+++ 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.

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.

WEEK 41 – Southaven Malco (Feature Presentation)

For this next portion of our album, we’ll be exploring the auditorium wings. Not either the left one or the right one specifically, I should say, but simply “the rest of the theater” in general; which is a good thing, actually, as I have absolutely no idea which wing I was walking down when I took this picture anyway XD

Regardless, my intention here was to show you the old changeable letterboards that Malco used to use to manually put up the movie names, show times, and auditorium locations, prior to replacing them with computerized versions. In the wake of the new automated signboards being installed, these old ones were downgraded merely to advertising a permanent “welcome” message; later, they were removed entirely.

As for the new movie screen signage, you can see the first iteration in this pic, which also shows you the spatial relationship between the new and the old (not to mention a very nice overview of the entire lobby). Since then, the signs have been replaced yet again; we saw those newest versions above both auditorium wings during Tuesday’s upload set.

(c) 2020 Retail Retell

These places are public so these photos are too, but just as I tell where they came from, I'd appreciate if you'd say who :)

Pinwheel Galaxy (M101)

Located in the Ursa Major Constellation, this galaxy is about 21 million light years away from us. If you look closely you will see about 1/2 dozen other galaxies in this photo. The galaxy to the lower right of the Pinwheel, is NGC 5474. It is distorted because of gravitational pull from the Pinwheel.

Last night the wind finally settled down a bit and the skies cleared. This photo is a compilation of 96, three minute exposures for a total of 5 hours of integration.

Still using my Nikon 600mm f4e wildlife lens with a dedicated CMOS astro camera and a computerized equatorial mount. Waiting for my new scope being built in Auburn, Ca. Hopefully will be ready next month.

Photographed 21 million years later from the Alexander Valley, Sonoma County, Calif.

March 23, 2021

Southeast Financial Center is a two-acre development in Miami, Florida, United States. It consists of a 764 feet (233 m) tall office skyscraper and its 15-story parking garage. It was previously known as the Southeast Financial Center (1984–1992), the First Union Financial Center (1992–2003), and the Wachovia Financial Center (2003-2011). In 2011, it retook its old name of Southeast Financial Center as Wachovia merged with Wells Fargo and moved to the nearby Wells Fargo Center.

When topped-off in August 1983, it was the tallest building south of New York City and east of the Mississippi River, taking away the same title from the Westin Peachtree Plaza Hotel, in Atlanta, Georgia. It remained the tallest building in the southeastern U.S. until 1987, when it was surpassed by One Atlantic Center in Atlanta and the tallest in Florida until October 1, 2003, when it was surpassed by the Four Seasons Hotel and Tower, also in Miami. It remains the tallest office tower in Florida and the third tallest building in Miami.

Southeast Financial Center was constructed in three years with more than 500 construction workers. Approximately 6,650 tons of structural steel, 80,000 cubic yards of concrete and 7000 cubic tons of reinforcing steel bars went into its construction. The complex sits on a series of reinforced concrete grade beams tied to 150 concrete caissons as much as ten feet in diameter and to a depth of 80 feet. A steel space-frame canopy with glass skylights covers the outdoor plaza between the tower and low-rise building.

The tower has a composite structure. The exterior columns and beams are concrete encased steel wide flanges surrounded by reinforcing bars. The composite exterior frame was formed using hydraulic steel forms, or "flying forms," jacked into place with a "kangaroo" crane, that was located in the core and manually clamped into place. Wide flange beams topped by a metal deck and concrete form the interior floor framing. The core is A braced steel frame, designed to laterally resist wind loads. The construction of one typical floor was completed every five days.

The low-rise banking hall and parking building is a concrete-framed structure. Each floor consists of nearly an acre of continuously poured concrete. When the concrete had sufficiently hardened, compressed air was used to blow the forms fiberglass forms from under the completed floor. It was then rolled out to the exterior where it was raised by crane into position for the next floor.

The building was recognized as Miami's first and only office building to be certified for the LEED Gold award in January 2010.

The center was developed by a partnership consisting of Gerald D. Hines Interests, Southeast Bank and Corporate Property Investors for $180 million. It was originally built as the headquarters for Southeast Bank, which originally occupied 50 percent of the complex's space. It remained Southeast Bank's headquarters there until it was liquidated in 1991.

The Southeast Financial Center comprises two buildings: the 55-story office tower and the 15-story parking annex. The tower has 53 stories of office space. The first floor is dedicated for retail, the second floor is the lobby and the 55th floor was home to the luxurious Miami City Club. The parking annex has 12 floors of parking space for 1,150 cars. The first floor is dedicated for retail, the second floor is a banking hall and the 15th floor has the Downtown Athletic Club. A landscaped plaza lies between the office tower and the parking annex. An enclosed walkway connects the second story of the tower with the second story of the annex. The courtyard is partially protected from the elements by a steel and glass space frame canopy spanning the plaza and attached to the tower and annex. Southeast Bank's executive offices were located on the 38th floor. Ground was broken on the complex on December 12, 1981 and the official dedication and opening for the complex was held on October 23, 1984.

The Southeast Financial Center was designed by Edward Charles Bassett of Skidmore, Owings and Merrill. The Associate Architect was Spillis Candela & Partners. It has 1,145,311 ft² (106,000 m²) of office space. A typical floor has about 22,000 ft² (2,043.87 m²) of office space. Each floor has 9 ft x 9 ft (2.7 m x 2.7 m) floor to ceiling windows. (All of the building's windows are tinted except for the top floor, resulting in strikingly bright and clear views from there.) The total complex has over 2.2 million ft² (204,000 m²). The distinctive setbacks begin at the 43rd floor. Each typical floor plate has 9 corner offices and the top twelve floors have as many as 16. There are 43 elevators in the office tower. An emergency control station provides computerized monitoring for the entire complex, and four generators for backup power.

The Southeast Financial Center can be seen as far away as Ft. Lauderdale and halfway toward Bimini. Night space shuttle launches from Cape Canaveral 200 miles to the north were plainly visible from the higher floors. The roof of the building was featured in the Wesley Snipes motion picture Drop Zone, where an eccentric base jumper named Swoop parachutes down to the street from a suspended window cleaning trolley. The building also appeared in several episodes of the 1980s TV show Miami Vice and at the end of each episode's opening credits.

Zara founder Amancio Ortega purchased the building from J.P. Morgan Asset Management in December 2016. The purchase price was reportedly over $500 million, making it one of the largest real estate transactions in South Florida history.

Credit for the data above is given to the following websites:

en.wikipedia.org/wiki/Southeast_Financial_Center

www.emporis.com/buildings/122292/wachovia-financial-cente...

© All Rights Reserved - you may not use this image in any form without my prior permission.

I almost got mugged soon after.

A Lockheed Martin F-35A-2B "Lightning II" "Joint Strike Fighter" (s/n 12-5056) (MSN AF067) flies alongside a General Dynamics (its aviation unit now part of Lockheed Martin) F-16C Block 42A "Fighting Falcon" (s/n 87-0360) June 25, 2015, at Luke Air Force Base. In October, F-35 and F-16 pilots began integrated training designed to improve mission cooperation and flight skills in both airframes.

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.

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Before getting into A, B, and C differences for the F-35, a short primer on how to tell an F-35 from an F-22 may help avoid an even larger fighter faux pas. After all, the F-22 and F-35 look similar as well, especially from certain angles and at a distance. Both the F-22 and F-35 have two intakes, two tails, and similar planforms.

If the two aircraft happen to be parked together, the F-22, however, is noticeably larger. The Raptor is about ten feet longer than a Lightning II. Its wingspan is about ten feet wider than an F-35A’s and F-35B’s, and roughly the same as an F-35C’s.

From behind, the twin, rectangular thrust-vectoring exhaust nozzles on the F-22 are an obvious difference. The F-35 has one round exhaust nozzle for its single engine. The geometry of the engine intakes distinguishes the two aircraft from the top and side. The Raptor’s intakes angle back. On the Lightning II, they point forward. Intake differences are visible from the front view as well. Opposing sides of the F-22’s intakes are parallel. The corners are slightly rounded. The F-35’s intake angles are sharper. A space between the intake and the fuselage, called a diverter, is found only on the Raptor as well. The F-35’s diverterless intake sits flush to the fuselage.

The single- vs. twin-engine difference plays out on the top sides of the two aircraft as well. The F-22 has two humps between the tails. The F-35 has just one. On the underside, the F-22 is much flatter with one main (though split) weapon bay with two doors. The F-35 is more rounded and has two distinct main weapon bays each with two doors. Taxiing, the F-22 sits about a foot lower than an F-35.

Context also matters. If the airplane in question is operating from an aircraft carrier, landing vertically, taking off in a very short distance, or displaying non-USAF markings, it’s not an F-22.

Context And The F-35 Variants

When it comes to distinguishing among F-35 variants, context can provide some tips as well. If the F-35 in question is being catapulted from a carrier, it’s an F-35C. If it’s landing vertically, it’s an F-35B. If it has Royal Air Force markings, it’s an F-35B. If it has international markings that aren’t associated with the RAF, it’s an F-35A (at least until another international air force procures B or C models).

Basic A, B, & C Differences

The A model is most easily distinguished from other F-35 models by the blister on the upper left side for its internal GAU-22/A Gatling-type gun. (B and C models do not have internal guns.) Like the B model, the F-35A has a smaller wing. The A model is the only F-35 variant with a refueling receptacle on its dorsal spine. The receptacle markings are clearly visible from the top view.

The B model is most easily distinguished from other F-35 models by its vertical lift system. The system comes into play at almost every viewing angle of the aircraft. Even in up-and-away (non vertical) flight, the F-35B has visual clues for the vertical lift system. The lift fan door flattens the upper surface of the F-35 just behind the cockpit, giving this model a distinctive hump. The hump is especially noticeable from front and side perspectives. The lift fan itself abbreviates the aft end of the canopy line as well.

