:3). Ezekiel fully understood this to be the Lord talking to Him, that the vision was of spiritual beings, and that he had not had an encounter

 

en.wikipedia.org/wiki/Jacob%27s_Ladder

  

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One of the most remarkable of the Wunderwaffen (wonder weapons) produced by the Nazi Germany during World War II, the Messerschmitt Me 163 Komet holds the distinction of being the first and only tailless rocket-powered interceptor to see operational service. Like the other advanced weapons fielded by Germany during the final year of World War II, the Me 163 had little actual effect on the outcome of the war. Considering the conditions under which it was developed and deployed, however, the Me 163 can be rightly considered a significant technological accomplishment.

 

The concept for the Komet originated during the late thirties, when rocket propulsion for aircraft became increasingly attractive to a number of air planners in Nazi Germany. Although rockets potentially offered astounding performance advantages for an interceptor, their high fuel consumption posed seemingly insurmountable design difficulties. In spite of this, the Reichsluftfahrtministerium or RLM (Reich Air Ministry) supported the work of rocket engine designer Hellmuth Walter, issuing a contract in 1936 for the development of an 882 lb. thrust motor designated the R I-203. The engine was to be fueled by a mixture of T-Stoff (80 percent hydrogen peroxide with oxyquinoline or phosphate as a stabilizer and 20 percent water) and Z-Stoff (an aqueous solution of calcium permanganate) and intended to power the Heinkel He 176 aircraft then under development. Because the He 176, which had been designed solely as a high-speed aircraft with no military potential, the RLM ordered the Deutsches Forschungsinsitut für Segelflug (German Research Institute for Gliding Flight or DFS) to produce a second prototype of the DFS 39, a tailless aircraft designed by Dr. Alexander Lippisch. It was also to be a rocket-powered design under a top-secret program designated Project X. DFS was to build the aircraft's wings while Heinkel, which was already working on the He 176, was to manufacture the rest of the airframe. It soon became apparent to Lippisch, however, that the DFS 39's wingtip-mounted rudders would likely cause unacceptable flutter and that a central fin and rudder would offer better control. It was replaced by a new design, designated the DFS 194, with a single large vertical stabilizer mounted on the fuselage. Like the DFS 39, it was initially intended only to be a conventionally powered flying test bed for later rocket-powered designs.

 

Difficulties arising from the division of work between DFS and Heinkel and the secrecy surrounding the project led Lippisch to request that he be allowed to leave DFS and join Messerschmitt AG. The RLM granted his request on January 2, 1939, and shortly after Lippisch, his design team, and the partially completed DFS 194 arrived at the Messerschmitt works in Augsburg, it was decided to adopt rocket power for the aircraft. The airframe was completed at the Messerschmitt works in Augsburg and shipped to Pennemünde West early in 1940 for installation of a Walter R I-203. Flight-testing revealed that despite the unreliability its motor, the aircraft had excellent performance characteristics, reaching a speed of 342 mph in level flight during one test.

 

The move to Messerschmitt brought a change in the program's designation to Me 163. The success of the DFS 194 spurred development of the first prototype Me 163, designated the Me 163 V1, which was completed during early 1941. Flight testing commenced in the spring of 1941, comprising a series of unpowered flights before the Me 163 V1 was shipped to Peenemünde West for installation of a 1,653 lb. thrust Walter RII-203 rocket motor and its first powered flights. Despite a series of accidents and explosions involving the unreliable motor, on October 2, 1941, the Me 163 V1 set a new world speed record of 1,004.5 kph (623.8 mph). Impressed by the aircraft's performance, the RLM instructed Lippisch was to design an improved version of the Me 163 around a more powerful rocket motor under development by Walter. The new design, designated Me 163 B, was to be an operational interceptor and represented an almost complete redesign of the aircraft. Its landing gear remained similar to the earlier design, employing a wheeled trolley that was jettisoned after takeoff and an extendable skid for landing. Additional prototypes based on the Me 163 V1 configuration were designated Me 163 A.

 

The first Me 163 B prototype, the Me 163 V3, was completed in April 1942, but it was not until early fall that the first Walter 109-509A motors were ready for installation. The new motor used a more volatile fuel mixture of T-Stoff (80 percent hydrogen peroxide and 20 percent water) and C-Stoff (hydrazine hydrate, methyl alcohol, and water), which provided a maximum thrust of 1,500 kg (3,300 lb.). Unlike the earlier cold principle motor which directed all of the oxygen and water vapor produced by the decomposition of the hydrogen peroxide out of the engine's nozzle, the new motor employed a hot system in which the oxygen was ignited for additional thrust and better fuel efficiency. Flight testing of the first series of Me 163 B-0 preproduction aircraft proceeded through 1942 and demonstrated the dangers of the Me 163's unproven propulsion system. As fuel passed through the Walter motor's pumps, areas of vacuum sometimes formed in the liquid. This cavitation often caused a catastrophic explosion when the motor was started. Once in the air, the aircraft's climb rate proved remarkable, but compressibility problems limited its safe speed in a dive to below Mach 0.82. The Komet's landing gear also proved troublesome, with numerous pilots suffering back injuries as a result of the skid failing to extend properly or failing upon touchdown. Even when the skid operated properly, landings were always without power and at high speed, requiring the utmost care on the part of the pilot to prevent the aircraft from overturning on soft ground. Such mishaps often led to an explosion or the pilot being severely burned by leaking fuel.

 

Despite the problems encountered during testing, plans proceeded during 1943 to equip the first operational units with the operational version of the Komet, designated the Me 163 B-1a. Production began at dispersed facilities by the Klemm concern, but was later transferred to Junkers as the result of quality control problems. An operational training unit, Erprobungskommando 16 or EK 16 was formed during July 1943 at Pennemünde West, but moved to Bad Zwischenahn before the first group of pilot trainees arrived as the result of allied bombing of Pennemünde. The unit finally received its first group of 30 pilot trainees in the fall of 1943. By May 1944, organization of Jagdgeschwader 400 or JG 400, the first operational Me 163 wing, began in earnest with the formation of the unit's first group (I./JG 400) under the command of Hauptmann Wolfgang Späte. Späte planned to deploy Me 163s from a string of bases, each close enough that the short range of the Me 163 overlapped. The plan was never realized, owing in part to the special facilities needed for the aircraft. Instead, I./JG 400 was to provide protection for the synthetic oil refineries at Leuna, some 90 km (55 miles) from its base at Brandis. Two additional Me 163 groups, II. And III./JG 400 were formed before the end of the war, but saw limited combat.

 

The unit made its first interception of Allied bombers on August 16, 1944 without success. Early combat experiences demonstrated a number of problems that prevented the Me 163 from ever becoming an effective weapon. Although the aircraft's two MK 108 30mm cannons were capable of downing a four-engine bomber with only three or four hits, the Komet's high speed, coupled with the cannons' slow rate of fire and short range made effective gunnery nearly impossible against the slow moving bombers. As a result, Me 163 pilots recorded a total of only nine kills. Although capable of reaching its service ceiling of 12,100 m (39,690 ft) in just under three-and-a-half minutes, the Me 163 carried only enough fuel for eight minutes of powered flight. After one or two firing passes, the pilot had to glide back to base with no means of escaping Allied escort fighters. In response to pilots' combat reports, alternative weapons, including vertically firing 50mm cannons triggered by a photocell as the Me 163 passed through a bomber's shadow were tested but not produced in quantity. An improved variant of the aircraft with a greater endurance and a tricycle landing gear, designated the Me 163 C, was also produced in small numbers before the war's end, but was not flown operationally.

 

The operational history of the National Air and Space Museum's Me 163 B-1a, Werk-Nummer (serial number) 191301, remains obscure. One of five Me 163s brought to the United States after the war, it arrived at Freeman Field, Indiana, during the summer of 1945. There it received the foreign equipment code FE-500. On April 12, 1946, it was flown aboard a cargo aircraft to the U.S. Army Air Forces facility at Muroc dry lake in California for flight testing. Testing began there on May 3, 1946 in the presence of Dr. Alexander Lippisch and involved towing the unfueled Komet behind a B-29 to an altitude of 9,000 to 10,500 m (30,000 to 35,000 ft) before it was released for a glide back to earth under the control of test pilot Major Gus Lundquist. Powered tests were planned, but not carried out after delamination of the aircraft's wooden wings was discovered. It was then stored at Norton AFB, California until 1954, when it was transferred to the Smithsonian Institution. The aircraft remained on display in an unrestored condition at the museum's Paul E. Garber Restoration and Storage Facility in Suitland, Maryland, until 1996, when it was lent to the Mighty Eighth Air Force Heritage Museum in Savannah, Georgia. It is currently displayed at the Museum's Steven F. Udvar-Hazy Center in Chantilly, VA.

 

airandspace.si.edu/collection-objects/messerschmitt-me-16...

Fungi grow in the forest at the Ned Smith Center for Nature and Art near Millersburg, Pa., on Oct. 28, 2016. Fungi play a major role in regenerating the forest by digesting fallen trees and plant matter, effectively recycling the nutrients back into the soil. (Photo by Leslie Boorhem-Stephenson/Chesapeake Bay Program)

 

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Florence Shelly Preserve in Susquehanna County, Pa., on Aug. 2, 2016. The 357-acre preserve is owned by the Nature Conservancy and features forest, fields, a stream, and glacial pond surrounded by a floating bog. (Photo by Will Parson/Chesapeake Bay Program)

 

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+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The OV-10 Bronco was initially conceived in the early 1960s through an informal collaboration between W. H. Beckett and Colonel K. P. Rice, U.S. Marine Corps, who met at Naval Air Weapons Station China Lake, California, and who also happened to live near each other. The original concept was for a rugged, simple, close air support aircraft integrated with forward ground operations. At the time, the U.S. Army was still experimenting with armed helicopters, and the U.S. Air Force was not interested in close air support.

The concept aircraft was to operate from expedient forward air bases using roads as runways. Speed was to be from very slow to medium subsonic, with much longer loiter times than a pure jet. Efficient turboprop engines would give better performance than piston engines. Weapons were to be mounted on the centerline to get efficient aiming. The inventors favored strafing weapons such as self-loading recoilless rifles, which could deliver aimed explosive shells with less recoil than cannons, and a lower per-round weight than rockets. The airframe was to be designed to avoid the back blast.

 

Beckett and Rice developed a basic platform meeting these requirements, then attempted to build a fiberglass prototype in a garage. The effort produced enthusiastic supporters and an informal pamphlet describing the concept. W. H. Beckett, who had retired from the Marine Corps, went to work at North American Aviation to sell the aircraft.

The aircraft's design supported effective operations from forward bases. The OV-10 had a central nacelle containing a crew of two in tandem and space for cargo, and twin booms containing twin turboprop engines. The visually distinctive feature of the aircraft is the combination of the twin booms, with the horizontal stabilizer that connected them at the fin tips. The OV-10 could perform short takeoffs and landings, including on aircraft carriers and large-deck amphibious assault ships without using catapults or arresting wires. Further, the OV-10 was designed to take off and land on unimproved sites. Repairs could be made with ordinary tools. No ground equipment was required to start the engines. And, if necessary, the engines would operate on high-octane automobile fuel with only a slight loss of power.

