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Vice President Mike Pence, right, gives a thumbs up to the control room team after he talked with Expedition 53 crew members Joe Acaba, Randy Bresnik, and Mark Vande Hei onboard the International Space Station, while Rep. Robert Aderholt, R-Ala., center, and Marshall Space Flight Center International Space Station Payload Communications Manager Jessica Duckworth look on, Monday, Sept. 25, 2017, in the Payload Operations Integration Center (POIC) of the NASA Marshall Space Flight Center in Huntsville, Alabama. The Vice President visited the space center to view test hardware for NASA’s Space Launch System, America’s new deep space rocket and to call the crew onboard the International Space Station. Photo Credit: (NASA/Bill Ingalls)
CAPSTONE spacecraft, built by Terran Orbital and owned and operated by Advanced Space, being prepared for payload integration at Rocket Lab Launch Complex 1
VANDENBERG AIR FORCE BASE, Calif. – NASA's Orbiting Carbon Observatory-2, or OCO-2, satellite sits atop a United Launch Alliance Delta II rocket prior to encapsulation in its payload fairing at Space Launch Complex 2 at Vandenberg Air Force Base in California. Launch is scheduled for 2:56 a.m. PDT 5:56 a.m. EDT on July 1. OCO-2 is NASA’s first mission dedicated to studying atmospheric carbon dioxide, the leading human-produced greenhouse gas driving changes in Earth’s climate. OCO-2 will provide a new tool for understanding the human and natural sources of carbon dioxide emissions and the natural "sinks" that absorb carbon dioxide and help control its buildup. The observatory will measure the global geographic distribution of these sources and sinks and study their changes over time. To learn more about OCO-2, visit oco.jpl.nasa.gov Photo credit: NASA/Mark Mackley
VANDENBERG AIR FORCE BASE, Calif. – In the mobile service tower at Space Launch Complex 2 at Vandenberg Air Force Base in California, technicians are inspecting the NASA's Orbiting Carbon Observatory-2, or OCO-2, satellite. The task is taking place prior to encapsulation in its payload fairing atop a United Launch Alliance Delta II rocket. Launch is scheduled for 2:56 a.m. PDT 5:56 a.m. EDT on July 1. OCO-2 is NASA’s first mission dedicated to studying atmospheric carbon dioxide, the leading human-produced greenhouse gas driving changes in Earth’s climate. OCO-2 will provide a new tool for understanding the human and natural sources of carbon dioxide emissions and the natural "sinks" that absorb carbon dioxide and help control its buildup. The observatory will measure the global geographic distribution of these sources and sinks and study their changes over time. To learn more about OCO-2, visit oco.jpl.nasa.gov Photo credit: NASA/Mark Mackley
NASA image captured July 12, 2011
With his feet secured on a restraint on the space station remote manipulator system's robotic arm or Canadarm2, NASA astronaut Mike Fossum (frame center) holds the Robotics Refueling Mission payload, which was the focus of one of the primary chores accomplished on a six and a half hour spacewalk on July 12. The failed pump module is with DEXTRE on left side of the photo. NASA astronauts Fossum and Ron Garan performed the six-hour, 31-minute spacewalk, which represents the final scheduled extravehicular activity during shuttle missions.
Among Atlantis’s final contributions to the ISS is the Robotic Refueling Mission, developed at Goddard Space Flight Center. Atlantis brought this module to the International Space Station, where it will provide key support in maintaining future spacecrafts for years to come. STS-135 astronauts traveled to Goddard to complete special training for these robotics, a major component of the final shuttle mission. RRM is one of dozens of Goddard payloads to travel aboard orbiters into space throughout the 30-year flight history of the Shuttle Program.
Photo credit: NASA
NASA image SI35-E-007547 (12 July 2011)
NASA Goddard Space Flight Center enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission.
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Inside a clean room in Building 1555 at Vandenberg Air Force Base in California, technicians install the first half of the Northrop Grumman Pegasus XL payload fairing around NASA's Ionospheric Connection Explorer (ICON) on Oct. 4, 2018. ICON is being prepared for its launch on the Pegasus XL, which is attached to the company's L-1011 Stargazer aircraft, from the Skid Strip at Cape Canaveral Air Force Station in Florida. Launch is scheduled for Oct. 26. ICON will study the frontier of space - the dynamic zone high in Earth's atmosphere where terrestrial weather from below meets space weather above. The explorer will help determine the physics of Earth's space environment and pave the way for mitigating its effects on our technology, communications systems and society. Photo credit: NASA/Dan Quinajon
Quoting Smithsonian National Air and Space Museum | Lockheed SR-71 Blackbird:
No reconnaissance aircraft in history has operated globally in more hostile airspace or with such complete impunity than the SR-71, the world's fastest jet-propelled aircraft. The Blackbird's performance and operational achievements placed it at the pinnacle of aviation technology developments during the Cold War.
This Blackbird accrued about 2,800 hours of flight time during 24 years of active service with the U.S. Air Force. On its last flight, March 6, 1990, Lt. Col. Ed Yielding and Lt. Col. Joseph Vida set a speed record by flying from Los Angeles to Washington, D.C., in 1 hour, 4 minutes, and 20 seconds, averaging 3,418 kilometers (2,124 miles) per hour. At the flight's conclusion, they landed at Washington-Dulles International Airport and turned the airplane over to the Smithsonian.
Transferred from the United States Air Force.
Manufacturer:
Designer:
Date:
1964
Country of Origin:
United States of America
Dimensions:
Overall: 18ft 5 15/16in. x 55ft 7in. x 107ft 5in., 169998.5lb. (5.638m x 16.942m x 32.741m, 77110.8kg)
Other: 18ft 5 15/16in. x 107ft 5in. x 55ft 7in. (5.638m x 32.741m x 16.942m)
Materials:
Titanium
Physical Description:
Twin-engine, two-seat, supersonic strategic reconnaissance aircraft; airframe constructed largley of titanium and its alloys; vertical tail fins are constructed of a composite (laminated plastic-type material) to reduce radar cross-section; Pratt and Whitney J58 (JT11D-20B) turbojet engines feature large inlet shock cones.