Panel lines and markings are associated with the lift system are visible on the top and bottom sides of the F-35B. From above, panel lines for the lift fan door and the auxiliary air inlet are visible. From below, the doors for lift fan exhaust appear just behind the front landing gear doors. The aft end of the lower fuselage also has a seam for the doors that open when the three-bearing swivel duct goes into action in STOVL mode. (The A and C models have a hump in this location where their arresting/barricade tailhooks are stored.) The B model also has a diamond-shaped roll duct on the underside of each wing.

The C model is most easily distinguished from other F-35 models by its larger wing, which provides almost fifty percent more wing area than the A and B models. The hinge line for the wing fold is visible from top and bottom views. The F-35C wing has an additional control surfaces, called ailerons, on the trailing edge as well (two control surfaces on each wing instead of one). The inner control surfaces on the F-35C wing and the ones on the A and B are called flaperons. The landing gear on the F-35C is noticeable beefier. The nose gear has two tires and a launch bar that extends forward and upward from the wheels.

Another Trick: Markings

Markings can also be used to distinguish F-35 variants. US Air Force markings equate to the A model. US Marines to the B or C model. (The Marine Corps is purchasing eighty C models.) And US Navy to the C model only. The Air Force puts the aircraft identification number, or serial number, on the tail (F-35A). The US Marines and Navy put their identification numbers, called Bureau numbers, on the empennage just below the horizontal tails. To make identification somewhat easier, the F-35 variant designation appears just above the bureau number for the US Marine Corps and Navy. Unfortunately, because of their location these markings are not apparent in most photos. International operators have their own specific requirements for markings.

Other Notes

As noted in a previous Code One article, Norwegian F-35s will be distinguishable by a small, aerodynamically clean bump on the upper fuselage between the two vertical tails. The bump contains a dragchute.

Nosebooms are peculiar to flight test F-35s dedicated to flight sciences testing.

The major differences between the X-35 demonstrator aircraft, which are no longer flying, and F-35 were covered in another previous Code One article.

Basic Cheat Sheet

The F-35A has a small wing, full canopy, gun blister on the left upper side, and aerial refueling receptacle markings on its dorsal. It has no panel lines or markings associated with a STOVL lift system.

The F-35B has a small wing, distinctive fuselage hump and abbreviated canopy (thanks to the lift fan), refueling probe on the right side, and numerous markings, panel lines, and actual hardware associated with its vertical lift system.

The F-35C has the big wing, wing folds, ailerons, full canopy, refueling probe on the right side, and a launch bar and two tires on the front landing gear. If the aircraft has Navy markings, it’s an F-35C.

Three Lockheed Martin F-35A Lightning II "Joint Strike Fighter's", assigned to the 63rd Fighter Squadron at Luke Air Force Base, Ariz., fly in formation during a refueling mission Aug. 27, 2019, near Phoenix. A Boeing KC-135 Stratotanker, assigned to the Arizona Air National Guard, 161st Fueling Wing, refueled six F-35s. During a refueling mission, the boom operator extends the boom to make contact with the aircraft and once in contact, fuel is pumped through the boom to the aircraft.

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.

A formation flight of Lockheed Martin F-35 "Lightning II" "Joint Strike Fighter's" over Edwards Air Force Base, California. The 31st Test and Evaluation Squadron recently completed its initial operational test and evaluation mission and six F-35s were reassigned to the 422nd Test and Evaluation Squadron at Nellis Air Force Base, Nevada. Included in the formation are two F-35As, two F-35Bs, and one F-35C.

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.

I'm going to be using this image in a new posting on my blog this weekend. I've been doing a lot of reading on the topic of "transhumanism". What if someday they developed the technology to allow you to take your consciousness, your soul maybe, out of your frail, fleshy body and import it into a machine? Your life could go on possibly in a 'Virtual Environment' very similar to Second Life. Maybe this is what Second Life is going to evolve into someday. Hypothetically you could live forever; a sort of computerized immortality.

Would you be willing or even interested in trading your physical body for life in a robot or computer simulation?

bernardbroonosworld.blogspot.com/

I'll be speculating on this in my next blog update...

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.

This is an old pic from my apartment in Vienna, we lived on 6th floor and had a roof terrace No I wasn´t rich, :) I wish I had been because then I could have rented a larger studio than my tiny room in the apartment That would really have been needed since most of my paintings at that time was 100 x 100 cm and my room was probably only twice as wide, and all my art had to share room with most or my belongings and also be the storage room for finished art ready for hanging!

well, still if someone game me a free space in Vienna which was only half that I would take it, it would work quite fine with my smaller style paintings and drawings now :)

--------------------------------------------

Café Frequenters Episode 174

--------------------------------------------

Jimmy was sitting in a sleazy café staring down his coffee cup, why was he here? he would only end up at cafés if he was gonna do some professional business like meeting an agent or "take a fellow agent out" that is not for a dinner, that is for elimination, but that goes without saying doesn´t it?

Why was he sitting here staring in to this coffeecup waiting for nothing to happen, listening to the other guest chatting away..

...if Jimmy was free, that is an agent is never free, but always woriking, but when he had no emediate actions or orders to perform he would rather end up on a sleazy pub rather than a café with mostly sober people...

Why had he walked all the way here? just stupid, what was he gonna do here? take a free commercial ad postcard and pull up his agent pen and doodle or perhaps talk to some of the strangers. laughing and telling stories, ha, ha, how pointless that would be...

Jimmy left as fast as he could before he would actually produce a doodle, if he would have done that he would have lost all of his self-respect...

Jimmy said to him self; "hey Jimmy Shape up, you are on your way down!"

------

Hello dear Thord!

I know you have been waiting for the next episode of this wonderful pulp fiction...

oh by the way do you know what happened at the restaurant today? my Swedish friend came to visit, that is, he dind´t know that I was there, it is a friend of Silva and Ines and I have´t been seeing them a lot since I started working here in the danish capital, an how he and some friend stumbled in to the basement and I greeted them in Danish, then he just said, oh it is Johnny working here, we gotta eat here... Sadly I didn´t get to talk to him much more since one group of 153 Koreans and a Guide came in, so it was swearing in Yugoslav by me and the Swedish-Albanian chef in the Kitchen again, since the owner had forgotten (as usual) to book them in to our computerized schedule...

Well see you soon, either in Denmark or Sweden or any other less likely country!

Take care!

/ Jonny the octopus on speed

1962 Oldsmbile F-85 Jetfire Hardtop Coupe

General Motors was flexing its engineering muscles in the early Sixties, especially when it came to the corporation’s new Y-body small cars. The line of 112-inch-wheelbase premium compacts included the Pontiac Tempest with independent rear suspension and curved “rope drive” driveshaft. Meanwhile, the Buick Special and Oldsmobile F-85 bowed in 1961 with an aluminum V8, followed in ’62 by a 90-degree V6 initially exclusive to Buick.

In April 1962, Olds introduced America’s first mass-market turbocharged car, the F-85 Jetfire. (Chevrolet brought out its turbocharged Corvair Monza Spyder about a month later.) A turbocharger uses the force of escaping exhaust gas to turn impellers that raise air pressure in the intake manifold, forcing the fuel mixture into the combustion chambers for more power. Working with Garrett AirResearch, Olds adapted a turbocharger to the 215-cid aluminum V-8. Where naturally aspirated versions made 155 or 185 horsepower, the Jetfire’s “Turbo Rocket” version put out 215 horsepower.

Turbo engines usually have reduced compression to avoid preignition or “pinging,” but to reach the magic one-horsepower-per-cubic-inch mark, Olds engineers used a high 10.25:1 compression. To head off detonation, an ingenious fluid-injection system added a 50/50 mix of water and alcohol (“Turbo-Rocket Fluid”) to the fuel mixture to lower the combustion-chamber temperature. A wastegate limited turbo boost.

Inside, a vacuum-boost gauge on the standard center console indicated if the turbo was doing its job. The gauge also included a warning light to remind owners to refill the Turbo-Rocket Fluid tank—a bottle in the engine bay held an emergency supply.

A Jetfire could go 0-60 mph in 8.5 seconds and had a top speed of 107. The quarter-mile run was achieved in 16.8 seconds. All Jetfires were hardtop coupes with standard front bucket seats. The Jetfire cost $3049.

Oldsmobile engineers came up with a lot of ingenious engineering to make the turbo work, but ultimately the engine was unreliable in the hands of average owners who often failed to refill the Turbo-Rocket Fluid tank. In 1965 Olds recalled the Jetfires to replace the turbocharger with a conventional four-barrel carburetor. Today, turbos benefit from computerized technology and are increasingly popular because they generate more power from small, fuel-efficient engines.

Only 3765 Jetfires were sold in 1962, with a further 5842 built in its final year of 1963. It’s estimated that only 30-35 with a functioning turbocharger remain. It is one of only about 50 ’62s with a four-speed manual transmission.

Post lunar eclipse, Ewa Bch, HI.

Shot with a 5DMkIII and a EF800mm lens on a Celestron CGEM DX computerized mount.

08Oct14

Graphic altered in a session with This Tree and the surrounding landscape. 2008 © All rights reserved.

- it's been raining, and it stoped - still very dark clouds, then the sun came through - we have this changing weather here - and sometimes like this, always makes great sceneries !

BILD0634=(hdr)+(hdr)(IRF)_X2(hdr)+Enh1Porc

<The full moon last summer in the village

Or look; Around the Village...

- The Lone Tree

Ford Escort Mk.III XR3 (1981-83) Engine 1597cc S4 OC

Registration Number DTA 325 Y (Exeter)

FORD (UK) SET

www.flickr.com/photos/45676495@N05/sets/72157623665118181...