 

The aircraft had responsive handling and could fly for up to 5½ hours with external fuel tanks. The cockpit had extremely good visibility for both pilot and co-pilot, provided by a wrap-around "greenhouse" that was wider than the fuselage. North American Rockwell custom ejection seats were standard, with many successful ejections during service. With the second seat removed, the OV-10 could carry 3,200 pounds (1,500 kg) of cargo, five paratroopers, or two litter patients and an attendant. Empty weight was 6,969 pounds (3,161 kg). Normal operating fueled weight with two crew was 9,908 pounds (4,494 kg). Maximum takeoff weight was 14,446 pounds (6,553 kg).

The bottom of the fuselage bore sponsons or "stub wings" that improved flight performance by decreasing aerodynamic drag underneath the fuselage. Normally, four 7.62 mm (.308 in) M60C machine guns were carried on the sponsons, accessed through large forward-opening hatches. The sponsons also had four racks to carry bombs, pods, or fuel. The wings outboard of the engines contained two additional hardpoints, one per side. Racked armament in the Vietnam War was usually seven-shot 2.75 in (70 mm) rocket pods with white phosphorus marker rounds or high-explosive rockets, or 5" (127 mm) four-shot Zuni rocket pods. Bombs, ADSIDS air-delivered/para-dropped unattended seismic sensors, Mk-6 battlefield illumination flares, and other stores were also carried.

Operational experience showed some weaknesses in the OV-10's design. It was significantly underpowered, which contributed to crashes in Vietnam in sloping terrain because the pilots could not climb fast enough. While specifications stated that the aircraft could reach 26,000 feet (7,900 m), in Vietnam the aircraft could reach only 18,000 feet (5,500 m). Also, no OV-10 pilot survived ditching the aircraft.

 

The OV-10 served in the U.S. Air Force, U.S. Marine Corps, and U.S. Navy, as well as in the service of a number of other countries. In U.S. military service, the Bronco was operated until the early Nineties, and obsoleted USAF OV-10s were passed on to the Bureau of Alcohol, Tobacco, and Firearms for anti-drug operations. A number of OV-10As furthermore ended up in the hands of the California Department of Forestry (CDF) and were used for spotting fires and directing fire bombers onto hot spots.

 

This was not the end of the OV-10 in American military service, though: In 2012, the type gained new attention because of its unique qualities. A $20 million budget was allocated to activate an experimental USAF unit of two airworthy OV-10Gs, acquired from NASA and the State Department. These machines were retrofitted with military equipment and were, starting in May 2015, deployed overseas to support Operation “Inherent Resolve”, flying more than 120 combat sorties over 82 days over Iraq and Syria. Their concrete missions remained unclear, and it is speculated they provided close air support for Special Forces missions, esp. in confined urban environments where the Broncos’ loitering time and high agility at low speed and altitude made them highly effective and less vulnerable than helicopters.

Furthermore, these Broncos reputedly performed strikes with the experimental AGR-20A “Advanced Precision Kill Weapons System (APKWS)”, a Hydra 70-millimeter rocket with a laser-seeking head as guidance - developed for precision strikes against small urban targets with little collateral damage. The experiment ended satisfactorily, but the machines were retired again, and the small unit was dissolved.

 

However, the machines had shown their worth in asymmetric warfare, and the U.S. Air Force decided to invest in reactivating the OV-10 on a regular basis, despite the overhead cost of operating an additional aircraft type in relatively small numbers – but development and production of a similar new type would have caused much higher costs, with an uncertain time until an operational aircraft would be ready for service. Re-activating a proven design and updating an existing airframe appeared more efficient.

The result became the MV-10H, suitably christened “Super Bronco” but also known as “Black Pony”, after the program's internal name. This aircraft was derived from the official OV-10X proposal by Boeing from 2009 for the USAF's Light Attack/Armed Reconnaissance requirement. Initially, Boeing proposed to re-start OV-10 manufacture, but this was deemed uneconomical, due to the expected small production number of new serial aircraft, so the “Black Pony” program became a modernization project. In consequence, all airframes for the "new" MV-10Hs were recovered OV-10s of various types from the "boneyard" at Davis-Monthan Air Force Base in Arizona.

 

While the revamped aircraft would maintain much of its 1960s-vintage rugged external design, modernizations included a completely new, armored central fuselage with a highly modified cockpit section, ejection seats and a computerized glass cockpit. The “Black Pony” OV-10 had full dual controls, so that either crewmen could steer the aircraft while the other operated sensors and/or weapons. This feature would also improve survivability in case of incapacitation of a crew member as the result from a hit.

The cockpit armor protected the crew and many vital systems from 23mm shells and shrapnel (e. g. from MANPADS). The crew still sat in tandem under a common, generously glazed canopy with flat, bulletproof panels for reduced sun reflections, with the pilot in the front seat and an observer/WSO behind. The Bronco’s original cargo capacity and the rear door were retained, even though the extra armor and defensive measures like chaff/flare dispensers as well as an additional fuel cell in the central fuselage limited the capacity. However, it was still possible to carry and deploy personnel, e. g. small special ops teams of up to four when the aircraft flew in clean configuration.

Additional updates for the MV-10H included structural reinforcements for a higher AUW and higher g load maneuvers, similar to OV-10D+ standards. The landing gear was also reinforced, and the aircraft kept its ability to operate from short, improvised airstrips. A fixed refueling probe was added to improve range and loiter time.

 

Intelligence sensors and smart weapon capabilities included a FLIR sensor and a laser range finder/target designator, both mounted in a small turret on the aircraft’s nose. The MV-10H was also outfitted with a data link and the ability to carry an integrated targeting pod such as the Northrop Grumman LITENING or the Lockheed Martin Sniper Advanced Targeting Pod (ATP). Also included was the Remotely Operated Video Enhanced Receiver (ROVER) to provide live sensor data and video recordings to personnel on the ground.

 

To improve overall performance and to better cope with the higher empty weight of the modified aircraft as well as with operations under hot-and-high conditions, the engines were beefed up. The new General Electric CT7-9D turboprop engines improved the Bronco's performance considerably: top speed increased by 100 mph (160 km/h), the climb rate was tripled (a weak point of early OV-10s despite the type’s good STOL capability) and both take-off as well as landing run were almost halved. The new engines called for longer nacelles, and their circular diameter markedly differed from the former Garrett T76-G-420/421 turboprop engines. To better exploit the additional power and reduce the aircraft’s audio signature, reversible contraprops, each with eight fiberglass blades, were fitted. These allowed a reduced number of revolutions per minute, resulting in less noise from the blades and their tips, while the engine responsiveness was greatly improved. The CT7-9Ds’ exhausts were fitted with muzzlers/air mixers to further reduce the aircraft's noise and heat signature.

Another novel and striking feature was the addition of so-called “tip sails” to the wings: each wingtip was elongated with a small, cigar-shaped fairing, each carrying three staggered, small “feather blade” winglets. Reputedly, this installation contributed ~10% to the higher climb rate and improved lift/drag ratio by ~6%, improving range and loiter time, too.

Drawing from the Iraq experience as well as from the USMC’s NOGS test program with a converted OV-10D as a night/all-weather gunship/reconnaissance platform, the MV-10H received a heavier gun armament: the original four light machine guns that were only good for strafing unarmored targets were deleted and their space in the sponsons replaced by avionics. Instead, the aircraft was outfitted with a lightweight M197 three-barrel 20mm gatling gun in a chin turret. This could be fixed in a forward position at high speed or when carrying forward-firing ordnance under the stub wings, or it could be deployed to cover a wide field of fire under the aircraft when it was flying slower, being either slaved to the FLIR or to a helmet sighting auto targeting system.

The original seven hardpoints were retained (1x ventral, 2x under each sponson, and another pair under the outer wings), but the total ordnance load was slightly increased and an additional pair of launch rails for AIM-9 Sidewinders or other light AAMs under the wing tips were added – not only as a defensive measure, but also with an anti-helicopter role in mind; four more Sidewinders could be carried on twin launchers under the outer wings against aerial targets. Other guided weapons cleared for the MV-10H were the light laser-guided AGR-20A and AGM-119 Hellfire missiles, the Advanced Precision Kill Weapon System upgrade to the light Hydra 70 rockets, the new Laser Guided Zuni Rocket which had been cleared for service in 2010, TV-/IR-/laser-guided AGM-65 Maverick AGMs and AGM-122 Sidearm anti-radar missiles, plus a wide range of gun and missile pods, iron and cluster bombs, as well as ECM and flare/chaff pods, which were not only carried defensively, but also in order to disrupt enemy ground communication.

 

In this configuration, a contract for the conversion of twelve mothballed American Broncos to the new MV-10H standard was signed with Boeing in 2016, and the first MV-10H was handed over to the USAF in early 2018, with further deliveries lasting into early 2020. All machines were allocated to the newly founded 919th Special Operations Support Squadron at Duke Field (Florida). This unit was part of the 919th Special Operations Wing, an Air Reserve Component (ARC) of the United States Air Force. It was assigned to the Tenth Air Force of Air Force Reserve Command and an associate unit of the 1st Special Operations Wing, Air Force Special Operations Command (AFSOC). If mobilized the wing was gained by AFSOC (Air Force Special Operations Command) to support Special Tactics, the U.S. Air Force's special operations ground force. Similar in ability and employment to Marine Special Operations Command (MARSOC), U.S. Army Special Forces and U.S. Navy SEALs, Air Force Special Tactics personnel were typically the first to enter combat and often found themselves deep behind enemy lines in demanding, austere conditions, usually with little or no support.

 

The MV-10Hs are expected to provide support for these ground units in the form of all-weather reconnaissance and observation, close air support and also forward air control duties for supporting ground units. Precision ground strikes and protection from enemy helicopters and low-flying aircraft were other, secondary missions for the modernized Broncos, which are expected to serve well into the 2040s. Exports or conversions of foreign OV-10s to the Black Pony standard are not planned, though.

  

General characteristics:

Crew: 2

Length: 42 ft 2½ in (12,88 m) incl. pitot

Wingspan: 45 ft 10½ in(14 m) incl. tip sails

Height: 15 ft 2 in (4.62 m)

Wing area: 290.95 sq ft (27.03 m²)

Airfoil: NACA 64A315

Empty weight: 9,090 lb (4,127 kg)

Gross weight: 13,068 lb (5,931 kg)

Max. takeoff weight: 17,318 lb (7,862 kg)

 

Powerplant:

2× General Electric CT7-9D turboprop engines, 1,305 kW (1,750 hp) each,

driving 8-bladed Hamilton Standard 8 ft 6 in (2.59 m) diameter constant-speed,

fully feathering, reversible contra-rotating propellers with metal hub and composite blades

 

Performance:

Maximum speed: 390 mph (340 kn, 625 km/h)

Combat range: 198 nmi (228 mi, 367 km)

Ferry range: 1,200 nmi (1,400 mi, 2,200 km) with auxiliary fuel

Maximum loiter time: 5.5 h with auxiliary fuel

Service ceiling: 32.750 ft (10,000 m)

13,500 ft (4.210 m) on one engine

Rate of climb: 17.400 ft/min (48 m/s) at sea level

Take-off run: 480 ft (150 m)

740 ft (227 m) to 50 ft (15 m)

1,870 ft (570 m) to 50 ft (15 m) at MTOW

Landing run: 490 ft (150 m)

785 ft (240 m) at MTOW

1,015 ft (310 m) from 50 ft (15 m)

 

Armament:

1x M197 3-barreled 20 mm Gatling cannon in a chin turret with 750 rounds ammo capacity

7x hardpoints for a total load of 5.000 lb (2,270 kg)

2x wingtip launch rails for AIM-9 Sidewinder AAMs

  

The kit and its assembly:

This fictional Bronco update/conversion was simply spawned by the idea: could it be possible to replace the original cockpit section with one from an AH-1 Cobra, for a kind of gunship version?