• • • • •
See more photos of this, and the Wikipedia article.
Details, quoting from Smithsonian National Air and Space Museum | Vought F4U-1D Corsair:
By V-J Day, September 2, 1945, Corsair pilots had amassed an 11:1 kill ratio against enemy aircraft. The aircraft's distinctive inverted gull-wing design allowed ground clearance for the huge, three-bladed Hamilton Standard Hydromatic propeller, which spanned more than 4 meters (13 feet). The Pratt and Whitney R-2800 radial engine and Hydromatic propeller was the largest and one of the most powerful engine-propeller combinations ever flown on a fighter aircraft.
Charles Lindbergh flew bombing missions in a Corsair with Marine Air Group 31 against Japanese strongholds in the Pacific in 1944. This airplane is painted in the colors and markings of the Corsair Sun Setter, a Marine close-support fighter assigned to the USS Essex in July 1944.
Transferred from the United States Navy.
Manufacturer:
Date:
1940
Country of Origin:
United States of America
Dimensions:
Overall: 460 x 1020cm, 4037kg, 1250cm (15ft 1 1/8in. x 33ft 5 9/16in., 8900lb., 41ft 1/8in.)
Materials:
All metal with fabric-covered wings behind the main spar.
Physical Description:
R-2800 radial air-cooled engine with 1,850 horsepower, turned a three-blade Hamilton Standard Hydromatic propeller with solid aluminum blades spanning 13 feet 1 inch; wing bent gull-shaped on both sides of the fuselage.
Long Description:
On February 1, 1938, the United States Navy Bureau of Aeronautics requested proposals from American aircraft manufacturers for a new carrier-based fighter airplane. During April, the Vought Aircraft Corporation responded with two designs and one of them, powered by a Pratt & Whitney R-2800 engine, won the competition in June. Less than a year later, Vought test pilot Lyman A. Bullard, Jr., first flew the Vought XF4U-1 prototype on May 29, 1940. At that time, the largest engine driving the biggest propeller ever flown on a fighter aircraft propelled Bullard on this test flight. The R-2800 radial air-cooled engine developed 1,850 horsepower and it turned a three-blade Hamilton Standard Hydromatic propeller with solid aluminum blades spanning 13 feet 1 inch.
The airplane Bullard flew also had another striking feature, a wing bent gull-shaped on both sides of the fuselage. This arrangement gave additional ground clearance for the propeller and reduced drag at the wing-to-fuselage joint. Ironically for a 644-kph (400 mph) airplane, Vought covered the wing with fabric behind the main spar, a practice the company also followed on the OS2U Kingfisher (see NASM collection).
When naval air strategists had crafted the requirements for the new fighter, the need for speed had overridden all other performance goals. With this in mind, the Bureau of Aeronautics selected the most powerful air-cooled engine available, the R-2800. Vought assembled a team, lead by chief designer Rex Biesel, to design the best airframe around this powerful engine. The group included project engineer Frank Albright, aerodynamics engineer Paul Baker, and propulsion engineer James Shoemaker. Biesel and his team succeeded in building a very fast fighter but when they redesigned the prototype for production, they were forced to make an unfortunate compromise.
The Navy requested heavier armament for production Corsairs and Biesel redesigned each outboard folding wing panel to carry three .50 caliber machine guns. These guns displaced fuel tanks installed in each wing leading edge. To replace this lost capacity, an 897-liter (237 gal) fuselage tank was installed between the cockpit and the engine. To maintain the speedy and narrow fuselage profile, Biesel could not stack the cockpit on top of the tank, so he moved it nearly three feet aft. Now the wing completely blocked the pilot's line of sight during the most critical stages of landing. The early Corsair also had a vicious stall, powerful torque and propeller effects at slow speed, a short tail wheel strut, main gear struts that often bounced the airplane at touchdown, and cowl flap actuators that leaked oil onto the windshield. These difficulties, combined with the lack of cockpit visibility, made the airplane nearly impossible to land on the tiny deck of an aircraft carrier. Navy pilots soon nicknamed the F4U the 'ensign eliminator' for its tendency to kill these inexperienced aviators. The Navy refused to clear the F4U for carrier operations until late in 1944, more than seven years after the project started.
This flaw did not deter the Navy from accepting Corsairs because Navy and Marine pilots sorely needed an improved fighter to replace the Grumman F4F Wildcat (see NASM collection). By New Year's Eve, 1942, the service owned 178 F4U-1 airplanes. Early in 1943, the Navy decided to divert all Corsairs to land-based United States Marine Corps squadrons and fill Navy carrier-based units with the Grumman F6F Hellcat (see NASM collection). At its best speed of 612 kph (380 mph) at 6,992 m (23,000 ft), the Hellcat was about 24 kph (15 mph) slower than the Corsair but it was a joy to fly aboard the carrier. The F6F filled in splendidly until improvements to the F4U qualified it for carrier operations. Meanwhile, the Marines on Guadalcanal took their Corsairs into combat and engaged the enemy for the first time on February 14, 1943, six months before Hellcat pilots on that battle-scared island first encountered enemy aircraft.