The Mark III Escort was launched in 1980, unlike the Mark II the new car was more than a reskin of the previous generation Escort. The Mark III was a departure from the two previous models, the biggest changes being the adoption of front-wheel drive, and the new hatchback body. The car used Ford's contemporary design language of the period with the black louvred radiator grille and straked rear lamp clusters, as well as introducing the aerodynamic "bustle-back" bootlid stump.

To compete with Volkswagen's Golf GTI, a hot hatch version of the Mark III was developed – the XR3. Initially this featured a tuned version of the 1.6 L CVH engine of 96bhp

fitted with a twin-choke Weber carburettor, uprated suspension and numerous cosmetic alterations.

The car lacked the five speed transmission and fuel injection of its Volkswagen rival a situation addressed in October 1982 for the 1983 model year with the arrival of the XR3i with 105bhp eight months behind the limited edition (8,659 examples), racetrack-influenced RS 1600i. The Cologne-developed RS received a more powerful engine with 115 PS (85 kW), thanks to computerized ignition and a modified head as well as the fuel injection.

Diolch yn fawr am 67,364,638 o olygfeydd anhygoel, mwynhewch ac arhoswch yn ddiogel

Thank you 67,364,368 amazing views, enjoy and stay safe

Shot 02.09.2018 at Himley Hall, Wolverhampton Ref 136-075

Southeast Financial Center is a two-acre development in Miami, Florida, United States. It consists of a 764 feet (233 m) tall office skyscraper and its 15-story parking garage. It was previously known as the Southeast Financial Center (1984–1992), the First Union Financial Center (1992–2003), and the Wachovia Financial Center (2003-2011). In 2011, it retook its old name of Southeast Financial Center as Wachovia merged with Wells Fargo and moved to the nearby Wells Fargo Center.

When topped-off in August 1983, it was the tallest building south of New York City and east of the Mississippi River, taking away the same title from the Westin Peachtree Plaza Hotel, in Atlanta, Georgia. It remained the tallest building in the southeastern U.S. until 1987, when it was surpassed by One Atlantic Center in Atlanta and the tallest in Florida until October 1, 2003, when it was surpassed by the Four Seasons Hotel and Tower, also in Miami. It remains the tallest office tower in Florida and the third tallest building in Miami.

Southeast Financial Center was constructed in three years with more than 500 construction workers. Approximately 6,650 tons of structural steel, 80,000 cubic yards of concrete and 7000 cubic tons of reinforcing steel bars went into its construction. The complex sits on a series of reinforced concrete grade beams tied to 150 concrete caissons as much as ten feet in diameter and to a depth of 80 feet. A steel space-frame canopy with glass skylights covers the outdoor plaza between the tower and low-rise building.

The tower has a composite structure. The exterior columns and beams are concrete encased steel wide flanges surrounded by reinforcing bars. The composite exterior frame was formed using hydraulic steel forms, or "flying forms," jacked into place with a "kangaroo" crane, that was located in the core and manually clamped into place. Wide flange beams topped by a metal deck and concrete form the interior floor framing. The core is A braced steel frame, designed to laterally resist wind loads. The construction of one typical floor was completed every five days.

The low-rise banking hall and parking building is a concrete-framed structure. Each floor consists of nearly an acre of continuously poured concrete. When the concrete had sufficiently hardened, compressed air was used to blow the forms fiberglass forms from under the completed floor. It was then rolled out to the exterior where it was raised by crane into position for the next floor.

The building was recognized as Miami's first and only office building to be certified for the LEED Gold award in January 2010.

The center was developed by a partnership consisting of Gerald D. Hines Interests, Southeast Bank and Corporate Property Investors for $180 million. It was originally built as the headquarters for Southeast Bank, which originally occupied 50 percent of the complex's space. It remained Southeast Bank's headquarters there until it was liquidated in 1991.

The Southeast Financial Center comprises two buildings: the 55-story office tower and the 15-story parking annex. The tower has 53 stories of office space. The first floor is dedicated for retail, the second floor is the lobby and the 55th floor was home to the luxurious Miami City Club. The parking annex has 12 floors of parking space for 1,150 cars. The first floor is dedicated for retail, the second floor is a banking hall and the 15th floor has the Downtown Athletic Club. A landscaped plaza lies between the office tower and the parking annex. An enclosed walkway connects the second story of the tower with the second story of the annex. The courtyard is partially protected from the elements by a steel and glass space frame canopy spanning the plaza and attached to the tower and annex. Southeast Bank's executive offices were located on the 38th floor. Ground was broken on the complex on December 12, 1981 and the official dedication and opening for the complex was held on October 23, 1984.

The Southeast Financial Center was designed by Edward Charles Bassett of Skidmore, Owings and Merrill. The Associate Architect was Spillis Candela & Partners. It has 1,145,311 ft² (106,000 m²) of office space. A typical floor has about 22,000 ft² (2,043.87 m²) of office space. Each floor has 9 ft x 9 ft (2.7 m x 2.7 m) floor to ceiling windows. (All of the building's windows are tinted except for the top floor, resulting in strikingly bright and clear views from there.) The total complex has over 2.2 million ft² (204,000 m²). The distinctive setbacks begin at the 43rd floor. Each typical floor plate has 9 corner offices and the top twelve floors have as many as 16. There are 43 elevators in the office tower. An emergency control station provides computerized monitoring for the entire complex, and four generators for backup power.

The Southeast Financial Center can be seen as far away as Ft. Lauderdale and halfway toward Bimini. Night space shuttle launches from Cape Canaveral 200 miles to the north were plainly visible from the higher floors. The roof of the building was featured in the Wesley Snipes motion picture Drop Zone, where an eccentric base jumper named Swoop parachutes down to the street from a suspended window cleaning trolley. The building also appeared in several episodes of the 1980s TV show Miami Vice and at the end of each episode's opening credits.

Zara founder Amancio Ortega purchased the building from J.P. Morgan Asset Management in December 2016. The purchase price was reportedly over $500 million, making it one of the largest real estate transactions in South Florida history.

Credit for the data above is given to the following websites:

en.wikipedia.org/wiki/Southeast_Financial_Center

www.emporis.com/buildings/122292/wachovia-financial-cente...

© All Rights Reserved - you may not use this image in any form without my prior permission.

Ford Escort (MkIII) RS1600i (1984-90) Engine 1597 cc S4 OC 115PS

Registration Number YWX 88- - (Not fully visable, originally allocated from Leeds)

FORD EUROPE ALBUM

www.flickr.com/photos/45676495@N05/sets/72157623665118181...

The Mark III Escort was developed under the code name Erika, and launched in 1980, unlike the Mark II the new car was more than a reskin of the previous generation Escort. The Mark III was a departure from the two previous models, the biggest changes being the adoption of front-wheel drive, and the new hatchback body. The car used Ford's contemporary design language of the period with the black louvred radiator grille and straked rear lamp clusters, as well as introducing the aerodynamic "bustle-back" bootlid stump. Sales in the United Kingdom increased, and by 1982 it had overtaken the ageing Cortina as the nation's best-selling car, beginning an eight-year run as Britain's best selling car.

New were the overhead camshaft CVH engines in 1.3 L and 1.6 L formats, with the older Ford Kent-based "Valencia" engine from the Fiesta powering the 1.1 L. From launch, the car was available in base (Popular), L, GL, Ghia and XR3 trim.

A convertible version, made by coachbuilder Karmann, appeared the same year as the five-door estate (1983). It was the first drop-top car produced by Ford Europe since the Corsair of the 1960s. The Escort Cabriolet was initially available in both XR3i and Ghia specification, but the Ghia variant was later dropped.

To compete with Volkswagen's Golf GTI, a hot hatch version of the Mark III was developed – the XR3. Initially this featured a tuned version of the 1.6 L CVH engine of 96bhp

fitted with a twin-choke Weber carburettor, uprated suspension and numerous cosmetic alterations.

The car lacked the five speed transmission and fuel injection of its Volkswagen rival a situation addressed in October 1982 for the 1983 model year with the arrival of the XR3i with 105bhp eight months behind the limited edition (8,659 examples), racetrack-influenced RS 1600i. The Cologne-developed RS received a more powerful engine with 115 PS (85 kW), thanks to computerized ignition and a modified head as well as the fuel injection

Diolch yn fawr am 72,317,139 o olygfeydd anhygoel, mwynhewch ac arhoswch yn ddiogel

Thank you 72,317,139 amazing views, enjoy and stay safe

Shot 05.05.2019 at Catton Park Classic Car Show Ref 141-066

Made for SWFactions.

Original Post: www.eurobricks.com/forum/index.php?/forums/topic/180781-v...

The heroic Captain Phoenix (part-time swoop racer and part-time bounty hunter) stalks the treacherous radioactive wastelands of Malagarr!

Working off intelligence received from the CFS vigilante network known as Nimbus Cell, Captain Phoenix has tracked down a scientist from the nefarious Techno Union.

“Curse you, Phoenix!” screeches the scientist, technologically. “Don’t you know what we could learn from this place? Entire planets turned into reactors! Think of the power, you fool!”

“This inhospitable trash heap has a lesson to share, you’re right about that,” replies the Captain, dashingly. “I’m just not sure it’s a lesson you’re willing to learn.”

“Ha! These fools made mistakes! We would do it better!” The scientist began cackling. Evil, computerized cackling!

Captain Phoenix clenched his jaw. “Your hubris blinds you, doctor!” He raised his ray blaster, set to ‘enjustify’. Time to end this mad scheme once and for all.

Just then, movement on the ridge! A cloud of red dust fades to reveal a new danger, a wrench in the cogs: a vicious reaver gang with weapons primed! The Techno Union scientist started to shuffle away in the chaos.

“Blast, Reavers! Watch out, scum! No one can stand in the way of justice!”