 

The basis is the Academy OV-10D kit, mated with the cockpit section from a Fujimi AH-1S TOW Cobra (Revell re-boxing, though), chosen because of its “boxy” cockpit section with flat glass panels – I think that it conveys the idea of an armored cockpit section best. Combining these parts was not easy, though, even though the plan sound simple. Initially, the Bronco’s twin booms, wings and stabilizer were built separately, because this made PSR on these sections easier than trying the same on a completed airframe. One of the initial challenges: the different engines. I wanted something uprated, and a different look, and I had a pair of (excellent!) 1:144 resin engines from the Russian company Kompakt Zip for a Tu-95 bomber at hand, which come together with movable(!) eight-blade contraprops that were an almost perfect size match for the original three-blade props. Biggest problem: the Tu-95 nacelles have a perfectly circular diameter, while the OV-10’s booms are square and rectangular. Combining these parts and shapes was already a messy PST affair, but it worked out quite well – even though the result rather reminds of some Chinese upgrade measure (anyone know the Tu-4 copies with turboprops? This here looks similar!). But while not pretty, I think that the beafier look works well and adds to the idea of a “revived” aircraft. And you can hardly beat the menacing look of contraprops on anything...

The exotic, so-called “tip sails” on the wings, mounted on short booms, are a detail borrowed from the Shijiazhuang Y-5B-100, an updated Chinese variant/copy of the Antonov An-2 biplane transporter. The booms are simple pieces of sprue from the Bronco kit, the winglets were cut from 0.5mm styrene sheet.

 

For the cockpit donor, the AH-1’s front section was roughly built, including the engine section (which is a separate module, so that the basic kit can be sold with different engine sections), and then the helicopter hull was cut and trimmed down to match the original Bronco pod and to fit under the wing. This became more complicated than expected, because a) the AH-1 cockpit and the nose are considerably shorter than the OV-10s, b) the AH-1 fuselage is markedly taller than the Bronco’s and c) the engine section, which would end up in the area of the wing, features major recesses, making the surface very uneven – calling for massive PSR to even this out. PSR was also necessary to hide the openings for the Fujimi AH-1’s stub wings. Other issues: the front landing gear (and its well) had to be added, as well as the OV-10 wing stubs. Furthermore, the new cockpit pod’s rear section needed an aerodynamical end/fairing, but I found a leftover Academy OV-10 section from a build/kitbashing many moons ago. Perfect match!

All these challenges could be tackled, even though the AH-1 cockpit looks surprisingly stout and massive on the Bronco’s airframe - the result looks stockier than expected, but it works well for the "Gunship" theme. Lots of PSR went into the new central fuselage section, though, even before it was mated with the OV-10 wing and the rest of the model.

Once cockpit and wing were finally mated, the seams had to disappear under even more PSR and a spinal extension of the canopy had to be sculpted across the upper wing surface, which would meld with the pod’s tail in a (more or less) harmonious shape. Not an easy task, and the fairing was eventually sculpted with 2C putty, plus even more PSR… Looks quite homogenous, though.

 

After this massive body work, other hardware challenges appeared like small distractions. The landing gear was another major issue because the deeper AH-1 section lowered the ground clearance, also because of the chin turret. To counter this, I raised the OV-10’s main landing gear by ~2mm – not much, but it was enough to create a credible stance, together with the front landing gear transplant under the cockpit, which received an internal console to match the main landing gear’s length. Due to the chin turret and the shorter nose, the front wheel retracts backwards now. But this looks quite plausible, thanks to the additional space under the cockpit tub, which also made a belt feed for the gun’s ammunition supply believable.

To enhance the menacing look I gave the model a fixed refueling boom, made from 1mm steel wire and a receptor adapter sculpted with white glue. The latter stuff was also used add some antenna fairings around the hull. Some antennae, chaff dispensers and an IR decoy were taken from the Academy kit.

 

The ordnance came from various sources. The Sidewinders under the wing tips were taken from an Italeri F-16C/D kit, they look better than the missiles from the Academy Bronco kit. Their launch rails came from an Italeri Bae Hawk 200. The quadruple Hellfire launchers on the underwing hardpoints were left over from an Italeri AH-1W, and they are a perfect load for this aircraft and its role. The LAU-10 and -19 missile pods on the stub wings were taken from the OV-10 kit.

  

Painting and markings:

Finding a suitable and somewhat interesting – but still plausible – paint scheme was not easy. Taking the A-10 as benchmark, an overall light grey livery (with focus on low contrast against the sky as protection against ground fire) would have been a likely choice – and in fact the last operational American OV-10s were painted in this fashion. But in order to provide a different look I used the contemporary USAF V-22Bs and Special Operations MC-130s as benchmark, which typically carry a darker paint scheme consisting of FS 36118 (suitably “Gunship Gray” :D) from above, FS 36375 underneath, with a low, wavy waterline, plus low-viz markings. Not spectacular, but plausible – and very similar to the late r/w Colombian OV-10s.

The cockpit tub became Dark Gull Grey (FS 36231, Humbrol 140) and the landing gear white (Revell 301).

 

The model received an overall black ink washing and some post-panel-shading, to liven up the dull all-grey livery. The decals were gathered from various sources, and I settled for black USAF low-viz markings. The “stars and bars” come from a late USAF F-4, the “IP” tail code was tailored from F-16 markings and the shark mouth was taken from an Academy AH-64. Most stencils came from another Academy OV-10 sheet and some other sources.

Decals were also used to create the trim on the propeller blades and markings on the ordnance.

 

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri) and some exhaust soot stains were added with graphite along the tail boom flanks.

  

A successful transplantation – but is this still a modified Bronco or already a kitbashing? The result looks quite plausible and menacing, even though the TOW Cobra front section appears relatively massive. But thanks to the bigger engines and extended wing tips the proportions still work. The large low-pressure tires look a bit goofy under the aircraft, but they are original. The grey livery works IMHO well, too – a more colorful or garish scheme would certainly have distracted from the modified technical basis.

The 2016 Chesapeake Executive Council meeting is held on Oct. 4, 2016 at the Blandy Experimental Farm in Boyce, Virginia. It was announced that Pennsylvania will have $28 million in the next year to combat agricultural pollution, with $12.7 million coming from the U.S. Department of Agriculture, $4 million from the U.S. Environmental Protection Agency and $11.8 coming mostly from shifts within the Pennsylvania budget. (Photo by Leslie Boorhem-Stephenson/Chesapeake Bay Program)

 

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The Mohonk Mountain House, also known as Lake Mohonk Mountain House, is an American resort hotel located on the Shawangunk Ridge in Ulster County, New York. Its location in the town of New Paltz, New York is just beyond the southern border of the Catskill Mountains, west of the Hudson River.

 

The National Historic Landmark Program's "Statement of Significance", as of the site's historic landmark designation in 1986, stated:

 

Begun in the 1870s as a small resort for family and friends by the Smiley brothers, it became so popular that it was enlarged many times. Because of the Smileys' love of the outdoor life, the area around the hotel was treated as an integral part of the attractions of the resort. Much of this area was planned as an experiment in conservation of the natural environment, and as an educational tool for the study of botany, geology, and outdoor living.

 

The resort is located on the shore of Lake Mohonk, which is half a mile (800 m) long and 60 feet (18 m) deep. The main structure was built by Quaker twin brothers Albert and Alfred Smiley between 1869 and 1910.

 

From 1883 to 1916, annual conferences took place at Mohonk Mountain House, sponsored by Albert Smiley, to improve the living standards of Native American Indian populations. These meetings brought together government representatives of the Bureau of Indian Affairs and the House and Senate committees on Indian Affairs, as well as educators, philanthropists, and Indian leaders to discuss the formulation of policy. The Haverford College library holds 22,000 records from the 34 conference reports for researchers and students of American history.

 

The hotel hosted the Lake Mohonk Conference on International Arbitration between 1895 and 1916, which was instrumental in creating the Permanent Court of Arbitration in The Hague, Netherlands. Those conference papers were donated by the Smiley Family to Swarthmore College for research.

 

The house was given a United Nations Environment Programme Award in 1994 in honor of "125 years of stewardship". According to the National Trust for Historic Preservation, "Through its buildings and roads, its land, and its spirit, Mohonk exemplifies America's history and culture. Mohonk has since managed to maintain its 19th century character into the 21st century."

 

The resort was sued in 2014 by 200 guests who had become ill in a norovirus outbreak after staying there, who claimed the owners of the Mohonk Mountain House had been aware of the gastrointestinal illness at the resort prior to the arrival of the guests. The guests accused Mohonk of “intentional, willful, wanton, illegal ... and deliberate disregard for the health, safety and rights of plaintiffs.” The resort settled the claims for $875,000 two years later.

Description

 

Mohonk Mountain House has 259 guest rooms, including 28 tower rooms, an indoor pool and spa, and an outdoor ice-skating rink for winter use. The property consists of 1,325 acres (536 ha), and much of it is landscaped with meadows and gardens. It adjoins the Mohonk Preserve, which is crisscrossed by 85 miles (140 km) of hiking trails and carriage roads. The Smileys conveyed the majority of their property to the preserve.

 

The Mohonk Mountain House has hosted many famous visitors including industrialist John D. Rockefeller, naturalist John Burroughs, industrialist Andrew Carnegie, and American presidents Theodore Roosevelt, William Howard Taft, Rutherford B. Hayes, Chester A. Arthur, and Bill Clinton. Guests have also included former First Lady Julia Grant, author Thomas Mann, and religious leaders such as Rabbi Louis Finkelstein, Reverend Ralph W. Sockman, Reverend Francis Edward Clark. `Abdu'l-Bahá, the eldest son of Bahá'í Faith founder Bahá'u'lláh, stayed there in 1912 during the Lake Mohonk Conference on International Arbitration as part of his journeys to the West.

 

from Wikipedia

The Space Shuttle prototype Enterprise flies free after being released from NASA's 747 Shuttle Carrier Aircraft (SCA) over Rogers Dry Lakebed during the second of five free flights carried out at the Dryden Flight Research Center, Edwards, California, as part of the Shuttle program's Approach and Landing Tests (ALT).