The F4U had an immediate impact on the Pacific air war. Pilots could use the Corsair's speed and firepower to engage the more maneuverable Japanese airplanes only when the advantage favored the Americans. Unprotected by armor or self-sealing fuel tanks, no Japanese fighter or bomber could withstand for more than a few seconds the concentrated volley from the six .50 caliber machine guns carried by a Corsair. Major Gregory "Pappy" Boyington assumed command of Marine Corsair squadron VMF-214, nicknamed the 'Black Sheep' squadron, on September 7, 1943. During less than 5 months of action, Boyington received credit for downing 28 enemy aircraft. Enemy aircraft shot him down on January 3, 1944, but he survived the war in a Japanese prison camp.
In May and June 1944, Charles A. Lindbergh flew Corsair missions with Marine pilots at Green Island and Emirau. On September 3, 1944, Lindbergh demonstrated the F4U's bomb hauling capacity by flying a Corsair from Marine Air Group 31 carrying three bombs each weighing 450 kg (1,000 lb). He dropped this load on enemy positions at Wotje Atoll. On the September 8, Lindbergh dropped the first 900-kg (2,000 lb) bomb during an attack on the atoll. For the finale five days later, the Atlantic flyer delivered a 900-kg (2,000 lb) bomb and two 450-kg (1,000 lb) bombs. Lindbergh went ahead and flew these missions after the commander of MAG-31 informed him that if he was forced down and captured, the Japanese would almost certainly execute him.
As of V-J Day, September 2, 1945, the Navy credited Corsair pilots with destroying 2,140 enemy aircraft in aerial combat. The Navy and Marines lost 189 F4Us in combat and 1,435 Corsairs in non-combat accidents. Beginning on February 13, 1942, Marine and Navy pilots flew 64,051 operational sorties, 54,470 from runways and 9,581 from carrier decks. During the war, the British Royal Navy accepted 2,012 Corsairs and the Royal New Zealand Air Force accepted 364. The demand was so great that the Goodyear Aircraft Corporation and the Brewster Aeronautical Corporation also produced the F4U.
Corsairs returned to Navy carrier decks and Marine airfields during the Korean War. On September 10, 1952, Captain Jesse Folmar of Marine Fighter Squadron VMF-312 destroyed a MiG-15 in aerial combat over the west coast of Korea. However, F4U pilots did not have many air-to-air encounters over Korea. Their primary mission was to support Allied ground units along the battlefront.
After the World War II, civilian pilots adapted the speedy bent-wing bird from Vought to fly in competitive air races. They preferred modified versions of the F2G-1 and -2 originally built by Goodyear. Corsairs won the prestigious Thompson Trophy twice. In 1952, Vought manufactured 94 F4U-7s for the French Navy, and these aircraft saw action over Indochina but this order marked the end of Corsair production. In production longer than any other U.S. fighter to see service in World War II, Vought, Goodyear, and Brewster built a total of 12,582 F4Us.
The United States Navy donated an F4U-1D to the National Air and Space Museum in September 1960. Vought delivered this Corsair, Bureau of Aeronautics serial number 50375, to the Navy on April 26, 1944. By October, pilots of VF-10 were flying it but in November, the airplane was transferred to VF-89 at Naval Air Station Atlantic City. It remained there as the squadron moved to NAS Oceana and NAS Norfolk. During February 1945, the Navy withdrew the airplane from active service and transferred it to a pool of surplus aircraft stored at Quantico, Virginia. In 1980, NASM craftsmen restored the F4U-1D in the colors and markings of a Corsair named "Sun Setter," a fighter assigned to Marine Fighter Squadron VMF-114 when that unit served aboard the "USS Essex" in July 1944.
• • •
Quoting from Wikipedia | Vought F4U Corsair:
The Chance Vought F4U Corsair was a carrier-capable fighter aircraft that saw service primarily in World War II and the Korean War. Demand for the aircraft soon overwhelmed Vought's manufacturing capability, resulting in production by Goodyear and Brewster: Goodyear-built Corsairs were designated FG and Brewster-built aircraft F3A. From the first prototype delivery to the U.S. Navy in 1940, to final delivery in 1953 to the French, 12,571 F4U Corsairs were manufactured by Vought, in 16 separate models, in the longest production run of any piston-engined fighter in U.S. history (1942–1953).
The Corsair served in the U.S. Navy, U.S. Marines, Fleet Air Arm and the Royal New Zealand Air Force, as well as the French Navy Aeronavale and other, smaller, air forces until the 1960s. It quickly became the most capable carrier-based fighter-bomber of World War II. Some Japanese pilots regarded it as the most formidable American fighter of World War II, and the U.S. Navy counted an 11:1 kill ratio with the F4U Corsair.
F4U-1D (Corsair Mk IV): Built in parallel with the F4U-1C, but was introduced in April 1944. It had the new -8W water-injection engine. This change gave the aircraft up to 250 hp (190 kW) more power, which, in turn, increased performance. Speed, for example, was boosted from 417 miles per hour (671 km/h) to 425 miles per hour (684 km/h). Because of the U.S. Navy's need for fighter-bombers, it had a payload of rockets double the -1A's, as well as twin-rack plumbing for an additional belly drop tank. Such modifications necessitated the need for rocket tabs (attached to fully metal-plated underwing surfaces) and bomb pylons to be bolted on the fighter, however, causing extra drag. Additionally, the role of fighter-bombing was a new task for the Corsair and the wing fuel cells proved too vulnerable and were removed.[] The extra fuel carried by the two drop tanks would still allow the aircraft to fly relatively long missions despite the heavy, un-aerodynamic load. The regular armament of six machine guns were implemented as well. The canopies of most -1Ds had their struts removed along with their metal caps, which were used — at one point — as a measure to prevent the canopies' glass from cracking as they moved along the fuselage spines of the fighters.[] Also, the clear-view style "Malcolm Hood" canopy used initially on Supermarine Spitfire and P-51C Mustang aircraft was adopted as standard equipment for the -1D model, and all later F4U production aircraft. Additional production was carried out by Goodyear (FG-1D) and Brewster (F3A-1D). In Fleet Air Arm service, the latter was known as the Corsair III, and both had their wingtips clipped by 8" per wing to allow storage in the lower hangars of British carriers.