How will the dashing Captain Phoenix get out of this one? You’ll have to leave that one to your imagination, dear reader. This build isn’t getting a sequel!

+++ 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.

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.

Seriously. This is a whine. My dishwasher has been a lemon from the start. Five service calls in 11-1/2 years, and several times on my own hands and knees, head inside the machine, trying to figure out what the red light is for THIS time. It says intake/drain, but is also a computerized "red flag" for anything that might have gone wrong. Twice, the service calls have required that the dishwasher be removed and placed face down on the floor to have a part replaced. In addition to services at the house, I've been walked through various procedures via phone. I was even taught how to reset the warning light when it appeared nothing was really wrong.

So -- it happened again yesterday. We've had it. We spent the rest of the day researching and shopping for a new dishwasher. THIS one will soon be history! Meanwhile I'm sucking lemons! I'm so glad I have company on Wednesdays are for Whining! HWW

#19 of 50: 50 days of 50mm

BF-4 Flt 511 Sqn Ldr Andy Edgell and BF-5 Flt 374 Mr. Peter Wilson, Night flying aboard HMS Queen Elizabeth on 29 Sep 2018

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 Stridsfordon 9040 (STRF 9040) is a modern IFV designed to give its users an excellent blend of firepower, mobility, and protection all in a low-maintenance and easily modifiable package.

Designed to transport a squad of 8 soldiers over the rough terrain of the Nordic sub-arctic environment, the STRF 9040 gives its crew excellent mobility in places where many other competitors would fail.

The vehicle has all-around protection against 14.5 mm armor-piercing rounds while the frontal plate can stop rounds up to 30mm APFSDS.

For armament, it uses a 40mm Bofors cannon which gives it considerable firepower against targets such as infantry, fortifications, helicopters, and lightly armored vehicles. Even the sides of tanks can be engaged using APFSDS rounds. Secondary armament includes a coaxial machine gun and smoke grenade dispensers.

Despite all these great features, the STRF 90 isn't perfect. While the vehicle does have thermal imaging, its gun lacks any sort of advanced computerized fire control and isn't stabilized making it inaccurate at long range engagements. Furthermore, the vehicle only has an operational range of 320 kilometers before it needs to be refueled.

Stridsfordon 9040 (1.1 price reduction)

Category: IFV

Gun: 40mm (0)

Armor: (+1)

Speed: 70 kmh (0)

Low Maintenance: (+1)

Amphibious: (+1)

Can't hit anything: (-1)

Fuel Inefficient: (-1)

Overheats: (-1)

LEMOORE, California (June 5, 2019) The first Marine Fighter Attack Squadron (VMFA) 314 "Black Knights" Lockheed Martin F-35C "Lightning II" from Naval Air Station (NAS) Lemoore flown by CAPT Tommy Beau Locke from Strike Fighter Squadron (VFA) 125 "Rough Raiders" flies in formation over the Sierra's with the VFMA-314 squadron F/A-18A++, flown by LtCol Cedar Hinton aircraft "passing the lead" as part of the F/A-18 Sundown with the "Black Knights".

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 Lockheed Martin 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 Boeing 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 Lockheed Martin 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 Lake Superior Terminal & Transfer Railway's "Connor's Point Job" went on duty at 4:01PM. The Terminal actually called it the Soo Job but it did quite a bit more work than just interchanging freight cars with the Soo Line at the Soo's Belknap Street yard. After making the run to the Soo, this pair of switch engines (two were always assigned to this job account heavy tonnage and steep grades to the harbor front, usually the 103-104 but also the 105 when one of the others was in the shop) moved on to handle the industries located on Connor's Point. This included switching of Continental Grain Company, Marine Fueling, Cutler-Laliberte-McDougal Corporation, Huron Cement, Superior Fibre Products, the sewage plant, and Great Lakes Storage Company. The Soo Job's crew did all they could handle in a 12 hour shift and that all started right here at Superior Union Depot.

The Terminal actually owned this building. During this era Amtrak used the ticket office and lobby located center building on the first floor, and the baggage room on this end too. The rest of it was used by the LST&T Railway. Their general offices were located on the second floor. The yardmaster's office and crew lunch and locker room were on the first floor behind the locomotives. Which is why you'll always see engines parked near the north end of the depot as the crews stopped here briefly to pick up their instructions before departing with cars, to take a break and grab lunch, and to drop off the conductor and his paperwork at the end of the day.

But here's the real story that I want to share with this image. You see, under those black, pitched roofs on both ends of the building were the Terminal's file storage. All of the paperwork for every penny of wage EVER paid, every car EVER switched and accounted for, and EVERY asset bought, maintained and retired, was neatly filed away inside those hot attics.

Much of the information was kept inside steel file cabinets but there were row upon row of ledger books too. Luckily, at least one of the car movement ledger books was rescued from the dumpster after the Terminal was shut down at the end of 1985. I got it from Andy Sharp after he became frustrated with the "hieroglyphics" used by the line long before the advert of computers. The Terminal never had a computer. The Terminal did it all in pencil on paper and they abbreviated everything including car numbers. And I don't mean basic number and initial. Even the car number itself was abbreviated and without showing you how that was done it would be difficult to explain.

Fortunately, I had one ledger book from Andy, all of the maps for the entire railroad, and a numbered industry list that explained which numbered codes went with which location on the railroad. Only by comparing the codes in the ledger book with the codes on the industry list and maps were we finally able to unravel the mystery of car movements on the whole of the LST&T. Of course, an LST&T Railway yardmaster could have easily explained it to any of us, but we didn't have one of them handy here in Chicago, so we figured it out from scratch. Basically we reverse-engineered the different data sets until it made sense.

The work of spread-sheeting all of the raw data was dished off to Dan Holbrook who "computerized" all of the data contained within my June 1955 ledger. Dan was a yardmaster with BN so he understood what the codes could mean. His work on this book was the only thing that was ever computerized about the LST&T. A small sampling of his final work on the DSS&A and Soo tranfers ended up on page 11 of "The Soo" (quarterly publication of the Soo Line Historical and Technical Society) Winter 2007, Vol. 29, No. 1 edition. Those breakouts would have been impossible to determine without the ledger book, the maps and industry list, and a basic understanding of railroad accounting.

Much of the data that has been saved on the history of equipment used by the Terminal came from these files too, partially as a result of meetings I had with Ass't. Superintendent Dennis J. MacKay. Dennis was very helpful to me and when the Terminal was shut down he became a track inspector with the BN. But before that happened, hundreds of pages of material and all of the Terminals standard forms were copied and saved in order to preserve the history of this little railroad. None of that would have happened without sharing of information and caring to take the time to do the work in the first place.

Andy Roth did a fine series of stories on the Terminal in the SLH&TS magazines (mentioned above) and those stories benefited from his meeting with Lew C. Michael and others from the Terminal plus the ground work we did from Chicagoland. All of this labor to interview people who worked here and to unravel the mystery of the files sitting inside the cabinets stored under those black, pitched roofs was a collective win for saving and sharing history of this little railroad. As is often the case, pictures can be worth even more than a thousands words when we know the whole story.

Job well done, everyone. Long live The Terminal!

"Solar Lottery" was Philip K. Dick's first published novel. It takes place in a world dominated by logic and numbers. Loosely based on a numerical military strategy employed by U.S. and Soviet intelligence called minimax (part of game theory), the Quizmaster, head of world government, is chosen through a sophisticated, computerized lottery. This element of randomization in the society serves as a form of social control since nobody, in theory at least, has any more of an advantage over anybody else in becoming the next Quizmaster.

Society is further entertained by a televised selection process in which an assassin is also allegedly chosen at random. By countering and putting down these threats to his life (using telepathic bodyguards as defense), the leader gains the respect of the people. If he loses his life, a new Quizmaster, as well as another assassin, are again randomly selected. Quizmasters have historically held office for timespans ranging from a few minutes to several years. The average life expectancy is therefore on the order of a couple of weeks. [Source: Wikipedia]

Canon FD 50mm f1.8 S.C. lens

Expired 2004 WH Smith 200 film

Photo job opportunity: bblkwok[AT] hotmail[DOT]com

Instagram/EyeEm/YouTube/Tumblr/500px: bblkwok

This photograph shows a solar prominence taken from Skylab on August 21, 1973. Interpretation of the rich store of Skylab ultraviolet solar data was facilitated by computerized color enhancement of the original black-and-white images, highlighting subtle but important brightness differences.

NASA Media Usage Guidelines

Credit: NASA

Image Number: 7461522

Date: August 21, 1973

We recently visited the USS Alabama Battleship Memorial Park. In addition to the amazing battleship there are many military airplanes on display. I was absolutely fascinated with the SR-71 Blackbird. Visually and operationally, this is an extraordinary aircraft! I was inspired to honor it by creating a series of photo-art pieces. In these pictures, the photos of the SR-71 were taken by me; either of the airplane on display at the park or a model airplane which I bought. The aerial shots of the earth were downloaded from NASA's website.

Interesting info about this beautiful bird:

The SR-71 reconnaissance aircraft flew missions at speeds beyond 2,000 mph and could survey the ground from 80,000 feet!! This extreme height allowed the aircraft to avoid interceptor fighter jets or missiles. The SR-71 is covered with a special black paint to absorb radar and camouflage the bird against dark skies, which inspired the Air Force to give it the official "Blackbird" name. To withstand the friction-generated heat at Mach 3+, the frame is made of titanium composite and the tires have been impregnated with aluminum and are filled with nitrogen. In the 1960s when this plane was built, computerized equipment was non-existent, thus the cockpit and flight systems were all analog.

A total of 3,551 mission sorties were flown to spy on military installations, troop movements and nuclear silos during the cold war.

The use of satellites for space surveillance and the growing danger of more effective air defense caused the Air Force to end SR-71 operations in 1990. On it's last flight it set a speed record by flying from Los Angeles to Washington DC in 1 hour, 4 minutes, 20 seconds!