 

The tests were conducted to verify orbiter aerodynamics and handling characteristics in preparation for orbital flights with the Space Shuttle Columbia beginning in April 1981. A tail cone over the main engine area of Enterprise smoothed out turbulent air flow during flight. It was removed on the two last free flights to accurately check approach and landing characteristics. A series of test flights during which Enterprise was taken aloft atop the SCA, but was not released, preceded the free flight tests. The Space Shuttle Approach and Landing Tests (ALT) program allowed pilots and engineers to learn how the Space Shuttle and the modified Boeing 747 Shuttle Carrier Aircraft (SCA) handled during low-speed flight and landing. The Enterprise, a prototype of the Space Shuttles, and the SCA were flown to conduct the approach and landing tests at the NASA Dryden Flight Research Center, Edwards, California, from February to October 1977. The first flight of the program consisted of the Space Shuttle Enterprise attached to the Shuttle Carrier Aircraft.

 

These flights were to determine how well the two vehicles flew together. Five "captive-inactive" flights were flown during this first phase in which there was no crew in the Enterprise. The next series of captive flights was flown with a flight crew of two on board the prototype Space Shuttle. Only three such flights proved necessary. This led to the free-flight test series. The free-flight phase of the ALT program allowed pilots and engineers to learn how the Space Shuttle handled in low-speed flight and landing attitudes. For these landings, the Enterprise was flown by a crew of two after it was released from the top of the SCA. The vehicle was released at altitudes ranging from 19,000 to 26,000 feet.

 

The Enterprise had no propulsion system, but its first four glides to the Rogers Dry Lake runway provided realistic, in-flight simulations of how subsequent Space Shuttles would be flown at the end of an orbital mission. The fifth approach and landing test, with the Enterprise landing on the Edwards Air Force Base concrete runway, revealed a problem with the Space Shuttle flight control system that made it susceptible to Pilot-Induced Oscillation (PIO), a potentially dangerous control problem during a landing. Further research using other NASA aircraft, especially the F-8 Digital-Fly-By-Wire aircraft, led to correction of the PIO problem before the first orbital flight. The Enterprise's last free-flight was October 26, 1977, after which it was ferried to other NASA centers for ground-based flight simulations that tested Space Shuttle systems and structure.

  

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Visit the Review of Human Space Flight Committee Web Site

The first internationally-produced F-35 Lightning II took to the skies on Sept. 7, 2015, marking the F-35 program’s first international flight. Learn more: bit.ly/1VM9rPn

A Royal Australian Air Force Lockheed Martin F-35A Lightning II "Joint Strike Fighter" taxis at Luke Air Force Base, Ariz., Dec. 3, 2018. Two F-35s were preparing to take off and fly to Hawaii as part of their multi-day journey to Australia.

 

To RAF as A 36-009

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 "Lightning II" is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the "Joint Strike Fighter" (JSF) program over the competing Boeing X-32. The official "Lightning II" name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 "Raptor", intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 "Raptor", drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E "Strike Eagle" in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 "Raptor", and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's "Super Hornet".

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

The skipjack Dee of St. Mary's is docked on Back Creek, next to the Drum Point Lighthouse, at the Calvert Marine Museum in Solomons, Md., on May 7, 2017. (Photo by Will Parson/Chesapeake Bay Program)

 

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A unicorn, not only being the emblem for an obscure (at least to me) program, but also in that it doesn’t quite match up with the other ‘more prevalent’ version of it. Maybe it’s an “oops” printing, since “Manned Spaceflight Program” (MSP?), which is not an actual/recognized term/acronym ≠ MSE. ¯\_(ツ)_/¯

 

The design is a variation of the NASA Astronaut pin/device. See forthcoming linked image below.

  

Lengthy, but interesting:

 

“Blue Shuttle: The Manned Spaceflight Engineer Program

 

The Manned Spaceflight Engineer (MSE) Program was an attempt to train American military personnel as payload specialists for Department of Defense (DoD) Space Shuttle missions. Only two of the thirty-two MSE's selected flew in space in the nine years the program was active.

 

Since its official beginning in 1969, the US Air Force (USAF) and National Reconnaissance Office (NRO) participated in the development of the Space Shuttle. The most prominent military influence on the vehicle is the size of the orbiter's payload bay. Still retaining the desire to fly all-military space missions, like with the previous decade's Man In Space, X-20 Dynamic Soarer, and Manned Orbiting Laboratory programs, the DoD wanted its own Shuttles flown by its own crews. When this so-called "Blue Shuttle" was not granted, the Air Force settled with their own astronauts hitching rides with NASA missions to handle highly classified payloads, thus beginning the MSE Program.

 

The DoD required the MSE program to consist of officers from the Army, Navy, and Air Force. Each officer would remain at NASA for four to six years during which he or she would fly at least one Space Shuttle mission before returning to their respective branch. The requirements for the first group of candidates were the following:

 

- Have at least three to ten years of service as an officer on active duty

- Hold rank from First Lieutenant to Major

- Be able to pass the NASA Class III physical exam (required for all NASA payload specialists)

- Hold a Bachelor of Science in engineering, science, or space operations

- Have a minimum of two years of experience in program acquisition or testing and launch support of flight and missile operations

 

Flight backgrounds were not required but candidates also needed appropriate security clearances to be able to work on specific classified payloads. Originally, twelve Air Force and two Navy officers were chosen but one from each branch declined. The naval officer was not replaced but the Air Force officer was replaced by Gary Payton. The thirteen MSE's were selected in 1979. All officers could anticipate flying at least once and some twice.

 

- 1st Lt. Frank Casserino, USAF

- 1st Lt. Jeffrey Detroye, USAF

- Capt. Michael Halem, USAF

- Capt. Terry Higbee, USAF

- Capt. Daryl Joseph, USAF

- Capt. Malcolm Lydon, USAF

- Capt. Gary Payton, USAF

- Capt. Jerry Rij, USAF

- Maj. Paul Sefchek, USAF

- Maj. Eric Sundberg, USAF

- Lt. Cmdr. David Vidrine, USN

- Capt. Keith Wright, USAF

- Capt. Brett Watterson, USAF

 

At the time, NASA had yet to define its own payload specialist training program so the agency was not sure how to train the new MSE's. The Air Force did not want the MSE's to go through standard NASA astronaut training because they were supposed to enter back into the service after their Shuttle flights— most military officers who became NASA astronauts never returned. When the Air Force refused to put its own astronaut candidates through general NASA training, the agency refused to provide any assistance: It was NASA's belief that since it did not select the MSE's, it did not have control over them. This led to persistent tension between NASA and the visiting MSE's. The DoD came up with its own training program, consisting of underwater EVA and manned maneuvering unit simulations at NASA Marshall and Martin Marietta [1], Shuttle mission simulations at Rockwell [2], and T-38 training at Edwards Air Force Base for those with previous flight experience. In late 1981, the first cadre of MSE's completed training.

 

The second class of MSE's, this time consisting of fourteen Air Force officers, was selected in August 1982 and began training the following May. Selection criteria were the same but did not emphasize science, engineering, and space operations backgrounds. For example, Captains James Armor and Craig Puz were commanders of Minuteman missile crews while Captain Randy Odle was a bio-environmental researcher at RAF Alconbury in the United Kingdom. This cadre included two women, 1st Lieutenant Maureen LaComb and Captain Katherine Roberts, and one African American, Captain Livingston Holder. Captain Charles Jones was killed in the September 11 hijacking in 2001 [3]. Due to the size of the MSE corps, the second class was told only half of them might fly in space.

 

- Capt. James Armor

- 1st Lt. Michael Booen

- Capt. Livingston Holder

- Capt. Larry James

- Capt. Charles Jones

- 1st Lt. Maureen LaComb

- Capt. Michael Mantz

- Capt. Randy Odle

- Capt. William Pailes

- Capt. Craig Puz

- Capt. Katherine Roberts

- Capt. Jess Sponable

- Capt. W. Davis Thompson

- Capt. Glenn Yeakel

 

MSE's Sefchek and Watterson worked on the STS-4 payload, the P-80-1 experiment package, while Casserino, Detroye, and Payton were "paycoms" (payload communicators) at the Air Force Satellite Control Facility in Sunnydale, California. In early 1982, seven MSE's were chosen as prime and backup candidates for three Shuttle missions scheduled for 1983 and '84. These flights were delayed due to issues with their payloads [4], which were developed by TRW, Hughes, Martin Marietta, and Lockheed under the direction of the NRO. Setbacks in the program reignited the decades-old debate inside the Air Force on the usefulness and feasibility of manned spaceflight. It also resulted in the DoD developing a new unmanned rocket capable of launching Shuttle payload bay-sized payloads into geosynchronous orbit, an orbit frequently occupied by military satellites. This vehicle became the Titan IV and flew from 1989 to 2005. Vidrine was a candidate for a payload specialist "observer" on STS-41-C (originally STS-13) and participated in flight simulations with commander Bob Crippen. One month before the scheduled April launch the Space Division refused to authorize Vidrine's flight because it had "no value" to the Air Force and he was removed from the crew. In late 1985 three officers from the Air Weather Service were selected for the Weather Officer in Space Experiment flight which never took place [5].

 

In late 1984, Brett Watterson was assigned as payload specialist to STS-62A, the planned first Shuttle mission from Vandenberg Air Force Base in California. Two successful DoD-dedicated Shuttle missions flew Gary Payton and William Pailes of the second class in 1985. This resulted in an additional five DoD missions scheduled for 1986 and '87 along with STS-62A and two launches of the Navstar GPS satellites. A third cadre of five more MSE's rounded out the program's astronaut corps in 1985.

 

- Capt. Joseph Caretto

- Capt. Robert Crombie

- Capt. Frank DeArmond

- Capt. David Staib

- 1st Lt. Teresa Stevens

 

After the Challenger disaster in early 1986, however, NASA was more concerned with making it safe to fly again than it was with the MSE's. Administrator James Fletcher expressed the desire to fly five-member crews and potentially eliminate the position of "payload specialist". By the end of 1987, only ten officers remained active. The Manned Spaceflight Engineer program ended in 1988 primarily due to lack of need for crewed DoD missions now that an uncrewed heavy-lift launch vehicle was available [6]. The DoD, yet again, had lost manned space capability.

 

Black and Blue: The Real DoD Shuttle Missions

 

Despite the unsuccessfulness of the Manned Spaceflight Engineer program, a total of eleven Shuttle flights flew with classified payloads and required a higher level of secrecy than regular NASA flights. Although the DoD requested the media not disclose flight details to maintain confidentiality, the press nonetheless reported whatever they could using open-source intelligence. An example of this is correlating the direction of the Shuttle after liftoff with orbital inclination— different payloads require different orbits to operate properly. Unlike with other Shuttle missions, NASA began public countdowns for DoD launches only a few minutes before liftoff, did not distribute press kits, and did not broadcast Shuttle-to-ground communications. With two exceptions, only active-duty military NASA astronauts flew these missions [7]. Below are those missions:

 

- STS-4

- STS-51C

- STS-51J

- STS-27

- STS-28

- STS-33

- STS-36

- STS-38

- STS-39

- STS-44

- STS-53

 

In 1993, after the final DoD mission flew, all crew members of classified flights were awarded the National Intelligence Achievement Medal. Some details of these missions are still classified three or four decades later.