+++ 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 Messerschmitt Me 262 F was a series of multi-purpose jet planes designed by Messerschmitt for the Luftwaffe that entered service during the final phase of the Second World War in Europe. The aircraft’s design was begun in the summer of 1943 under the project handle P.1099, intended as an improvement to the successful Messerschmitt Me 262 jet fighter and also as a replacement for the Arado Ar 234 bomber/reconnaissance aircraft. The primary focus was on more payload, being either usable for more fuel (since early jet engines had poor mileage and therefore range and endurance) or for weapons, including bombs in an internal bomb bay that would enable the aircraft to fulfil a similar tactical role as the British de Havilland Mosquito. Beyond this high-speed bomber (Schnellbomber) variant, the P.1099 would also be a suitable basis for a fast reconnaissance plane, interceptors and night fighters, and trainer versions were also planned.
The Messerschmitt P.1099 was a 12 m long, conventional-looking aircraft with a wingspan of 12.6 m. It had a much wider fuselage than the Messerschmitt Me 262. It had a circular shape with a diameter of 1.7m (5 ft 6¾ in) and the cockpit was now moved closer to the aircraft’s nose, above the front landing gear well. The baseline aircraft featured a side-by-side cockpit for a crew of two, even though different layouts were envisioned for the specialized variants, including single-seaters. To save development time and to use existing jigs and tools as much as possible, the P.1099 retained the wings and the tail section of the Me 262A-2a. Despite a higher total weight (the P.1099’ MTOW was about 3 tons higher), the planned powerplants were initially two uprated Junkers Jumo 004 turbojet engines, later to be replaced by more powerful Heinkel HeS 011 turbojets.
In January 1944 the P.1099 was accepted by the RLM and received, despite the aircraft’s different structure, the designation “Me 262 F”. The first variant, the Me 262 F-1 (internally designated P.1099A), was the baseline aircraft under the handle “Jäger I”, a jet-powered single seat daytime fighter. There were three planned versions, differing mainly in armament: Version F-1a was armed with four MK 108 30 mm cannon in the lower fuselage, comparable with the earlier Me 262 A fighter, just with more fuel and ammunition. Version F-1b carried two MK 103 30 mm cannon with longer range, firepower and ammunition supply, and Version F-1c was a heavy daytime fighter with two MK 108 and two MK 103 cannon in the nose.
In parallel the Me 262 F-2 was developed as a more heavily armed and armored variant, as a dedicated heavy bomber interceptor (“Pulkjäger” or “Zerstörer”) under the handle “Jäger II”. Again, three versions were foreseen: Version F-2a would be armed with a single MK 108 cannon and a heavy MK 112 55 mm cannon in the nose. Version F-2b was the same, but it was armed with a MK 114 50 mm cannon instead of the Mk 112. Both were single seaters with a heavily armored cockpit and canopy.
The F-2c was a more thoroughly modified two-seater version; it was armed with a single MG151/20 in a small nose turret, a pair of Mk 103 in the rear of the cockpit firing up- and backwards and two defensive MG 131 in remote-controlled FDL 151 barbettes in the tail. Due to the significant changes this model had the internal project designation P.1099B.
Another two-seater, the F-2d, remained very close to the original baseline aircraft with a crew of two in a side-by-side cockpit. This aircraft was armed with the standard four MK 108 in the nose, plus one launch rail under each wing for Ruhrstahl X-4 guided missiles, which were launched and steered by the second crewman via a wire connection with the mothership. This variant did not come to fruition, however, after the X-4 missile project had been cancelled in early 1945.
All P.1099 fighters also had hardpoints under the outer wings for racks with twelve 55mm R4M unguided air-to-air missiles each, a detail taken over from the Me 262 A, even though the fuel load had to be reduced to carry them. The radio equipment of all these versions would be a FuG 16, Peil G6, FuG 101 radio altimeter, FuBl 2 blind landing equipment, as well as the FuG 25a Erstling identification friend or foe transceiver.
Beyond these initial day fighter variants, further types based on the P.1099 airframe were envisioned, too. The F-3 was a dedicated night fighter version, developed in parallel to the Me 262 G. It was based on the F-2a heavy day fighter, but it carried a crew of two (the pilot and a rearward-facing radar operator) and was equipped with a FuG 240 “Berlin” radar set and a rotating dish antenna under a streamlined plywood cover in the nose. The armament consisted of four MK 108 under the nose, similar to the F-1a day fighter, plus two additional, upward-firing MK 108 cannon (“Schräge Musik”) in the rear fuselage.
Other proposed variants (with less priority, though) were the F-4 and the F-5, which were to become the basis for fast bombers and reconnaissance aircraft with only light defensive armament, typically only a pair of MG 131 in remote-controlled tail barbettes was to be carried. The F-4 resembled the baseline P.1099A, with two bomb bays in front of and behind the main landing gear wells and a crew of two seated side-by-side in a pressurized cockpit. Two MK 108 were carried in the nose, plus the MG 131 tail barbettes. The F-5 was similar but featured a glazed bomb aimer/navigator station in the nose instead of the MK 108’s and the glazing above the pilot’s station was reduced and asymmetrical. In both bomber variants the fuselage tanks were re-arranged to make room for a single SC 1.200 in the front bomb bay, but combinations of smaller bombs could be carried, too. Alternatively, mounts for up to three cameras or a 1.350 l auxiliary tank for extended range could be carried in the bays, too.