+++ DISCLAIMER +++

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

Some background:

The Georgian Air Force and Air Defense Division (თავდაცვის ძალების ავიაციისა და საჰაერო თავდაცვის სარდლობა; tavdatsvis dzalebis aviatsiisa da sahaero tavdatsvis sardloba) was established on January 1, 1992, and in September the Georgian Air Force conducted its first combat flight during the separatist war in Abkhazia. On August 18, 1998, the two divisions were unified in a joint command structure and renamed the Georgian Air Force.

In 2010, the Georgian Air Force was abolished as a separate branch and incorporated into the Georgian Land Forces as Air and Air Defense sections. By that time, the equipment – primarily consisting of Eastern Bloc aircraft inherited from the Soviet Union after the country’s dissolution – was totally outdated, the most potent aircraft were a dozen Suchoj Su-25 attack aircraft and a handful of MiG-21U trainers.

The TAM-1’s development was long and protracted, though, primarily due to lack of resources and the fact that the Georgian air force was in an almost comatose state for several years, so that the potential prime customer for the TAM-1 was not officially available. However, the first TAM-1 prototype eventually made its maiden flight in September 2017. This was just in time, because the Georgian Air Force had formally been re-established in 2016, with plans for a major modernization and procurement program. Under the leadership of Georgian Minister of Defense Irakli Garibashvili the Air Force was re-prioritized and aircraft owned by the Georgian Air Force were being modernized and re-serviced after they were left abandoned for 4 years. This program lasted until 2020. In order to become more independent from foreign sources and support its domestic aircraft industry, the Georgian Air Force eventually ordered eight TAM-1s as Su-25K replacements, which would operate alongside a handful of modernized Su-25KMs from national stock. In the meantime, the new type also attained interest from abroad, e. g. from Bulgaria, the Congo and Cyprus. The IDF thoroughly tested two early production TAM-1s of the Georgian Air Force in 2018, too.

General characteristics:

Crew: 1

Length: 15.53 m (50 ft 11 in), including pitot

Wingspan: 14.36 m (47 ft 1 in)

Height: 4.8 m (15 ft 9 in)

Wing area: 35.2 m² (378 sq ft)

Empty weight: 9,800 kg (21,605 lb)

Gross weight: 14,440 kg (31,835 lb)

Max takeoff weight: 19,300 kg (42,549 lb)

Powerplant:

2× Rolls-Royce AE 3012 turbofans with 44.1 kN (9,920 lbf) thrust each

Performance:

Maximum speed: 975 km/h (606 mph, 526 kn, Mach 0.79)

Range: 1.000 km (620 mi, 540 nmi) with internal fuel, clean

Combat range: 750 km (470 mi, 400 nmi) at sea level with 4.500 kg (9,911 lb) of ordnance,

incl. two external fuel tanks

Service ceiling: 7.800 m (25,550 ft)

g limits: +6.5

Rate of climb: 58 m/s (11,400 ft/min)

Armament:

1× 35 mm (1.38 in) Oerlikon KDA cannon with 200 rds in two magazines

under the lower forward fuselage, offset to port side.

11× hardpoints with a capacity of up to 4.500 kg (9,911 lb) of external stores

The kit and its assembly:

This rather rigorous conversion had been on my project list for many years, and with the “Gunships” group build at whatifmodellers.com in late 2021 I eventually gathered my mojo to tackle it. The ingredients had already been procured long ago, but there are ideas that make you think twice before you take action…

This build was somewhat inspired by a CG rendition of a modified Su-25 that I came across while doing online search for potential ideas, running under the moniker “Su-125”, apparently created by someone called “Bispro” and published at DeviantArt in 2010; check this: (www.deviantart.com/bispro/art/Sukhoi-Su-125-Foghorn-15043...). The rendition shows a Su-25 with its engines re-located to the rear fuselage in separate nacelles, much like an A-10, plus a T-tail. However, as many photoshopped aircraft, the shown concept had IMHO some flaws. Where would a landing gear go, as the Su-125 still had shoulder wings? The engines’ position and size also looked fishy to me, quite small/narrow and very far high and back – I had doubts concerning the center of gravity. Nevertheless, I liked the idea, and the idea of an “A-10-esque remix” of the classic Frogfoot was born.

This idea was fueled even further when I found out that the Hobbycraft kit lends itself to such a conversion. The kit itself is not a brilliant Su-25 rendition, there are certainly better models of the aircraft in 1:72. However, what spoke for the kit as whiffing fodder was/is the fact that it is quite cheap (righteously so!) and AFAIK the only offering that comes with separate engine nacelles. These are attached to a completely independent central fuselage, and this avoids massive bodywork that would be necessary (if possible at all) with more conventional kits of this aircraft.

Another beneficial design feature is that the wing roots are an integral part of the original engine nacelles, forming their top side up to the fuselage spine. Through this, the original wingspan could be retained even without the nacelles, no wing extension would be necessary to retain the original proportions.

Work started with the central fuselage and the cockpit tub, which received a different (better) armored ejection seat and a pilot figure; the canopy remained unmodified and closed, because representing the model with an open cockpit would have required additional major body work on the spinal area behind the canopy. Inside, a new dashboard (from an Italeri BAe Hawk) was added, too – the original instrument panel is just a flat front bulkhead, there’s no space for the pilot to place the legs underneath the dashboard!

In parallel, the fin underwent major surgery. I initially considered an A-10-ish twin tail, but the Su-25’s high “tail stinger” prevented its implementation: the jet efflux would come very close to the tail surfaces. So, I went for something similar to the “Su-125” layout.

Mounting the OOB stabilizers to the fin was challenging, though. The fin lost its di-electric tip fairing, and it was cut into two sections, so that the tip would become long enough to match the stabilizers. A lucky find in the scrap box was a leftover tail tip from a Matchbox Blackburn Buccaneer, already shortened from a former, stillborn project: it had now the perfect length to take the Su-25 stabilizers! To make it fit on the fin, an 8mm deep section was inserted, in the form of a simple 1.5mm styrene sheet strip. Once dry, the surface was re-built with several PSR layers. Since it would sit further back on the new aircraft’s tail, the stinger with a RHAWS sensor was shortened.

On the fuselage, the attachment points for the wings and the engine nacelles were PSRed away and the front section filled with lots of lead beads, hoping that it would be enough to keep the model’s nose down.

Even though the wings had a proper span for a re-location into a low position, they still needed some attention: at the roots, there’s a ~1cm wide section without sweep (the area which would normally cover the original engine nacelles’ tops). This was mended through triangular 1.5 mm styrene wedges that extended the leading-edge sweep, roughly cut into shape once attached and later PSRed into the wings’ surfaces

The next construction site were the new landing gear attachment points. This had caused some serious headaches – where do you place and stow it? With new, low wings settled, the wings were the only logical place. But the wings were too thin to suitably take the retracted wheels, and, following the idea of a retrofitted existing design, I decided to adopt the A-10’s solution of nacelles into which the landing gear retracts forward, with the wheels still partly showing. This layout option appears quite plausible, since it would be a “graft-on” solution, and it also has the benefit of leaving lots of space for underwing stores, since the hardpoints’ position had to be modified now, too.

I was lucky to have a pair of A-10 landing gear nacelles at hand, left over from a wrecked Matchbox model from childhood time (the parts are probably 35 years old!). They were simply cut out, glued to the Su-25 wings and PSRed into shape. The result looked really good!

At this point I had to decide the model’s overall layout – where to place the wings, the tail and the new engine nacelles. The latter were not 1:72 A-10 transplants. I had some spare engine pods from the aforementioned Matchbox wreck, but these looked too rough and toylike for my taste. They were furthermore too bulky for the Su-25, which is markedly smaller than an A-10, so I had to look elsewhere. As a neat alternative for this project, I had already procured many moons ago a set of 1:144 resin PS-90A engines from a Russian company called “A.M.U.R. Reaver”, originally intended for a Tu-204 airliner or an Il-76 transport aircraft. These turbofan nacelles not only look very much like A-10 nacelles, just a bit smaller and more elegant, they are among the best resin aftermarket parts I have ever encountered: almost no flash, crisp molding, no bubbles, and perfect fit of the parts – WOW!

With these three elements at hand I was able to define the wings’ position, based on the tail, and from that the nacelles’ location, relative to the wings and the fin.

The next challenge: how to attach the new engines to the fuselage? The PS-90A engines came without pylons, so I had to improvise. I eventually found suitable pylons in the form of parts from F-14A underwing missile pylons, left over from an Italeri kit. Some major tailoring was necessary to find a proper position on the nacelles and on the fuselage, and PSRing these parts turned out to be quite difficult because of the tight and labyrinthine space.

When the engines were in place, work shifted towards the model’s underside. The landing gear was fully replaced. I initially wanted to retain the front wheel leg and the main wheels but found that the low wings would not allow a good ground clearance for underwing stores and re-arming the aircraft, a slightly taller solution was necessary. I eventually found a complete landing gear set in the scrap box, even though I am not certain to which aircraft it once belonged? I guess that the front wheel came from a Hasegawa RA-5C Vigilante, while the main gear and the wheels once belonged to an Italeri F-14A, alle struts were slightly shortened. The resulting stance is still a bit stalky, but an A-10 is also quite tall – this is just not so obvious because of the aircraft’s sheer size.

Due to the low wings and the landing gear pods, the Su-25’s hardpoints had to be re-arranged, and this eventually led to a layout very similar to the A-10. I gave the aircraft a pair of pylons inside of the pods, plus three hardpoints under the fuselage, even though all of these would only be used when slim ordnance was carried. I just fitted the outer pair. Outside of the landing gear fairings there would have been enough space for the Frogfoot’s original four outer for pylons, but I found this to be a little too much. So I gave it “just” three, with more space between them.