 

California Dreamin': Vandenberg and the Space Shuttle

 

The DoD was also interested in flying polar-orbital Shuttle missions. These flights could not launch from the Kennedy Space Center in Florida because they would have flown over populated areas along the southeastern United States. Additionally, the external fuel tank would have traveled over not only Canada but Soviet Russia and possibly China. Space Launch Complex-6 (SLC-6 or "Slick Six") was constructed at Vandenberg Air Force Base (now Space Force Base) in California in the mid-1960s to support Titan III launches for the Manned Orbiting Laboratory program. It was refurbished and upgraded in the '80s for the Space Shuttle. The planned inaugural flight was to be STS-62A Discovery launching in the summer of 1986. Its primary objective was to deploy Teal Ruby, an experimental early warning satellite. The mission also would have performed a series of Earth atmospheric observations using telescopes and instruments in the orbiter's payload bay. Payload specialist no. 2 was Brett Watterson, an MSE from the first class of DoD astronauts. Due to the poor relationship between NASA astronauts and MSE's, Under Secretary of the Air Force and NRO Director Pete Aldridge was named payload specialist no. 1. After the mission was cancelled post-Challenger, STS-62A's pilot and two mission specialists (Guy Gardner, Mike Mullane, and Jerry Ross, respectively) flew STS-27 in 1988. Aldridge was promoted to Secretary of the Air Force.

 

Although STS-62-A was the only mission with a full crew planned before Californian operations ceased, two more missions were in the early planning stages. STS-62B, set to launch in late 1986 [8], would have included Kathrine Roberts as a payload specialist and would have deployed the KH-12 Advanced Kennan reconnaissance satellite. STS-82B would have deployed the Cosmic Background Explorer observatory, which later launched on a Delta rocket in 1989. Aldridge directed the Air Force to transfer all Shuttle assets from Vandenberg to the Kennedy Space Center and the Vandenberg extension of the Shuttle program was terminated on December 26, 1989. SLC-6 and its sister pads on the west coast are still active, though, and the most recent launch from SLC-6 was a Delta IV Heavy on April 26, 2021.

  

[1] Martin Marietta was responsible for the Manned Maneuvering Unit, a "jetpack" that allowed astronauts to perform untethered EVAs.

[2] Space Shuttle orbiters were assembled at Rockwell's facility in Palmdale, California.

[3] He is memorialized at the North Pool on Panel N-74 at the National 9/11 Memorial

[4] These missions are difficult to describe because they are listed by their original designations, such as STS-16. STS-16 was later designated STS-41-H. However, no mission called STS-41-H ever took place. The original STS-16 may have taken place in 1985 instead, giving it a new designation such as STS-51-[letter].

[5] I was unable to find any further information about the Weather Officer in Space Experiment but what I included in this post came from the reference with the asterisk (*)

[6] Similarly, twenty years earlier a more reliable unmanned reconnaissance satellite caused the cancellation of the Manned Orbiting Laboratory program.

[7] The exceptions are former Marine Story Musgrave and former DoD scientist Kathryn Thornton, both of whom flew on STS-33.

[8] Discovery was the only Shuttle planned to launch from SLC-6. However, it was found that turnaround time at Vandenberg was not fast enough to have STS-62B launch in 1986 so it likely would have launched in the first half of 1987.”

 

The above, slightly paraphrased, at/from:

 

www.spaceflighthistories.com/post/blue-shuttle

Credit: Aeryn Avilla/”SPACEFLIGHT HISTORIES” website

 

The above individual I believe gleaned much/most of her content from the following 1989 article written by Michael Cassutt. Click at your own risk, even though it looks (or is made to look?) like it’s no longer maintained, it’s a Godless Russian website nonetheless, so anything nefarious is possible/to be expected:

 

epizodsspace.narod.ru/bibl/spaceflight/31/mse.html

 

Multiple other sites are available regarding the MSE Program, although it’s mostly circular reporting.

 

Another view of the ‘more prevalent’ version of the emblem:

 

www.spacepatchdatabase.com/patches/space-shuttle/manned-s...

Credit: “Space Patch Database” website

 

Interesting:

 

www.losangeles.spaceforce.mil/News/Article-Display/Articl...

Credit: LOS ANGELES AIR FORCE BASE website

 

Who knew???

Did you!?!

I didn't!!!

Two Lockheed Martin F-35B "Lightning II" fighter jets have successfully landed on board HMS Queen Elizabeth for the first time, laying the foundations for the next 50 years of fixed wing aviation in support of the UK’s Carrier Strike Capability.

 

Royal Navy Commander, Nathan Gray, 41, made history by being the first to land on board HMS Queen Elizabeth, carefully maneuvering his stealth jet onto the thermal coated deck. He was followed by Squadron Leader Andy Edgell, RAF, both of whom are test pilots, operating with the Integrated Test Force (ITF) based at Naval Air Station Patuxent River, Maryland.

 

Shortly afterwards, once a deck inspection has been conducted and the all-clear given, Cmdr Gray became the first pilot to take off using the ship’s ski-ramp.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

  

The intersection of West 63rd Street and Broadway — where the Sesame Workshop offices are located — has been renamed as part of the program's 50th anniversary celebration.

 

-- CNN

PACIFIC OCEAN (Dec. 5, 2014) NASA’s Orion Crew Module descends to the Pacific Ocean under its three main parachutes as part of the Orion Program’s first exploration flight test. USS Anchorage (LPD 23) is supporting the first exploration test flight for the NASA Orion Program. EFT-1 is the fifth at sea testing of the Orion Crew Module using a Navy well deck recovery method. (U.S. Navy Photo by Mass Communication Specialist 1st Class Charles White/Released)

The Landsat Data Continuity Mission (LDCM) is a collaboration between NASA and the U.S. Geological Survey that will continue the Landsat Program's 40-year data record of monitoring Earth's landscapes from space. LDCM will expand and improve on that record with observations that advance a wide range of Earth sciences and contribute to the management of agriculture, water and forest resources.

 

The Landsat Program is a series of Earth-observing satellite missions jointly managed by NASA and the U.S. Geological Survey. The first Landsat satellite launched in 1972 and the next satellite in the series, the Landsat Data Continuity Mission – LDCM, is scheduled to launch on February 11, 2013.

 

LDCM will launch from Vandenburg Air Force Base using an Atlas V-401 rocket from ULA.

 

Credit: NASA's Goddard Space Flight Center

 

---

 

Managers have given the "go" to proceed toward a Feb.11 launch of NASA's Landsat Data Continuity Mission (LDCM) spacecraft atop a United Launch Alliance Atlas V rocket from Vandenberg Air Force Base in California.

 

The Landsat Data Continuity Mission (LDCM) is the future of Landsat satellites. It will continue to obtain valuable data and imagery to be used in agriculture, education, business, science, and government.

 

The mission will extend more than 40 years of global land observations that are critical in many areas, such as energy and water management, forest monitoring, human and environmental health, urban planning, disaster recovery and agriculture.

 

To learn more about LDCM and Landsat go to: 1.usa.gov/XSYBZ2

 

NASA image use policy.

 

NASA Goddard Space Flight Center enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission.

 

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As aviation enthusiasts from the Royal International Air Tattoo's Park & View area looked on, the F-35B performed the program's first vertical landing in the UK during validation flights for the show on July 6, 2016. bit.ly/294hI2g

Maj. Valerie Wetzbarger, 62nd Fighter Squadron Lockheed Martin F-35A Lightning II "Joint Strike Fighter" instructor pilot, stands in front an F-35 after landing, Feb. 8, 2019 at Luke Air Force Base, Ariz. In 1993 women were allowed to start fighter pilot training in the Air Force for the first time. Currently the Air Force has over 850 female pilots.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

The 2016 Chesapeake Executive Council meeting is held on Oct. 4, 2016 at the Blandy Experimental Farm in Boyce, Virginia. It was announced that Pennsylvania will have $28 million in the next year to combat agricultural pollution, with $12.7 million coming from the U.S. Department of Agriculture, $4 million from the U.S. Environmental Protection Agency and $11.8 coming mostly from shifts within the Pennsylvania budget. (Photo by Leslie Boorhem-Stephenson/Chesapeake Bay Program)

 

USAGE REQUEST INFORMATION

The Chesapeake Bay Program's photographic archive is available for media and non-commercial use at no charge.

 

To request permission, send an email briefly describing the proposed use to requests@chesapeakebay.net. Please do not attach jpegs. Instead, reference the corresponding Flickr URL of the image.

 

A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

Italy’s first F-35A Lightning II, known as AL-1 and assembled at the Cameri Final Assembly and Check Out (FACO) facility, flew for the first time on Sept. 7, 2015, marking the program’s first-ever F-35 flight outside the United States. Learn more: www.f35.com/news/detail/italys-f-35a-flies-inaugural-euro...

The Mohonk Mountain House, also known as Lake Mohonk Mountain House, is an American resort hotel located on the Shawangunk Ridge in Ulster County, New York. Its location in the town of New Paltz, New York is just beyond the southern border of the Catskill Mountains, west of the Hudson River.

 

The National Historic Landmark Program's "Statement of Significance", as of the site's historic landmark designation in 1986, stated:

 

Begun in the 1870s as a small resort for family and friends by the Smiley brothers, it became so popular that it was enlarged many times. Because of the Smileys' love of the outdoor life, the area around the hotel was treated as an integral part of the attractions of the resort. Much of this area was planned as an experiment in conservation of the natural environment, and as an educational tool for the study of botany, geology, and outdoor living.

 

The resort is located on the shore of Lake Mohonk, which is half a mile (800 m) long and 60 feet (18 m) deep. The main structure was built by Quaker twin brothers Albert and Alfred Smiley between 1869 and 1910.

 

From 1883 to 1916, annual conferences took place at Mohonk Mountain House, sponsored by Albert Smiley, to improve the living standards of Native American Indian populations. These meetings brought together government representatives of the Bureau of Indian Affairs and the House and Senate committees on Indian Affairs, as well as educators, philanthropists, and Indian leaders to discuss the formulation of policy. The Haverford College library holds 22,000 records from the 34 conference reports for researchers and students of American history.

 

The hotel hosted the Lake Mohonk Conference on International Arbitration between 1895 and 1916, which was instrumental in creating the Permanent Court of Arbitration in The Hague, Netherlands. Those conference papers were donated by the Smiley Family to Swarthmore College for research.

 

The house was given a United Nations Environment Programme Award in 1994 in honor of "125 years of stewardship". According to the National Trust for Historic Preservation, "Through its buildings and roads, its land, and its spirit, Mohonk exemplifies America's history and culture. Mohonk has since managed to maintain its 19th century character into the 21st century."

 

The resort was sued in 2014 by 200 guests who had become ill in a norovirus outbreak after staying there, who claimed the owners of the Mohonk Mountain House had been aware of the gastrointestinal illness at the resort prior to the arrival of the guests. The guests accused Mohonk of “intentional, willful, wanton, illegal ... and deliberate disregard for the health, safety and rights of plaintiffs.” The resort settled the claims for $875,000 two years later.