Initial flight tests of the Me 262 F in late 1944 showed severe directional instability: especially after fuel and ammunition had been depleted and the center of gravity shifted the aircraft tended to become nose-heavy and ditch down if it was not carefully monitored and trimmed by the pilot. To cope with this problem, the engine mounts were modified, so that the CoG was shifted back. Compared with the original Me 262 the engines were placed roughly 900 mm (35.5 in) further back under the wings. The emptying sequence of the fuselage tanks was also changed, and this mostly mended the problems. Another measure to mend the directional instability issues was the enlargement of the tail surfaces, even though later production aircraft frequently had smaller Me 262 A stabilizers fitted due to material shortages and simple lack of parts.- However, due to the higher weight the Me 262 F’s handling and agility were very limited – but most of its intended roles rather relied on speed, anyway, so that dogfights could be avoided.
From 1944 on the war situation worsened considerably, and production of the new Me 262 F superseded the A variant only on selected production lines. A disused mine complex under the Walpersberg mountain was adapted for the production of complete aircraft. These were hauled to the flat top of the hill where a runway had been cleared and flown out. Between 20 and 30 Me 262 Fs were built here until early 1946, primarily fighters, the underground factory being overrun by Allied troops before it could reach a meaningful output. Wings were produced in Germany's oldest motorway tunnel at Engelberg, to the west of Stuttgart. At B8 Bergkristall-Esche II, a vast network of tunnels was excavated beneath St. Georgen/Gusen, Austria, where fully equipped fuselages for the Me 262 at a planned monthly rate of 450 units on large assembly lines were to be produced from early 1945.
After the type’s introduction to frontline units in early 1945 further handling problems arose through the aircraft’ weight, resulting from its high wing load. Both starting and landing run were excessive, so that the number of airfields from which it could be operated was relatively small. No real short-term solution could be found without fully re-designing the wings, so that RATO bottles were frequently used to get a fully loaded Me 262 F up into the air from standard airfields. These were typically fitted to racks which were mounted under the fuselage, flanking the rear bomb bay.
The Me 262 F’s landing speed was dangerously high, too. A retrofittable brake parachute, housed in a simple tubular fairing under the tail, was developed to reduce the landing distance and save brakes, which frequently overheated and could set the landed aircraft aflame.
From the Me 262 F-2a “Pulkzerstörer I”, only a small number were built and eventually entered service. Its main armament, the MK 112, was a heavy German machine cannon produced by Rheinmetall-Borsig from 1945 on – in fact, the MK 112 was basically a scaled-up MK 108, a very compact weapon with relatively low weight. The MK 112 had a caliber of 55 mm and thus fired much larger shells than the 30 mm MK 108, but the rate of fire was significantly lower (300 rounds / min compared to about 600-660 rounds / min of the MK 108). This large-caliber gun was designed primarily to combat heavy bombers, its rate of fire would have been too slow for effective aerial battles with escort fighters – but the Me 262 F would not have been a dogfighter, anyway, so that the “hit-and-run” mission profile suited the aircraft well. Fire tests showed that a single MK 112 hit with mine grenades could destroy a bomber, and with a rate of fire of five shells per second this weapon could inflict considerably higher losses on the incoming streams of Allied bombers compared to other on-board weapons used on the German side. Only the unguided R4M missiles were as effective, but the MK 112 offered considerably higher accuracy and the opportunity to execute more than just a single attack run on an incoming bomber formation.
The MK 112 was mounted in the lower starboard section of the Me 262 F-2a’s nose, its barrel protruded more than 2 m (7 ft) from its nose. The gun’s drum magazine with sixty rounds partly took up the rear space of the cockpit behind the pilot and the gun mount even used up space of the weapon bay on port side, so that only a single MK 108 with 100 rounds as an additional weapon was mounted in the lower port side weapon bay.
Its sister, the Me 262 F-2b, remained on the drawing board, because its main weapon, the 50 mm MK 114 autocannon that had been derived from the 5 cm Pak 38 anti-tank gun, had turned out to be over-complicated, overweight and unreliable. A refined version was developed as the MK 214A, though, but after flight test from February 1945, but the weapon was not deployed operationally.
Only a handful Me 262 F-2a Pulkzerstörer were eventually fielded and operated before the end of hostilities – beyond the low production numbers the lack of fuel and loss of suitable airfields highly limited the aircraft’s potential. Probably less than ten were used by operational units, including JG 53 “Pik As”, in which they served alongside other interceptors, including other Me 262 variants. Typically, bomber formations were approached from the side of a bomber formation, where their silhouettes were widest, and while still out of range of the bombers' machine guns. This broadside-attack tactic was very effective, and the aircraft’s high speed allowed the interceptors to turn around 180° and make at least a second attack run from the opposite side, before the machines dashed off and returned to their bases.
General characteristics
Crew: One
Length: 14,32 m (46 ft 11 in) overall
12,00 m (39 ft 3¾ in) fuselage only, w/o brake parachute housing
Wingspan: 12,61 m (41 ft 3¾ in)
Height: 4,43 m (14 ft 6 in)
Wing area: 24,2 m² (236 sq ft)
Empty weight: 5.061 kg (11,148 lb)
Loaded weight: 8.762 kg (19,300 lb)
Max. take-off weight: 10.062 kg (22,163 lb)
Powerplant:
2× Junkers Jumo 004 C turbojets with 12 kN (2,697 lb st) each
Performance
Maximum speed: 930 km/h (577 mph, 505 kn)
Cruising speed: 805 km/h (500 mph, 438 kn) at 6.500 m (21,290 ft)
Range: 1.340 km (830 ml, 728 nm) at 6000 m with internal fuel only
Service ceiling: 11,450 m (37,570 ft)
Rate of climb: 18 m/s (3,540 ft/min) at max. weight
Armament:
1× 55 mm (1.96 in) MK 112 machine cannon with 60 rounds
1× 30 mm (1.18 in) MK 108 machine cannon with 100 rounds
Hardpoints under the outer wings for racks with twelve 55mm R4M unguided air-to-air missiles
The kit and its assembly:
This became a submission to the late 2021 “Gunships” group build at whatifmodellers.com – what would such a competition be without at least one gun-toting German Luft ’46 interceptor? The Messerschmitt P.1099 lent itself for such a build. Since 1996 Revell offers a 1:72 IP model kit of this paper aircraft, depicting more or less the two planned versions: a basic single-seat day fighter and a heavy two-seater Zerstörer, both based on the same basis.