The respective ordnance is a mix for a CAS mission with dedicated and occasional targets. It consists of:

- Drop tanks under the inner wings (left over from a Bilek Su-17/22 kit)

- A pair of B-8M1 FFAR pods under the fuselage (from a vintage Mastercraft USSR weapon set)

- Two MERs with four 200 kg bombs each, mounted on the pylons outside of the landing gear (the odd MERs came from a Special Hobby IDF SMB-2 Super Mystère kit, the bombs are actually 1:100 USAF 750 lb bombs from a Tamiya F-105 Thunderchief in that scale)

- Four CBU-100 Rockeye Mk. II cluster bombs on the outer stations (from two Italeri USA/NATO weapon sets, each only offers a pair of these)

Yes, it’s a mix of Russian and NATO ordnance – but, like the real Georgian Su-25KM “Scorpion” upgrade, the TAM-1 would certainly be able to carry the same or even a wider mix, thanks to modified bomb racks and wirings. Esp. “dumb” weapons, which do not call for special targeting and guidance avionics, are qualified.

The gun under the nose was replaced with a piece from a hollow steel needle.

Painting and markings:

Nothing unusual here. I considered some more “exotic” options, but eventually settled for a “conservative” Soviet/Russian-style four-tone tactical camouflage, something that “normal” Su-25s would carry, too.

The disruptive pattern was adapted from a Macedonian Frogfoot but underwent some changes due to the T-tail and the engine nacelles. The basic tones were Humbrol 119 (RAF Light Earth), 150 (Forest Green), 195 (Chrome Oxide Green, RAL 6020) and 98 (Chocolate) on the upper surfaces and RLM78 from (Modelmaster #2087) from below, with a relatively low waterline, due to the low-set wings.

As usual, the model received a light black ink washing and some post-shading – especially on the hull and on the fin, where many details had either disappeared under PSR or were simply not there at all.

The landing gear and the lower areas of the cockpit were painted in light grey (Humbrol 64), while the upper cockpit sections were painted with bright turquoise (Modelmaster #2135). The wheel hubs were painted in bright green (Humbrol 101), while some di-electric fairings received a slightly less intense tone (Humbrol 2). A few of these flat fairings on the hull were furthermore created with green decal sheet material (from TL Modellbau) to avoid masking and corrections with paint.

The tactical markings became minimal, matching the look of late Georgian Su-25s. The roundels came from a Balkan Models Frogfoot sheet. The “07” was taken from a Blue Rider decal sheet, it actually belongs to a Lithuanian An-2. Some white stencils from generic MiG-21 and Mi-8 Begemot sheets were added, too, and some small markings were just painted onto the hull with yellow.

Some soot stains around the jet nozzles and the gun were added with graphite, and finally the kit was sealed with a coat of matt acrylic varnish.

A major bodywork project – and it’s weird that this is basically just a conversion of a stock kit and no kitbashing. A true Frogfoot remix! The new engines were the biggest “outsourced” addition, the A-10 landing gear fairings were a lucky find in the scrap box, and the rest is quite generic and could have looked differently. The result is impressive and balanced, though, the fictional TAM-1 looks quite plausible. The landing gear turned out to be a bit tall and stalky, though, making the aircraft look smaller on the ground than it actually is – but I left it that way.

(BuNo 168843) to VFA-101 "Grim Reapers" May 2014.

(BuNo 168845) to VFA-101 "Grim Reapers" May 2014.

(BuNo (16xxxx) Boeing F/A-18F "Super Hornet"

(BuNo (166904) Boeing F/A-18E "Super Hornet"

The purpose of VFA-101’s visit to Nevada is to begin integration of Lockheed Martin F-35C "Lightning II" with the Fallon Range Training Complex and work with NAWDC to refine tactics, techniques and procedures (TTPs) for the Lockheed Martin F-35C "Lightning II" as it integrates into the carrier air wing.

From Wikipedia, the free encyclopedia

The Boeing F/A-18E and F/A-18F "Super Hornet" are twin-engine, carrier-capable, multirole fighter aircraft variants based on the McDonnell Douglas F/A-18 "Hornet". The F/A-18E single-seat and F/A-18F tandem-seat variants are larger and more advanced derivatives of the F/A-18C and D "Hornet". The "Super Hornet" has an internal 20 mm M61 rotary cannon and can carry air-to-air missiles and air-to-surface weapons. Additional fuel can be carried in up to five external fuel tanks and the aircraft can be configured as an airborne tanker by adding an external air refueling system.

Designed and initially produced by McDonnell Douglas, the "Super Hornet" first flew in 1995. Low-rate production began in early 1997 with full-rate production starting in September 1997, after the merger of McDonnell Douglas and Boeing the previous month. The "Super Hornet" entered service with the United States Navy in 2001, replacing the Grumman F-14 "Tomcat", which was retired in 2006; the "Super Hornet" serves alongside the original "Hornet". The Royal Australian Air Force (RAAF), which has operated the F/A-18A as its main fighter since 1984, ordered the F/A-18F in 2007 to replace its aging F-111C fleet. RAAF "Super Hornet's" entered service in December 2010.

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.

+++ 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.

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 wrecking yard (Australian, New Zealand, and Canadian English), scrapyard (Irish and British English) or junkyard (American English) is the location of a business in dismantling where wrecked or decommissioned vehicles are brought, their usable parts are sold for use in operating vehicles, while the unusable metal parts, known as scrap metal parts, are sold to metal-recycling companies.

Other terms include wreck yard, wrecker's yard, salvage yard, breakers yard, dismantler and scrapheap. In the United Kingdom, car salvage yards are known as car breakers, while motorcycle salvage yards are known as bike breakers. In Australia, they are often referred to as 'Wreckers'.

The most common type of wreck yards are automobile wreck yards, but junkyards for motorcycles, bicycles, small airplanes and boats exist too.

Many salvage yards operate on a local level—when an automobile is severely damaged, has malfunctioned beyond repair, or not worth the repair, the owner may sell it to a junkyard; in some cases—as when the car has become disabled in a place where derelict cars are not allowed to be left—the car owner will pay the wrecker to haul the car away.

Salvage yards also buy most of the wrecked, derelict and abandoned vehicles that are sold at auction from police impound storage lots,and often buy vehicles from insurance tow yards as well.

The salvage yard will usually tow the vehicle from the location of its purchase to the yard, but occasionally vehicles are driven in. At the salvage yard the automobiles are typically arranged in rows, often stacked on top of one another.

Some yards keep inventories in their offices, as to the usable parts in each car, as well as the car's location in the yard. Many yards have computerized inventory systems. About 75% of any given vehicle can be recycled and used for other goods.

In recent years it is becoming increasingly common to use satellite part finder services to contact multiple salvage yards from a single source.

In the 20th century these were call centres that charged a premium rate for calls and compiled a facsimile that was sent to various salvage yards so they could respond directly if the part was in stock. Many of these are now Web-based with requests for parts being e-mailed instantly.

My Website : Twitter : Facebook : Instagram : Photocrowd

I must admit I don't recall the name of this Florentine church. It was close to the central market but unlike most Tuscan churches it was incredibly plain outside. It's almost as though they ran out of money and couldn't afford the characteristic marble cladding........

Click here to see more photos from Tuscany and Florence : www.flickr.com/photos/darrellg/albums/72157714689304067

Update : A quick google image search and I can confirm that it's San Lorenzo Church. Wikipedia confirmed my suspicions "The Medici Pope Leo X gave Michelangelo the commission to design a façade in white Carrara marble in 1518. Michelangelo made a wooden model, which shows how he adjusted the classical proportions of the facade, drawn to scale, after the ideal proportions of the human body, to the greater height of the nave. The work remained unbuilt. Michelangelo did, however, design and build the internal facade, seen from the nave looking back toward the entrances. It comprises three doors between two pilasters with garlands of oak and laurel and a balcony on two Corinthian columns.

In recent years, the association of "Friends of the Elettrice Palatina" and the Comune of Florence re-visited the question of completing the outer facade according to Michelangelo's designs. To assist with the public debate, a computerized reconstruction was projected onto the plain brick facade in February 2007. As yet, no decision has been made on the project."

© D.Godliman

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 McDonnell Douglas (now Boeing) 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 Lockheed Martin 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.

I love seeing kids being kids, climbing trees and playing outdoors...it is good to see that computers and computerized devices do not take up all of their time.

~at my second cousin's birthday party, boys climbing a tree...

This series is a fraction of the millions of lights on display at the Toledo Zoo. Everything is pretty much covered in beautiful bright color. The dancing light trees are the most famous that change colors and patterns to Christmas music by a computerized program.

After a very long time i decided to do some new fractal work.

It's where i started with before i changed my emphasis to photography.

Guess i will do some more in Winter when running out of photos...

Hope you like it.

This is a great idea and destined to be copied by many companies and institutions in the years to come...

The interactive Christmas tree..

This trio of shots shows how the canvas covered tree changes via computerized video feed, A booth is on site where people can record a message to be recorded and projected onto the tree and via the internet.. People submitting a clip will be entered into a prize draw with the chance to win a holiday to see the Northern Lights in Norway.

A wrecking yard (Australian, New Zealand, and Canadian English), scrapyard (Irish and British English) or junkyard (American English) is the location of a business in dismantling where wrecked or decommissioned vehicles are brought, their usable parts are sold for use in operating vehicles, while the unusable metal parts, known as scrap metal parts, are sold to metal-recycling companies.

Other terms include wreck yard, wrecker's yard, salvage yard, breakers yard, dismantler and scrapheap. In the United Kingdom, car salvage yards are known as car breakers, while motorcycle salvage yards are known as bike breakers. In Australia, they are often referred to as 'Wreckers'.