Description

 

Mohonk Mountain House has 259 guest rooms, including 28 tower rooms, an indoor pool and spa, and an outdoor ice-skating rink for winter use. The property consists of 1,325 acres (536 ha), and much of it is landscaped with meadows and gardens. It adjoins the Mohonk Preserve, which is crisscrossed by 85 miles (140 km) of hiking trails and carriage roads. The Smileys conveyed the majority of their property to the preserve.

 

The Mohonk Mountain House has hosted many famous visitors including industrialist John D. Rockefeller, naturalist John Burroughs, industrialist Andrew Carnegie, and American presidents Theodore Roosevelt, William Howard Taft, Rutherford B. Hayes, Chester A. Arthur, and Bill Clinton. Guests have also included former First Lady Julia Grant, author Thomas Mann, and religious leaders such as Rabbi Louis Finkelstein, Reverend Ralph W. Sockman, Reverend Francis Edward Clark. `Abdu'l-Bahá, the eldest son of Bahá'í Faith founder Bahá'u'lláh, stayed there in 1912 during the Lake Mohonk Conference on International Arbitration as part of his journeys to the West.

 

from Wikipedia

Penn Theatre Arts Fall 2015 Mainstage Production

 

Directed by Dr. James F. Schlatter.

 

The Theatre Arts Program’s fall production, BURY THE DEAD, written by Irwin Shaw in 1936, is set “in the second year of the war that is to begin tomorrow night.” The scene is an unnamed battlefield somewhere in the world that also serves as the gravesite for six dead American soldiers. About to be interred, the six young soldiers stand up in their shared grave and plead not to be buried. This crisis is the focus of Shaw’s harrowing and deeply moving and provocative play, directed by Theatre Arts faculty member, Dr. James F. Schlatter, Can a war ever end if the dead won’t be buried? The play will be performed by an ensemble company.

 

Performances:

November 18–21, 7:00pm

@ Annenberg Center Live, Bruce Montgomery Theatre

 

theatre.sas.upenn.edu/events/fall-mainstage-production-bu...

 

provost.upenn.edu/initiatives/arts/stories/2015/11/16/the...

 

Not the best of shots - glare, human, marginal angle - but one I was very lucky and glad to take! A rare opportunity to peek into the MRJ program's Flight Test Article No. 3 - or FTA-3 - during its brief four-day visit to the 2017 Paris Air Show. Flown here from the Moses Lake testing facility in Washington state, JA23MJ is very much a test airframe, and as such has no interior or fittings - but the pointy end more than makes up for it.

Two Lockheed Martin F-35A Lighting II "Joint Strike Fighter's" assigned to the 62nd Fighter Squadron, Luke Air Force Base Ariz, fly near an Arizona National Guard Boeing KC-135 Stratotanker Aug. 4, 2017. Four F-35’s participated in a missing man formation fly-over during WWII pilot 2nd Lt. Charles E. Carlson’s funeral in Pennsylvania more than 70 years after being shot down over Germany in World War II when he was assigned to the 62 FS.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

On Sept. 20, 1979, the Marshall Space Flight Center’s third and final High Energy Astronomy Observatory (HEAO-C) was launched from Kennedy Space Center aboard an Atlas-Centaur vehicle. Known as HEAO-3 after its insertion into orbit, HEAO-C continued the program’s mission of probing the electromagnetic spectrum beyond the X-ray level, discovering a multitude of gamma and cosmic rays. Utilizing a gamma-ray spectrometer, a cosmic-ray isotope experiment, and a heavy cosmic-ray nuclei experiment to bring images of supernova remnants, pulsars, and distant galaxies into focus, the three HEAO missions propelled forward the then emerging field of high energy astrophysics. The HEAO-3 project was managed by Marshall Space Flight Center in Huntsville, Ala., with TRW, Inc. serving as the primary contractor.

 

Image credit: NASA/MSFC

 

Original image: www.nasa.gov/centers/marshall/history/gallery/launch-of-h...

 

More Marshall history images:

www.nasa.gov/centers/marshall/history/gallery/marshall_hi...

  

_____________________________________________

These official NASA photographs are being made available for publication by news organizations and/or for personal use printing by the subject(s) of the photographs. The photographs may not be used in materials, advertisements, products, or promotions that in any way suggest approval or endorsement by NASA. All Images used must be credited. For information on usage rights please visit: www.nasa.gov/audience/formedia/features/MP_Photo_Guidelin...

On my London study abroad program's weekend trip to Paris, my flatmates and I discovered the song "Grace Kelly" by MIKA on French television. At first we thought him silly, crazy, and very bizarre, but we loved him! He made us laugh! So we've gotten home to London and discovered his new CD in Sainsbury's grocery. Of course we bought it and have been playing it every 5 minutes and dancing around our flat. I appreciate his love of color and life.

 

EXPLORE #92

Dan Small of Washington College and landowner Harry Sears use a controlled fire to manage part of a warm season grassland at Chino Farms in Queen Anne's County, Md., on April 13, 2016. The grassland is ideal habitat for northern bobwhite quail. (Photo by Will Parson/Chesapeake Bay Program)

 

USAGE REQUEST INFORMATION

The Chesapeake Bay Program's photographic archive is available for media and non-commercial use at no charge. To request permission, send an email briefly describing the proposed use to requests@chesapeakebay.net. Please do not attach jpegs. Instead, reference the corresponding Flickr URL of the image.

 

A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

Two Lockheed Martin F-35B Lightning II fighter jets have successfully landed on board HMS Queen Elizabeth for the first time, laying the foundations for the next 50 years of fixed wing aviation in support of the UK’s Carrier Strike Capability.

 

Royal Navy Commander, Nathan Gray, 41, made history by being the first to land on board HMS Queen Elizabeth, carefully maneuvering his stealth jet onto the thermal coated deck. He was followed by Royal Navy Squadron Leader Andy Edgell, RAF, both of whom are test pilots, operating with the Integrated Test Force (ITF) based at Naval Air Station Patuxent River, Maryland.

 

Shortly afterwards, once a deck inspection has been conducted and the all-clear given, Cmdr Gray became the first pilot to take off using the ship’s ski-ramp.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

Royal Navy Commander Nathan Gray RN, gives the thumbs up after making the first ever Lockheed Martin F-35B Lightning II fighter jet vertical landing on board HMS Queen Elizabeth.

 

Two Lockheed Martin F-35B Lightning II fighter jets have successfully landed on board HMS Queen Elizabeth for the first time, laying the foundations for the next 50 years of fixed wing aviation in support of the UK’s Carrier Strike Capability.

 

Royal Navy Commander, Nathan Gray, 41, made history by being the first to land on board HMS Queen Elizabeth, carefully maneuvering his stealth jet onto the thermal coated deck. He was followed by Squadron Leader Andy Edgell, RAF, both of whom are test pilots, operating with the Integrated Test Force (ITF) based at Naval Air Station Patuxent River, Maryland.

 

Shortly afterwards, once a deck inspection has been conducted and the all-clear given, Cmdr Gray became the first pilot to take off using the ship’s ski-ramp.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

  

U.S. Senator Martin Heinrich tours the ¡YouthWorks! facility in Santa Fe and highlights the program's recognition as a Bright Spot in Hispanic Education by the White House. ¡YouthWorks! is a non-profit, community-based organization that provides opportunities to work on AmeriCorps projects, education, job training, counseling, and leadership development for young adults.

Maryland Park Ranger Jeremiah Corbin uses a hot poker to drill a hole in a piece of staghorn sumac to make a maple syrup spout, or stile, during the 46th Annual Maple Syrup Festival at Cunningham Falls State Park in Thurmont, Md., on March 20, 2016. (Photo by Will Parson/Chesapeake Bay Program)

 

USAGE REQUEST INFORMATION

The Chesapeake Bay Program's photographic archive is available for media and non-commercial use at no charge. To request permission, send an email briefly describing the proposed use to requests@chesapeakebay.net. Please do not attach jpegs. Instead, reference the corresponding Flickr URL of the image.

 

A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

Spartan Stadium (formerly College Field, Macklin Field and Macklin Stadium) opened in 1923 in East Lansing, Michigan, United States. It is primarily used for football, and is the home field of the Michigan State University Spartans. After the addition of luxury boxes and club seating in 2004–2005, the capacity of the stadium grew from 72,027 to 75,005—though it has held more than 80,000 fans—making it the Big Ten's sixth largest stadium.

 

In the early 1920s, school officials decided to construct a new stadium to replace Old College Field. The resulting stadium—the lower half of the current stadium—was ready in the fall of 1923 with a capacity of 14,000. Over the years, the stadium grew. In 1935, the seating capacity increased to 26,000 and the facility was dedicated as Macklin Field. John Macklin, football coach from 1911 to 1915, put Michigan State football on the map with a 29–5 record over five seasons with victories over big name programs such as Michigan, Notre Dame, Ohio State, Penn State, and Wisconsin. After admittance into the Big Ten in 1948, Michigan State increased stadium capacity to 51,000 and the field was renamed Macklin Stadium. With Spartan football attracting national attention under Clarence "Biggie" Munn and Hugh "Duffy" Daugherty, 9,000 seats were added in 1956. The following season upper decks were added to the east and west sides boosting the capacity to 76,000. That same season Michigan State dropped the name Macklin Stadium in favor of Spartan Stadium.

 

In 1969, TartanTurf replaced the natural grass field and a modern scoreboard was added in 1973. Later in the 1970s, AstroTurf replaced the TartanTurf. A new modern video scoreboard was added before the 1991 season. Renovations improving sight lines, field security, handicap access, and club seats in 1994 reduced Spartan Stadium's capacity to 72,027. New turf was also installed in the summer of 1994. In 1998, Spartan Stadium's sound system was upgraded, adding a 21' x 27' Mitsubishi Diamond Vision video board to the south end and a message board to the north end. Home to one of the top turfgrass research programs in the nation, Michigan State installed a natural grass field in 2002. The most recent expansion was completed in August 2005. A new press box, 24 luxury suites, and 862 club seats were constructed on the west side of Spartan Stadium. This addition made Spartan Stadium the tallest building in East Lansing.

 

Through the 2012 season until their game against Notre Dame, the Spartans had won 15 straight games in Spartan Stadium—the program's longest home streak since winning 19 straight from 1950-53. Michigan State went undefeated at home in back-to-back seasons (2010 and 2011) including marquee wins over Wisconsin, Michigan, and Notre Dame, marking the first consecutive perfect home seasons since 1955-56.

 

For almost 9 years, the stadium held the world record for the largest ice hockey crowd in history. On October 6, 2001, a rink was constructed at the center of the stadium for Michigan State's season-opening game against archrival Michigan.

 

Dubbed "The Cold War", 74,554 watched No. 1 nationally ranked Michigan State and No. 4 nationally ranked Michigan to a 3–3 tie. Country artist Shannon Brown sang during the second intermission. The game set off a wave of outdoor ice hockey games in large stadiums. The record for the highest-attended outdoor hockey game is now held by the University of Michigan where 104,173 came to Michigan Stadium to watch Michigan beat Michigan State 5-0 in The Big Chill at the Big House.