This what-if model was based on Revell’s interpretation of the P.1099A, and the kit goes together well. Fit is very good, even though some designs are IMHO a bit dubious. The kit’s weakest point: Revell unfortunately missed the important detail of the modified engine nacelles: the kit comes with standard Me 262 wings and engines, but due to CoG reasons the P.1099 would have had its engines moved back by about 900 mm, as mentioned in the background. I corrected this on this build with some PSR – sounds simple, but since the nacelles are not expected to be stuck to the wings in their new position roughly 1 cm further back, some serious bodywork had to be done.
Otherwise the kit was basically built OOB. I just left away the inner wheels from the main landing gear because I found the twin wheels to be “too much” for this upgraded Me 262. The P.1099 might have been heavier than the Me 262, but…? And the wheels’ tractor-like tread design looks IMHO out of place, too, so that I replaced them with a pair of MiG-21 wheels, left over from a KP kit.
The cockpit was taken OOB, even though I have doubts concerning the canopy. And when you look at mockup pictures of the P.1099 you realize that cockpit access had been facilitated through a side door at starboard, similar to the D. H. Mosquito. The cockpit tub does not consider this hatch at all, and the engraved door on the fuselage (it’s actually there!) is so tiny that only a Halfling might use it?
Well, I stuck with it “as is” and just added a pilot figure (specifically from a Matchbox Hawker tempest, because it is one of the rare cases that you get a WWII pilot wearing an oxygen mask) and a “barrel” behind the bulbous pilot seat because there’s a lot of free space in this single seat variant that is otherwise occupied by a rear gunner in Revell’s P.1099B kit. I also have doubts concerning the kit’s canopy, since the original P.1099 had a cockpit for two seated side-by-side, with a canopy that resembled the D.H. Mosquito’s a lot. I am also not certain about the stabilizers – the kit comes with standard Me 262 parts, but trustworthy sources I consulted suggest that not only the fin had been enlarged (depicted well in Revell’s kit), but also the stabilizers? To improve this, I implanted a pair of modified stabilizers that came from a Heller PZL P.23 light bomber. Sounds odd, but they were a very good match in size, shape and thickness!
The only major modification concerns the armament, even though it became just a “graft-on” solution. On the lower left side, the upper gun port was PSRed away. On the right side I added a bulged fairing for the MK 112. It was sculpted from a Matchbox Saab J29 drop tank and blended into the hull with PSR. Protruding spent cases fairings were added for both guns. The MK 112 gun barrel is a resin piece, left over from a ModelTrans tank conversion set and actually depicts a German 55 mm gun, so that this became a perfect donor piece.
Since the airframe still looked rather clean and boring I finally added a pair of JATO bottle racks to the rear fuselage (scratched from styrene profile but left empty) and a brake parachute fairing under the fin, carved from a piece of sprue.
Furthermore, a display adapter was installed into the fuselage for in-flight pictures.
Painting and markings:
This became a challenge, because I wanted a rather unusual livery, neither a standard RLM 81/82/76 late-war combo nor an improvised-cammo-over-bare-metal finish. After some research I settled upon something that was actually carried by some He 177 bombers around 1944: a uniform RLM 74 (Graugrün, Humbrol 245) upper surface with “cloudy” mottles in RLM 76 (Humbrol 247). This appears like a winter camouflage, but it’s actually quite effective at medium altitude, esp. over a cloudy landscape. The original bombers had light blue (RLM 65) undersides, but for the P.1099 from a later period and as a fighter I rather used a darker shade of RLM76 in the form of Tamiya XF-23 (Light Blue). The model received a black ink washing and some post-panel-shading.
The cockpit interior became RLM 66 (Schwarzgrau, Humbrol 67) while the landing gear and the well were painted in uniform RLM 02 (I used Revell 45, a slightly more greenish tone), with wheel discs in RLM 66, too.
Unit markings became minimal and quite sober. I gave the aircraft a typical late-war “Reichsverteidigung” fuselage band, and in JG 53’s case it is plain black. The black band was deliberately chosen because it is a good, much darker contrast to the murky RLM 74, so that the latter appears lighter than it actually is, lowering the contrast to the RLM 76 spots.
The decals were puzzled together from various sources. As an aircraft of the 3rd group the unit’s ID color would be yellow, reflected in the tactical code and the fin tip. For some contrast and to emphasize the long gun barrel I gave it white and black stripes – as a security measure for ground handling. For some more variety I painted one air intake in very dark grey (Revell 06, Anthracite) and the other one in steel Metallizer, simulating replacement parts. The Balkenkreuze come from various sheets – I used simplified “low viz” versions all around. The undulating yellow bar for the 3rd group comes from a TL Modellbau sheet, while the yellow “4” came from a Fw 190 A sheet from Sky Models. A small “4” on the nose was added as a wacky detail, too, the “Pik As” unit markings came IIRC from a Hobby Boss Bf 109 sheet. Since they turned out to have poor contrast/opacity I only used a few stencils from the P.1099A sheet, but due to the disruptive paint scheme this is not apparent.
Finally, the model was sealed with a coat of matt acrylic varnish (Italeri) and a wire antenna, scratched from heated black sprue material, was added between cockpit and fin.