The most common type of wreck yards are automobile wreck yards, but junkyards for motorcycles, bicycles, small airplanes and boats exist too.

Many salvage yards operate on a local level—when an automobile is severely damaged, has malfunctioned beyond repair, or not worth the repair, the owner may sell it to a junkyard; in some cases—as when the car has become disabled in a place where derelict cars are not allowed to be left—the car owner will pay the wrecker to haul the car away.

Salvage yards also buy most of the wrecked, derelict and abandoned vehicles that are sold at auction from police impound storage lots,and often buy vehicles from insurance tow yards as well.

The salvage yard will usually tow the vehicle from the location of its purchase to the yard, but occasionally vehicles are driven in. At the salvage yard the automobiles are typically arranged in rows, often stacked on top of one another.

Some yards keep inventories in their offices, as to the usable parts in each car, as well as the car's location in the yard. Many yards have computerized inventory systems. About 75% of any given vehicle can be recycled and used for other goods.

In recent years it is becoming increasingly common to use satellite part finder services to contact multiple salvage yards from a single source.

In the 20th century these were call centres that charged a premium rate for calls and compiled a facsimile that was sent to various salvage yards so they could respond directly if the part was in stock. Many of these are now Web-based with requests for parts being e-mailed instantly.

Members of the United States Coastguard SAR team "rescue" Rob Reider from the tarmac at the 2009 Cleveland National Air Show.

Meet Rob

Development (Wikipedia)

The SA366 G1 Dauphin version was selected by the United States Coast Guard in 1979 as its new short range recovery (SRR) air-sea rescue helicopter, replacing the Sikorsky HH-52A Sea Guard. In total 99 helicopters, optimised for the USCG's search and rescue role tasks and given the designation HH-65A Dolphin, were acquired. The HH-65A is not able to perform water landings.[1] The HH-65 normally carries a crew of four: Pilot, Copilot, Flight Mechanic and Rescue Swimmer.

In 1994, the USCG therefore held a fast-track competition to select a new powerplant, and in March 2004 the Guard announced the selection of the Turbomeca Arriel 2C2-CG, already installed on the EC155. This upgrade began in 2004, and has resulted in a safer and more capable aircraft. These modified HH-65As and HH-65Bs, which also gained new avionics and other enhancements, have been designated as HH-65Cs.

Design

The HH-65A's minimum equipment requirements exceeded anything previously packaged into one helicopter weighing in at less than 10,000 pounds. 75% of the HH-65's structure — including rotorhead, rotor blades and fuselage — consists of corrosion-resistant composite materials. Some Coast Guard pilots have nicknamed the Dolphin as "Tupperwolf", a portmanteau of tupperware (because of the aircraft's high composites content)[2] and Airwolf (from the 1980s TV series).

Certified for single-pilot instrument flight rules (IFR) operation, the HH-65A was the first helicopter certified with a four-axis autopilot, allowing for hands-off hover over a pre-determined location.

Source: Wikipedia

Three Lockheed Martin F-35A-2B Lightning II "Joint Strike Fighter's", from the 63rd Fighter Squadron, and a General Dynamics (its aviation unit now part of Lockheed Martin) General Dynamics F-16 Fighting Falcon, from the 309th Fighter Squadron, fly in formation alongside a Boeing KC-135 Stratotanker, from the 161st Air Refueling Wing, during a refueling mission near Phoenix Aug. 27, 2019. Six F-35s from the 63rd FS competed in Exercise Panther Beast where the pilots tested their munition dropping accuracy.

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.

Ford Escort (MkIII) RS1600i (1984-90) Engine 1597 cc S4 OC 115PS

Registration Number B 949 PDF (Gloucester)

FORD EUROPE

www.flickr.com/photos/45676495@N05/sets/72157623665118181...

The Mark III Escort was developed under the code name Erika, and launched in 1980, unlike the Mark II the new car was more than a reskin of the previous generation Escort. The Mark III was a departure from the two previous models, the biggest changes being the adoption of front-wheel drive, and the new hatchback body. The car used Ford's contemporary design language of the period with the black louvred radiator grille and straked rear lamp clusters, as well as introducing the aerodynamic "bustle-back" bootlid stump. Sales in the United Kingdom increased, and by 1982 it had overtaken the ageing Cortina as the nation's best-selling car, beginning an eight-year run as Britain's best selling car.

New were the overhead camshaft CVH engines in 1.3 L and 1.6 L formats, with the older Ford Kent-based "Valencia" engine from the Fiesta powering the 1.1 L. From launch, the car was available in base (Popular), L, GL, Ghia and XR3 trim.

A convertible version, made by coachbuilder Karmann, appeared the same year as the five-door estate (1983). It was the first drop-top car produced by Ford Europe since the Corsair of the 1960s. The Escort Cabriolet was initially available in both XR3i and Ghia specification, but the Ghia variant was later dropped.

To compete with Volkswagen's Golf GTI, a hot hatch version of the Mark III was developed – the XR3. Initially this featured a tuned version of the 1.6 L CVH engine of 96bhp

fitted with a twin-choke Weber carburettor, uprated suspension and numerous cosmetic alterations.

The car lacked the five speed transmission and fuel injection of its Volkswagen rival a situation addressed in October 1982 for the 1983 model year with the arrival of the XR3i with 105bhp eight months behind the limited edition (8,659 examples), racetrack-influenced RS 1600i. The Cologne-developed RS received a more powerful engine with 115 PS (85 kW), thanks to computerized ignition and a modified head as well as the fuel injection

Diolch yn fawr am 67,367,304 o olygfeydd anhygoel, mwynhewch ac arhoswch yn ddiogel

Thank you 67,367,304 amazing views, enjoy and stay safe

Shot 02.09.2018 at Himley Hall, Wolverhampton Ref 136-081

+++ 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 Waffenträger (Weapon Carrier) VTS3 “Diana” was a prototype for a wheeled tank destroyer. It was developed by Thyssen-Henschel (later Rheinmetall) in Kassel, Germany, in the late Seventies, in response to a German Army requirement for a highly mobile tank destroyer with the firepower of the Leopard 1 main battle tank then in service and about to be replaced with the more capable Leopard 2 MBT, but less complex and costly. The main mission of the Diana was light to medium territorial defense, protection of infantry units and other, lighter, elements of the cavalry as well as tactical reconnaissance. Instead of heavy armor it would rather use its good power-to-weight ratio, excellent range and cross-country ability (despite the wheeled design) for defense and a computerized fire control system to accomplish this mission.

Since the tactical value of the vehicle was doubtful and other light anti-tank weapons in the form of the HOT anti-tank missile had reached operational status, so that very light vehicles and even small infantry groups could now effectively fight against full-fledged enemy battle tanks from a safe distance, the Diana’s development was stopped in 1988. Both VTS3 prototypes were mothballed, stored at the Bundeswehr Munster Training Area camp and are still waiting to be revamped as historic exhibits alongside other prototypes like the Kampfpanzer 70 in the German Tank Museum located there, too.

Specifications:

Crew: 4 (commander, driver, gunner, radio operator/second driver)

Weight: 22.6 t

Length: 7.74 m (25 ft 4 ¼ in)

Width: 2.98 m ( 9 ft 9 in)

Height: XXX

Ground clearance: 440 mm (1 ft 4 in)

Suspension: hydraulic all-wheel drive and steering

Armor:

Unknown, but sufficient to withstand 14.5 mm AP rounds

Performance:

Speed: 90 km/h (56 mph) on roads

Operational range: 720 km (445 mi)

Power/weight: 13,3 hp/ton with petrol, 17,3 hp/ton with diesel

Engine:

1× Daimler Benz OM 403A turbocharged 10-cylinder 4-stroke multi-fuel engine,

delivering 300 hp with petrol, 390 hp with diesel

Armament:

1× 105 mm L7 rifled gun with autoloader (8 rounds ready, plus 16 in reserve)

1× co-axial 7.92 mm M3 machine gun with 2.000 rounds

Two groups of four Wegmann 76 mm smoke mortars

The kit and its assembly:

I have been a big Luchs fan since I witnessed one in action during a public Bundeswehr demo day when I was around 10 years old: a huge, boxy and futuristic vehicle with strange proportions, gigantic wheels, water propellers, a mind-boggling mobility and all of this utterly silent. Today you’d assume that this vehicle had an electric engine – spooky! So I always had a soft spot for it, and now it was time and a neat occasion to build a what-if model around it.

This fictional wheeled tank prototype model was spawned by a leftover Revell 1:72 Luchs kit, which I had bought some time ago primarily for the turret, used in a fictional post-WWII SdKfz. 234 “Puma” conversion. With just the chassis left I wondered what other use or equipment it might take, and, after several weeks with the idea in the back of my mind, I stumbled at Silesian Models over an M1128 resin conversion set for the Trumpeter M1126 “Stryker” 8x8 APC model. From this set as potential donor for a conversion the prototype idea with an unmanned turret was born.

Originally I just planned to mount the new turret onto the OOB hull, but when playing with the parts I found the look with an overhanging gun barrel and the bigger turret placed well forward on the hull goofy and unbalanced. I was about to shelf the idea again, until I recognized that the Luchs’ hull is almost symmetrical – the upper hull half could be easily reversed on the chassis tub (at least on the kit…), and this would allow much better proportions. From this conceptual change the build went straightforward, reversing the upper hull only took some minor PSR. The resin turret was taken mostly OOB, it only needed a scratched adapter to fit into the respective hull opening. I just added a co-axial machine gun fairing, antenna bases (from the Luchs kit, since they could, due to the long gun barrel, not be attached to the hull anymore) and smoke grenade mortars (also taken from the Luchs).

An unnerving challenge became the Luchs kit’s suspension and drive train – it took two days to assemble the vehicle’s underside alone! While this area is very accurate and delicate, the fact that almost EVERY lever and stabilizer is a separate piece on four(!) axles made the assembly a very slow process. Just for reference: the kit comes with three and a half sprues. A full one for the wheels (each consists of three parts, and more than another one for suspension and drivetrain!