 

Game days at Spartan Stadium provide opportunity for tailgating. Popular locations include the tennis courts, "the rock", and around the MSU library area on north campus. Open alcohol is permitted on campus during tailgating hours, with the exception of Munn field.

 

On the morning of each home game, the team completes a 10-minute walk from their hotel at the Kellogg Center, crossing the Red Cedar River, passing the Spartan Statue and finally into the stadium. The sidewalks are lined with fans applauding and cheering "Go Green, Go White."

 

"It's a beautiful day for football!" – Just before kickoff, the PA announcer gives the weather forecast and, with the help of the fans, declares that "it's a beautiful day for football!" This tradition takes place even during games played in poor weather.

 

Introduced in 2007, clips from the movie 300 were added to the "Thunderstruck" introduction sequence. A clip of Spartan King Leonidas shouting, "Spartans! What is your profession?" is played whenever the opponent is in a third down situation. The crowd responds with an emphatic "Ha-Ooh! Ha-Ooh! Ha-Ooh!" while thrusting their fists in the air as if they were carrying spears like in the movie. This is very popular with the football team. On October 16, 2010, 300 star Gerard Butler attended the Spartans' homecoming game. At the beginning of the game Butler walked onto the field repeating the familiar call to fans.

 

en.wikipedia.org/wiki/Spartan_Stadium_(East_Lansing%2C_Michigan)

 

en.wikipedia.org/wiki/Wikipedia:Text_of_Creative_Commons_...

 

the Cheese Fairy in Downtown Baker City. Sharing a storefront with Copperbelt Winery, the Cheese Fairy is one of the newest businesses to open in downtown baker City as part of the growing arts and culinary scene in this small Eastern Oregon town.

 

Visitors to downtown will also find numerous local restaurants featuring locally sourced cuisine and several local culinary makers including a local brewery, distillery and of course Copperbelt winery. In addition to the emerging culinary scene, there are also a variety of art galleries throughout Baker City’s historic downtown including the Crossroads Carnegie Art center in the restored Carnegie Library building.

 

For more information about downtown Baker City visit the local Main Street program's website www.bakercitydowntown.com or the Baker County Tourism website at www.basecampbaker.com

   

IMAGE VIEW INFORMATION

- The photographer's viewpoint is looking south from the access pathway that led back to Como Station.

- Note the stylized establishment date of "1890" on the facing roof facade (this reflects the year in Queen Victoria's reign when it was first Licensed as an Hotel).

- This image is very similar in point of view & date of capture as the previous image, which was taken by a different photographic business (the Star Photo Co).

*******************************

SOURCE INFO

- The original digitized photo-print is archived by the National Library of Australia in their William Robert Easdown photographic collection nla.gov.au/nla.obj-148979938/view.

- This digital copy was downloaded, restored & repaired by myself, using Adobe Photoshop Creative Suite 8.0 (with duo-tone enhancement) for public share & review via Flickr.

********************************

CREDIT INFO

Credits go to -

(a) Robert Easdown Collection for the original image, &

(b) The National Library of Australia for their valuable historic photograph digitization & archiving program(s).

********************************

COPYRIGHT STATUS

- Original image is no longer restricted by any form of Copyright, per NLA copyright advice -

Out of Copyright

Reason for copyright status: Created/Published Date is Before 1955

Copyright status was determined using the following information:

Material type: Photograph

Published status: Unpublished

Government copyright ownership: No Government Copyright Ownership

"The National Library of Australia supports creativity, innovation and knowledge-exchange but does not endorse any inappropriate or derogatory use. Please respect indigenous cultural and ethical concerns".

- As for my own work in creating this enlarged & substantially restored sepia version of the original image, I have applied Creative Commons "Attribution-NonCommercial-ShareAlike".

**************************************

HISTORIC INFORMATION

- Construction timeline - 2nd Version

17 Dec 1889 - Multiple Tenders are invited by building contractor R. Fielding for "carting building materials from Como siding, Illawarra line, to back of Como Station", "Quarrying a large quantitiy of Stone, at Como, near station, Illawarra line" & "for 160,000 Bricks, delivered Como station, Illawarra line".

12 Feb 1890 - Multiple Tenders are invited by building contractor Robert Fielding for "Plumbing of large Hotel at Como Station", "Plastering, &c., of large Hotel at Como Station" & "for a large quantity of Iron Columns, Balcony Railings, Ornamental Castings, &c., for large Hotel, Como".

17 Oct 1890 - A Conditional Publican's license is granted to George Agnew "for premises at Como"

- More detail about the history of the Como Hotel can be found here en.wikipedia.org/wiki/Como,_New_South_Wales

A Lockheed Martin F-35A Lightning II "Joint Strike Fighter" is inspected before for take-off at Luke Air Force Base, Ariz., Feb. 1, 2018. This year was the first time the F-35 participated in the Haboob Havoc, a fighter pilot competition, hosted by Thunderbolts.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 "Lightning II" is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the "Joint Strike Fighter" (JSF) program over the competing Boeing X-32. The official "Lightning II" name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 "Raptor", drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E "Strike Eagle" in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 "Raptor", and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

Located at the end of a sleepy little cul-de-sac in the leafy north east Melburnian suburb of Fairy Hills is a beautiful pebbledash Arts and Crafts style bungalow. Quiet and unassuming amid its well kept gardens, this bungalow is quite significant historically as it is the creation and home of nationally renowned husband and wife artists Christian and Napier Waller, and is known as the Waller House. Together they designed the house and much of its interior decoration and furnishings. Napier Waller lived in their purpose designed home for some fifty years. What is especially significant about the house is that both it and its contents are quite intact. Napier Waller's studios, examples of his art, that of his two wives and his niece, famous studio potter Klytie Pate, and items connected with his work remain exactly as he left them. Architecturally the house design is innovative in its internal use of space, specifically in the organisation of the studio cum living room and displays a high degree of artistic creativity in the interior decoration.

 

The Waller House in Fairy Hills is so named because it was the residence of Mervyn Napier Waller, the acclaimed artist who gained National fame from his water colours, stained glass, mosaic works and murals and his wife Christian, who was a distinguished artist and designer of stained glass in her own right. In particular Napier Waller's works adorn the Melbourne Town Hall, the Myer Emporium Mural Hall, the Victorian State Library and the Australian War Memorial. The Waller House is a split level house designed by Napier and his first wife Christian who intended the house to be both a home and a workplace. For this the design was conceived to accommodate the tall studies and pieces of the artist's work.

 

The Waller house was built by Phillip Millsom in 1922 and the architectural style of the house is a mixture of Interwar Arts and Crafts, Interwar Old English and Interwar California Bungalow. The house is constructed from reinforced concrete walls with a rough cast pebbledash finish. The roof is steeply pitched with a prominent half timbered gable over the front entrance and has Marseilles pattern terracotta tiles. There are small paned casement windows. There have been several additions to the original design over the years but these have all been sympathetic to the original design.

 

The house is entered from a two sided verandah into an entrance hall, panelled in Tasmanian wood. This has stairs leading to the different levels of the house interior. In one direction the hall leads to a main living hall which was Napier Waller's original studio and later used as the main living room in the house. This room has a high ceiling with casement windows, a musicians’ gallery and a broad brick fireplace flanked by fire-dogs and bellows made by the sculptress Ola Cohn (1892 – 1964). Like many of the other rooms in the house the studio is panelled and floored with Tasmanian hardwood and contains some of the studies for Napier Waller's murals: “The Five Lamps of Learning; the Wise and Foolish Virgins” a mosaic for the University of Western Australia and, “Peace After Victory” a study painting for the State Library of Victoria. Above the panelling the plaster walls are painted in muted colours in wood grain effect. The raftered plaster ceiling has been painted in marble effect with gold leaf. Book shelves, still containing the Wallers’ beautiful books, are built into the panelled walls. Furniture in the room includes a settee with a painted back panel featuring jousting knights, painted by Christian Waller, a leather suite and black bean sideboards and cupboards. This furniture was designed in the nineteen thirties by Napier Waller and by Percy Meldrum and a noted cabinet maker called Goulman. The studio cum hall also contains many ceramic works created by studio potter Klytie Pate who was Christian Waller’s niece and protégée. The entrance hall leads in the other direction to a guest room, known as the “Blue Room”. This was the idea of Napier's wife Christian and has simple built-in glass topped furniture and Napier's murals of the “Labours of Hercules” which include a self portrait of the artist. An alcove section of the room was constructed out of an extension to the verandah. Stairs lead from the entrance hall to the musicians’ gallery which has a window and overlooks the studio cum living room. The kitchen near the studio/hall is panelled and raftered with built-in cupboards conforming to the panelling. The ceiling is stencilled in a fleur-de-lys design by Napier. The dining room lies to the right of the studio cum hall and contains shoulder high panelling and raftered ceilings. It has an angled brick corner fireplace and the walls and ceiling have the same painted treatment as the studio cum living room. The oak dining furniture was designed by Napier. A small den with high window, furnished with leather chairs, opens off the dining room. Opening off the hall to the left is a long rectangular room known as the glass studio. This was added to the house by builder C. Trinck of Hampton in about 1931 and contains Napier Waller's kiln, paintbrushes and stained-glass tools on the benches, and stained glass designs and racks which are still stacked with radiant streaked glass from his work with stained glass windows. A bedroom and bathroom with attic pitched rafter ceiling and casement windows is situated on the upper level of the house. Another bedroom in ship's cabin style with flared wall light fittings and built in bunks opens off this first bedroom.

 

The house backs onto a courtyard enclosed by a long bluestone garden wall. The house is set in a three and a half acre site with cypress hedges and gravelled paths. The garden drops away to a hillside slope with manna gum trees. Set on the slope is a flat roofed studio built in 1937. It has an undercroft beneath a studio room and this contains a lithographic press and a printing press of 1849 for woodcuts and linocuts. This was used by Napier and his first wife Christian to produce prints in the 1930s. Napier was widowed and married his stained glass studio assistant Lorna Reyburn in 1958.

 

The Waller House has recently become famous for yet another reason. The exterior has been used as a backdrop in the ABC/ITV co-production television series, “The Doctor Blake Mysteries” (2013). The house serves as the residence of the program’s lead character, Doctor Lucien Blake (played by Australian actor Craig McLachlan), and the doctor’s 1930s tourer is often seen driving up to or away from the Waller House throughout the series. The Waller House is the only regular backdrop not filmed in the provincial Victorian gold rush city of Ballarat, in which the series is based.

 

The Waller House is still a private residence, even though it was bequeathed to the people of Victoria by Napier Waller under the proviso that it would not revert to state ownership until after the death of his second wife, Lorna. The current leasee of the Waller House is a well known Melbourne antique dealer, who was friends with Lorna Reyburn, and who acts as a loving informal caretaker. He was approached by the Napier Waller Committee of Management and keeps the house neat and tidy, and maintains the garden beautifully. I am very grateful to him for his willingness to open the Waller House, and for allowing me the opportunity to comprehensively photograph this rarely seen gem of Melbourne art, architecture and history.