Well, this modified Messerschmitt P.1099A looks simple, but the modified engine nacelles as well as the gun fairing under the nose called for serious PSR. The result looks quite natural, though, and AFAIK this weapon configuration was actually on German drawing boards. However, I am not certain about the cockpit canopy and other details on Revell’s kit, reference information is contradictive.
The paint scheme looks good, even though it was lent from a heavy bomber, and the poor Humbrol enamels did not yield a finish that I had hoped for – the paintwork could certainly have been better, but the overall impression of a late-war Pulkzerstörer is O.K., and this eventually counts.
CAPSTONE spacecraft, built by Terran Orbital and owned and operated by Advanced Space, being prepared for payload integration at Rocket Lab Launch Complex 1
Due to the extra weight of the test article, the Ares Projects team took extra precautions to load the drop test article onto an Air Force C-17 on April 13, 2010, in preparation for NASA's drogue parachute test at the U.S. Army Proving Ground near Yuma, Ariz.
Credit: NASA
About the drop test:
Under a brilliant early morning Arizona sky, NASA conducted a successful, record-breaking test of a drogue parachute being designed to return next-generation space vehicles safely to Earth. The 77,000-pound payload used in the test was dropped from the back of a U.S. Air Force C-17 at an altitude of 25,000 feet, setting a record for the heaviest single load ever extracted out of a C-17 during flight. NASA conducted the drop test, April 14, at the U.S. Army's Yuma Proving Ground near Yuma, Ariz.
Read more:
www.nasa.gov/mission_pages/constellation/ares/H10-134.html
Watch the video on YouTube:
STS064-S-001 (July 1994) --- The patch depicts the space shuttle Discovery in a payload-bay-to-Earth attitude with its primary payload, Lidar In-Space Technology Experiment (LITE-1) operating in support of Mission to Planet Earth. LITE-1 is a lidar (light detection and ranging) system that uses a three-wavelength laser, symbolized by the three gold rays emanating from the star in the payload bay that form part of the astronaut symbol. The major objective of this first flight of LITE-1 is to validate its design and operating characteristics by gathering data about the Earth's troposphere and stratosphere, represented by the clouds and dual-colored Earth limb. A secondary payload on STS-64 is the free-flier SPARTAN-201 satellite shown on the Remote Manipulator System (RMS) arm post-retrieval. The objective of SPARTAN-201 is to investigate the physics of the solar wind and complement data being obtained from the ULYSSES satellite launched on STS-41. The RMS will also operate another secondary payload, Shuttle Plume Impingement Flight Experiment (SPIFEX), which will assess the plume effects from the Orbiter's Reaction Control System thrusters. Additionally, STS-64 will test a new extravehicular activity (EVA) maneuvering device, Simplified Aid for EVA Rescue (SAFER), represented symbolically by the two small nozzles on the backpacks of the two untethered EVA crew men. The names of the crew members encircle the patch: astronauts Richard N. Richards, commander; L. Blaine Hammond Jr., pilot; Jerry M. Linenger; Susan J. Helms, Carl J. Meade and Mark C. Lee, all mission specialists. The gold or silver stars by each name represent that person's parent service.
The NASA insignia design for shuttle flights is reserved for use by the astronauts and for other official use as the NASA Administrator may authorize. Public availability has been approved only in the form of illustrations by the various news media. When and if there is any change in this policy, which we do not anticipate, it will be publicly announced.
NASA's Transiting Exoplanet Survey Satellite (TESS) container is pressure washed at the Multi-Payload Processing Facility at the agency's Kennedy Space Center in Florida. Tess will be moved to the Payload Hazardous Servicing Facility to be processed and prepared for flight. TESS is scheduled to launch atop a SpaceX Falcon 9 rocket from Space Launch Complex 40 at Cape Canaveral Air Force Station. TESS is the next step in NASA's search for planets outside our solar system, known as exoplanets. TESS is a NASA Astrophysics Explorer mission led and operated by MIT in Cambridge, Massachusetts, and managed by NASA’s Goddard Space Flight Center in Greenbelt, Maryland. Dr. George Ricker of MIT’s Kavli Institute for Astrophysics and Space Research serves as principal investigator for the mission. Additional partners include Orbital ATK, NASA’s Ames Research Center, the Harvard-Smithsonian Center for Astrophysics and the Space Telescope Science Institute. More than a dozen universities, research institutes and observatories worldwide are participants in the mission. NASA’s Launch Services Program is responsible for launch management. Photo Credit: Ben Smegelsky
Behind-the-scene image from inside our Payload Operations Integration Center of 3-D Printing in Zero-G
PictionID:44808994 - Title:Atlas Payload Component - Catalog:14_014229 - Filename:14_014229.TIF - - - Image from the Convair/General Dynamics Astronautics Atlas Negative Collection. The processing, cataloging and digitization of these images has been made possible by a generous National Historical Publications and Records grant from the National Archives and Records Administration---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
In the SpaceX Payload Processing Facility at Vandenberg Air Force Base in California, scientists and engineers who helped prepare the Jason-3 satellite for launch pose for a group photograph prior to the spacecraft begin encapsulated in its payload fairing. Once the encapsulating is complete, Jason-3 will be mated to a SpaceX Falcon 9 rocket at Vandenberg's Space Launch Complex 4. Built by Thales Alenia of France, Jason-3 will measure the topography of the ocean surface for a four-agency international partnership consisting of NOAA, NASA, Centre National d’Etudes Spatiales, France’s space agency, and the European Organization for the Exploitation of Meteorological Satellites.