Furthermore, the many hull surface details like tools or handles – these are more than a dozen bits and pieces – are separate, very fragile and small (tiny!), too. Cutting all these wee parts out and cleaning them was a tedious affair, too, plus painting them separately.

Otherwise the model went together well, but it’s certainly not good for quick builders and those with big fingers and/or poor sight.

Painting and markings:

The paint scheme was a conservative choice; it is a faithful adaptation of the Bundeswehr’s NATO standard camouflage for the European theatre of operations that was introduced in the Eighties. It was adopted by many armies to confuse potential aggressors from the East, so that observers could not easily identify a vehicle and its nationality. It consists of a green base with red-brown and black blotches, in Germany it was executed with RAL tones, namely 6031 (Bronze Green), 8027 (Leather Brown) and 9021 (Tar Black). The pattern was standardized for each vehicle type and I stuck to the official Luchs pattern, trying to adapt it to the new/bigger turret. I used Revell acrylic paints, since the authentic RAL tones are readily available in this product range (namely the tones 06, 65 and 84). The big tires were painted with Revell 09 (Anthracite).

Next the model was treated with a highly thinned washing with black and red-brown acrylic paint, before decals were applied, taken from the OOB sheet and without unit markings, since the Diana would represent a test vehicle. After sealing them with a thin coat of clear varnish the model was furthermore treated with lightly dry-brushed Revell 45 and 75 to emphasize edges and surface details, and the separately painted hull equipment was mounted. The following step was a cloudy treatment with watercolors (from a typical school paintbox, it’s great stuff for weathering!), simulating dust residue all over the hull. After a final protective coat with matt acrylic varnish I finally added some mineral artist pigments to the lower hull areas and created mud crusts on the wheels through light wet varnish traces into which pigments were “dusted”.

Basically a simple project, but the complex Luchs kit with its zillion of wee bits and pieces took time and cost some nerves. However, the result looks pretty good, and the Stryker turret blends well into the overall package. Not certain how realistic the swap of the Luchs’ internal layout would have been, but I think that the turret moved to the rear makes more sense than the original forward position? After all, the model is supposed to be a prototype, so there’s certainly room for creative freedom. And in classic Bundeswehr colors, the whole thing even looks pretty convincing.

computerized

FALLON, Nev. (Sept. 3, 2015) Lockheed Martin F-35C Lightning IIs, attached to the "Grim Reapers" of Strike Fighter Squadron (VFA) 101, and Boeing F/A-18E/F Super Hornets attached to the Naval Aviation Warfighter Development Center (NAWDC) fly over Naval Air Station Fallon's (NASF) Range Training Complex. VFA 101, based out of Eglin Air Force Base, is conducting an F-35C cross-country visit to NASF. The purpose is to begin integration of F-35C with the Fallon Range Training Complex and work with NAWDC to refine tactics, techniques and procedures (TTP) of F-35C as it integrates into the carrier air wing.

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 Lockheed Martin C-130J Super Hercules is a four-engine turboprop military transport aircraft. The C-130J is a comprehensive update of the Lockheed C-130 Hercules, with new engines, flight deck, and other systems. The Hercules family has the longest continuous production run of any military aircraft in history. During more than 60 years of service, the family has participated in military, civilian, and humanitarian aid operations. The Hercules has outlived several planned successor designs, most notably the Advanced Medium STOL Transport contestants.

The C-130J is the newest version of the Hercules and the only model still in production. Externally similar to the classic Hercules in general appearance, the J-model features considerably updated technology. These differences include new Rolls-Royce AE 2100 D3 turboprop engines with Dowty R391 composite scimitar propellers, digital avionics (including head-up displays (HUDs) for each pilot), and reduced crew requirements. These changes have improved performance over its C-130E/H predecessors, such as 40% greater range, 21% higher maximum speed, and 41% shorter takeoff distance.

As a cargo and airlift aircraft, the C-130J's crew includes two pilots and one loadmaster (no navigator or flight engineer), while specialized USAF variants (e.g., AC-130J, EC-130J, MC-130J, HC-130J, WC-130J) may have larger crews, such as navigators/Combat Systems Officers or other specialized officer and enlisted air crew. The U.S. Marine Corps KC-130J uses a crew chief for expeditionary operations. The C-130J's cargo compartment is approximately 41 feet (12.5 m) long, 9 feet (2.74 m) high, and 10 feet (3.05 m) wide, and loading is from the rear of the fuselage. The aircraft can also be configured with the "enhanced cargo handling system". The system consists of a computerized loadmaster's station from which the user can remotely control the under-floor winch and also configure the flip-floor system to palletized roller or flat-floor cargo handling. Initially developed for the USAF, this system enables rapid role changes to be carried out and so extends the C-130J's time available to complete taskings.

This woman was sitting at an outside table at a restaurant called "Arte Around the Corner." For what it's worth, I also saw her from a different angle (which turned out not be quite as photogenic), and can confirm that she was holding a cellphone in her left hand...

Note: this photo was published in an undated (Dec 2009) blog titled "Special Edition Cellphone Wrist Watch." It was also published in a Dec 28, 2009 HOT Mobile Phone Offers blog with the same title as the caption for the photo.

Note: on Dec 28, 2009 I edited this photo, mostly to remove the shadows from the woman's sweater, so that you could see the blue colors and the textured pattern more clearly... it's probably not a big deal, but I do think it's an improvement...

Note: this photo was published in a Mar 24, 2010 blog titled "Buy a town to work at home?" It was also published in an undated (Apr 2010) Cheap Cellphone Accessories blog, with the same title as the caption that I used on this Flickr page. And it was published in a Jun 30, 2010 Technologeek blog , with the same title as the caption that I used on this Flickr page. It was also published in an undated (late Aug 2010) "Best Deal on Phones" blog titled "The Hottest Cell Phone Accessories – Bluetooth Headset, Iphone Headset And Much More." And it was published in an undated (late Oct 2010) "Wireless Keyboard" blog titled "Internet Q & A." It was also published in an undated (mid-Nov 2010) "Wireless Keyboards" blog, titled " I want to build a home music studio. Can someone please help me out on what best accessories are required?" And it was published in a Dec 27, 2010 blog titled "Q&A: What are the steps to take when u hav an idea for a new product and want to get it out in the market?"

Moving into 2011, the photo was published in an undated (late Mar 2011) blog titled "Q&A: hp compaq small dc7600 form factor question..?" It was also published in an Apr 13, 2011 Cool How to Talk to Women Images blog, with the same caption and detailed notes that I had written on this Flickr page. And it was published in a Sep 1, 2011 blog titled "Alzheimer's Journey 2: Take the Team Approach."

Moving into 2012, the photo was published in an Apr 24, 2012 blog titled "Site Solves International Crisis of Women Dining Alone." It was also published in an Aug 3, 2012 blog titled "6 Ways to Make Caregiving & Dating Go Together ? AARP." And it was published in a Nov 13, 2012 blog titled "How to Survive the Holidays When the Kids Are with the Ex." It was also published in a Nov 20, 2012 blog titled "Trends That Will Help Shape Small Businesses In 2013."

Moving into 2013, the photo was published in a Jan 2, 2013 blog titled "Cholesterol and Women: The Menopausal Spike." And it was published in a Jan 30, 2013 blog titled "The Sandwich Generation, Part Two." It was also published in a Feb 6, 2013 blog titled "Cool Computer Accessories images," as well as a Feb 13, 2013 Gadget and News blog - both with the same caption and detailed notes that I had written on this Flickr page. And it was published as an illustration in an undated (mid-Apr 2013) "Thought Questions" blog, with the caption "What's One Thing Standing Between You and Success?" It was also published in a Jun 4, 2013 blog titled "Constructing an Effective Retirement Plan," as well as a Jun 17, 2013 blog titled "Sobredosis de ideas en tu estrategia de marketing de contenidos." And it was published in a Jul 25, 2013 blog titled "Vitamin B usporava Alchajmera."

Moving into 2014, the photo was published in a Jul 10, 2014 blog titled "The Surprising Perks to Having a Small Family." And it was published in a Sep 20, 2014 blog titled "Easy Parenting, Part I."

Moving into 2015, the photo was published in an Apr 20, 2015 blog titled "成功者不會做的15種動作 ." It was also published in an Apr 27, 2015 blog titled "Unmarried And Childless By Choice: Selfish or Sensational?"

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Looking back on some old photos from 40-50 years ago, I was struck by how visible the differences were between the culture of then, versus the culture of now. In some cases, it was evident from the things people wore, or carried, or did, back then which they no longer do today. But sometimes it was the opposite: things that didn't exist back in the 1960s and 1970s have become a pervasive part of today's culture.

A good example is the cellphone: 20 years ago, it simply didn't exist. Even ten years ago, it was a relatively uncommon sight, and usually only on major streets of big cities. Today, of course, cell phones are everywhere, and everyone is using them in a variety of culture contexts.

However, I don't think this is a permanent phenomenon; after all, if you think back to the early 1980s, you probably would have seen a lot of people carrying Sony Walkmans, or "boom-box" portable radios -- all of which have disappeared...

If Moore's Law (which basically says that computers double in power every 18 months) holds up for another decade, then we'll have computerized gadgets approximately 100 times smaller, faster, cheaper, and better -- which means far better integration of music, camera, messaging, and phone, but also the possibility of the devices being so tiny that they're embedded into our eyeglasses, our earrings, or a tattoo on our forehead.

So the point of this album is to provide a frame of reference -- so that we can (hopefully) look back 10-20 years from now, and say, "Wasn't it really weird that we behaved in such bizarre ways while we interacted with those primitive devices?"