 

Mervyn Napier Waller (1893 – 1972) was an Australian artist. Born in Penshurst, Victoria, Napier was the son of William Waller, contractor, and his wife Sarah, née Napier. Educated locally until aged 14, he then worked on his father's farm. In 1913 he began studies at the National Gallery schools, Melbourne, and first exhibited water-colours and drawings at the Victorian Artists' Society in 1915. On 31 August of that year he enlisted in the Australian Imperial Force, and on 21 October at the manse of St Andrew's Presbyterian Church, Carlton, married Christian Yandell, a fellow student and artist from Castlemaine. Serving in France from the end of 1916, Waller was seriously wounded in action, and his right arm had to be amputated at the shoulder. Whilst convalescing in France and England Napier learned to write and draw with his left hand. After coming home to Australia he exhibited a series of war sketches in Melbourne, Sydney, Adelaide and Hobart between 1918 and 1919 which helped to establish his reputation as a talented artist. Napier continued to paint in water-colour, taking his subjects from mythology and classical legend, but exhibited a group of linocuts in 1923. In 1927 Napier completed his first major mural for the Menzies Hotel, Melbourne. Next year his mural 'Peace after Victory' was installed in the State Library of Victoria. Visiting England and Europe in 1929 to study stained glass, the Wallers travelled in Italy where Napier was deeply impressed by the mosaics in Ravenna and studied mosaic in Venice. He returned to Melbourne in March 1930 and began to work almost exclusively in stained glass and mosaic. In 1931 he completed a great monumental mosaic for the University of Western Australia; two important commissions in Melbourne followed: the mosaic façade for Newspaper House (completed 1933) and murals for the dining hall in the Myer Emporium (completed 1935). During this time he also worked on a number of stained-glass commissions, some in collaboration with his wife, Christian. Between 1939 and 1945 he worked as an illustrator and undertook no major commissions. In 1946 he finished a three-lancet window commemorating the New Guinea martyrs for St Peter's Church, Eastern Hill. In 1952-58 he designed and completed the mosaics and stained glass for the Hall of Memory at the Australian War Memorial, Canberra. On 25 January 1958 in a civil ceremony in Melbourne Waller had married Lorna Marion Reyburn, a New Zealand-born artist who had long been his assistant in stained glass.

 

Christian Waller (1894 – 1954) was an Australian artist. Born in Castlemaine, Victoria, Christian was the fifth daughter and youngest of seven children of William Edward Yandell a Victorian-born plasterer, and his wife Emily, née James, who came from England. Christian began her art studies in 1905 under Carl Steiner at the Castlemaine School of Mines. The family moved in 1910 to Melbourne where Christian attended the National Gallery schools. She studied under Frederick McCubbin and Bernard Hall, won several student prizes, exhibited (1913-22) with the Victorian Artists Society and illustrated publications. On 21 October 1915 at the manse of St Andrew's Presbyterian Church, Carlton, she married her former fellow-student Mervyn Napier Waller; they were childless, but adopted Christian’s niece Klytie Pate, in all but a legal sense. During the 1920s Christian Waller became a leading book illustrator, winning acclaim as the first Australian artist to illustrate Alice in Wonderland (1924). Her work reflected Classical, Medieval, Pre-Raphaelite and Art Nouveau influences. She also produced woodcuts and linocuts, including fine bookplates. From about 1928 she designed stained-glass windows. The Wallers travelled to London in 1929 to investigate the manufacture of stained glass at Whall & Whall Ltd's premises. Returning to Australia via Italy, they studied the mosaics at Ravenna and Venice. Christian signed and exhibited her work under her maiden name until 1930, but thereafter used her married name. In the 1930s Waller produced her finest prints, book designs and stained glass, her work being more Art Deco in style and showing her interest in theosophy. She created stained-glass windows for a number of churches—especially for those designed by Louis Williams—in Melbourne, Geelong, and rural centres in New South Wales. Sometimes she collaborated with her husband, both being recognized as among Australia's leading stained-glass artists. Estranged from Napier, Christian went to New York in 1939. In 1940 she returned to the home she shared with her husband in Fairy Hills where she immersed herself in her work and became increasingly reclusive. In 1942 she painted a large mural for Christ Church, Geelong; by 1948 she had completed more than fifty stained-glass windows.

 

Klytie Pate (1912 – 2010) was an Australian Studio Potter who emerged as an innovator in the use of unusual glazes and the extensive incising, piercing and ornamentation of earthenware pottery. She was one of a small group of Melbourne art potters which included Marguerite Mahood and Reg Preston who were pioneers in the 1930‘s of ceramic art nationwide. Her early work was strongly influenced by her aunt, the artist and printmaker, Christian Waller. Klytie’s father remarried when she was 13, so Klytie went to live with her aunt, Christian Waller. Christian and her husband Napier Waller encouraged her interest in art and printmaking. She spent time at their studio in Fairy Hills, and thus her work reflected Art Deco, Art Nouveau, the Pre Raphaelites, Egyptian art, Greek mythology, and Theosophy. Klytie made several plaster masks that were displayed by the Wallers in their home and experimented with linocut, a medium used by Christian in her printmaking. Her aunt further encouraged Klytie by arranging for her to study modelling under Ola Cohn, the Melbourne sculptor. Klytie became renowned for her high quality, geometric Art Deco designed pottery which is eagerly sought after today by museums, art galleries, collectors and auction houses.

 

Fairy Hills is a small north eastern suburb of Melbourne. Leafy, with streets lined with banks of agapanthus, it is an area well known for its exclusivity, affluence and artistic connections. It was designed along the lines of London’s garden suburbs, such as Hampstead and Highgate, where houses and gardens blended together to create an informal, village like feel. Many of Fairy Hills’ houses have been designed by well known architects of the early Twentieth Century such as Walter Burley Griffin (1876 – 1937) and have gardens landscaped by designers like Edna Walling (1895 – 1973). Fairy Hills is the result of a subdivision of an 1840s farm called “Fairy Hills” which was commenced in the years just before the First World War (1914 – 1918). “Lucerne Farm”, a late 1830s farm associated with Governor La Trobe, was also nearby.

  

This program's prediction was correct, as I consulted it prior to the shot. The Monterra compass was off 1 degree at the time of the shot!

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather stealth multirole fighters. The fifth-generation combat aircraft is designed to perform ground attack and air defense missions. It has three main models: the F-35A conventional takeoff and landing (CTOL) variant, the F-35B short take-off and vertical-landing (STOVL) variant, and the F-35C carrier-based Catapult Assisted Take-Off But Arrested Recovery (CATOBAR) variant. On 31 July 2015, the United States Marines declared ready for deployment the first squadron of F-35B fighters after intensive testing. On 2 August 2016, the U.S. Air Force declared its first squadron of F-35A fighters combat-ready.

 

The F-35 descends from the X-35, the winning design of the Joint Strike Fighter (JSF) program. An aerospace industry team led by Lockheed Martin designed and manufactures it. Other major F-35 industry partners include Northrop Grumman, Pratt & Whitney and BAE Systems. The F-35 first flew on 15 December 2006. The United States plans to buy 2,663 aircraft. Its variants are to provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy and the Marine Corps over the coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

The United States principally funds the F-35 JSF development, with additional funding from partners. The partner nations are either NATO members or close U.S. allies. The United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and Turkey are part of the active development program; several additional countries have ordered, or are considering ordering, the F-35.

 

The program is the most expensive military weapons system in history, and has been much criticized inside and outside government, in the U.S. and in allied countries. Critics argue that the plane is "plagued with design flaws," with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time, instead of identifying and fixing defects before firing up its production line." By 2014, the program was "$163 billion over budget and seven years behind schedule." Critics also contend that the program's high sunk costs and political momentum make it "too big to kill."

 

The aircraft here was displaying at the 2016 Farnborough International Airshow which is a week-long event that combines a major trade exhibition for the aerospace and defence industries with a public airshow. The event is held in mid-July in even-numbered years at Farnborough Airport in Hampshire, United Kingdom. The first four days (Monday to Thursday) are dedicated exclusively to trade, with the final three days open to the public.

 

The airshow is an important event in the international aerospace and defence industry calendar, providing an opportunity to demonstrate civilian and military aircraft to potential customers and investors. The show is also used for the announcement of new developments and orders, and to attract media coverage. It is one of the largest air shows, after France's Salon du Bourget.

 

The UK show is organised by Farnborough International Limited, a wholly owned subsidiary of ADS Group Limited (ADS). According to the organisers, the 2012 Farnborough show attracted 109,000 trade visitors over the first five days, and 100,000 public visitors during the weekend. Orders and commitments for 758 aircraft were announced, worth US$72 billion.

 

en.wikipedia.org/wiki/Lockheed_Martin_F-35_Lightning_II

 

en.wikipedia.org/wiki/Farnborough_Airshow

Third Thursday Wine Walk in Downtown Baker City Oregon

 

Enjoying beautiful evening for Third Thursday in historic downtown Baker City, Oregon.

 

The monthly Third Thursday Wine Walk is one of numerous events hosted by the Baker City Main Street Program, Baker City Downtown giving customers an opportunity to visit and explore downtown after hours.

 

Visitors to downtown will find numerous art galleries throughout Baker City’s historic downtown including the Crossroads Carnegie Art center in the restored Carnegie Library building as well as multiple restaurants and a variety of gourmet and artisan food and spirits.

 

For more information about Third Thursday Wine Walk or other downtown Baker City events visit the Baker City Main Street Program's website at www.bakercitydowntown.com

 

For more information about other community events in Baker County visit the Baker County Tourism website at www.travelbakercounty.com

  

The Nature Conservancy hosts a group of roughly 30 visitors for a vernal pool hike at Forest Pools Preserve, adjacent to Kings Gap State Park in Cumberland County, Pa., on March 25, 2016. Because vernal pools, or seasonal wetlands, dry up every year, they don't harbor fish and thus are critical habitat for many amphibian species. (Photo by Will Parson/Chesapeake Bay Program)

 

USAGE REQUEST INFORMATION

The Chesapeake Bay Program's photographic archive is available for media and non-commercial use at no charge. To request permission, send an email briefly describing the proposed use to requests@chesapeakebay.net. Please do not attach jpegs. Instead, reference the corresponding Flickr URL of the image.

 

A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

Downtown Baltimore is seen facing west toward the Inner Harbor from Dundalk, Md., on June 27, 2016. (Photo by Will Parson/Chesapeake Bay Program with aerial support by LightHawk)

 

USAGE REQUEST INFORMATION

The Chesapeake Bay Program's photographic archive is available for media and non-commercial use at no charge. To request permission, send an email briefly describing the proposed use to requests@chesapeakebay.net. Please do not attach jpegs. Instead, reference the corresponding Flickr URL of the image.

 

A photo credit mentioning the Chesapeake Bay Program is mandatory. The photograph may not be manipulated in any way or used in any way that suggests approval or endorsement of the Chesapeake Bay Program. Requestors should also respect the publicity rights of individuals photographed, and seek their consent if necessary.

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