Photo credit: NASA/Thiep Nguyen and Christopher Wiant
Enclosed in its payload fairing, NOAA's Geostationary Operational Environmental Satellite (GOES-R) is lifted into the Vertical Integration Facility at Space Launch Complex 41 at Cape Canaveral Air Force Station in Florida. GOES-R will be mated to the United Launch Alliance Atlas V Centaur upper stage in preparation for launch aboard the rocket in November. GOES-R is the first satellite in a series of next-generation NOAA GOES Satellites. Photo credit: NASA/Daniel Casper
S85-43441 (December 1985) --- The joint GFSC/University of Colorado Spartan-Halley payload will be represented on STS-51L by this insignia. Spartan-Halley hardware is scheduled to fly aboard the space shuttle Challenger in January of next year. Photo credit: NASA
See more photos of this, and the Wikipedia article.
Details, quoting from Smithsonian National Air and Space Museum | Space Shuttle Enterprise:
Manufacturer:
Rockwell International Corporation
Country of Origin:
United States of America
Dimensions:
Overall: 57 ft. tall x 122 ft. long x 78 ft. wing span, 150,000 lb.
(1737.36 x 3718.57 x 2377.44cm, 68039.6kg)
Materials:
Aluminum airframe and body with some fiberglass features; payload bay doors are graphite epoxy composite; thermal tiles are simulated (polyurethane foam) except for test samples of actual tiles and thermal blankets.
The first Space Shuttle orbiter, "Enterprise," is a full-scale test vehicle used for flights in the atmosphere and tests on the ground; it is not equipped for spaceflight. Although the airframe and flight control elements are like those of the Shuttles flown in space, this vehicle has no propulsion system and only simulated thermal tiles because these features were not needed for atmospheric and ground tests. "Enterprise" was rolled out at Rockwell International's assembly facility in Palmdale, California, in 1976. In 1977, it entered service for a nine-month-long approach-and-landing test flight program. Thereafter it was used for vibration tests and fit checks at NASA centers, and it also appeared in the 1983 Paris Air Show and the 1984 World's Fair in New Orleans. In 1985, NASA transferred "Enterprise" to the Smithsonian Institution's National Air and Space Museum.
Transferred from National Aeronautics and Space Administration
• • •
Quoting from Wikipedia | Space Shuttle Enterprise:
The Space Shuttle Enterprise (NASA Orbiter Vehicle Designation: OV-101) was the first Space Shuttle orbiter. It was built for NASA as part of the Space Shuttle program to perform test flights in the atmosphere. It was constructed without engines or a functional heat shield, and was therefore not capable of spaceflight.
Originally, Enterprise had been intended to be refitted for orbital flight, which would have made it the second space shuttle to fly after Columbia. However, during the construction of Columbia, details of the final design changed, particularly with regard to the weight of the fuselage and wings. Refitting Enterprise for spaceflight would have involved dismantling the orbiter and returning the sections to subcontractors across the country. As this was an expensive proposition, it was determined to be less costly to build Challenger around a body frame (STA-099) that had been created as a test article. Similarly, Enterprise was considered for refit to replace Challenger after the latter was destroyed, but Endeavour was built from structural spares instead.
Service
Construction began on the first orbiter on June 4, 1974. Designated OV-101, it was originally planned to be named Constitution and unveiled on Constitution Day, September 17, 1976. A write-in campaign by Trekkies to President Gerald Ford asked that the orbiter be named after the Starship Enterprise, featured on the television show Star Trek. Although Ford did not mention the campaign, the president—who during World War II had served on the aircraft carrier USS Monterey (CVL-26) that served with USS Enterprise (CV-6)—said that he was "partial to the name" and overrode NASA officials.
The design of OV-101 was not the same as that planned for OV-102, the first flight model; the tail was constructed differently, and it did not have the interfaces to mount OMS pods. A large number of subsystems—ranging from main engines to radar equipment—were not installed on this vehicle, but the capacity to add them in the future was retained. Instead of a thermal protection system, its surface was primarily fiberglass.
In mid-1976, the orbiter was used for ground vibration tests, allowing engineers to compare data from an actual flight vehicle with theoretical models.
On September 17, 1976, Enterprise was rolled out of Rockwell's plant at Palmdale, California. In recognition of its fictional namesake, Star Trek creator Gene Roddenberry and most of the principal cast of the original series of Star Trek were on hand at the dedication ceremony.
Approach and landing tests (ALT)
Main article: Approach and Landing Tests
On January 31, 1977, it was taken by road to Dryden Flight Research Center at Edwards Air Force Base, to begin operational testing.
While at NASA Dryden, Enterprise was used by NASA for a variety of ground and flight tests intended to validate aspects of the shuttle program. The initial nine-month testing period was referred to by the acronym ALT, for "Approach and Landing Test". These tests included a maiden "flight" on February 18, 1977 atop a Boeing 747 Shuttle Carrier Aircraft (SCA) to measure structural loads and ground handling and braking characteristics of the mated system. Ground tests of all orbiter subsystems were carried out to verify functionality prior to atmospheric flight.
The mated Enterprise/SCA combination was then subjected to five test flights with Enterprise unmanned and unactivated. The purpose of these test flights was to measure the flight characteristics of the mated combination. These tests were followed with three test flights with Enterprise manned to test the shuttle flight control systems.
Enterprise underwent five free flights where the craft separated from the SCA and was landed under astronaut control. These tests verified the flight characteristics of the orbiter design and were carried out under several aerodynamic and weight configurations. On the fifth and final glider flight, pilot-induced oscillation problems were revealed, which had to be addressed before the first orbital launch occurred.
On August 12, 1977, the space shuttle Enterprise flew on its own for the first time.
Preparation for STS-1
Following the ALT program, Enterprise was ferried among several NASA facilities to configure the craft for vibration testing. In June 1979, it was mated with an external tank and solid rocket boosters (known as a boilerplate configuration) and tested in a launch configuration at Kennedy Space Center Launch Pad 39A.
Retirement
With the completion of critical testing, Enterprise was partially disassembled to allow certain components to be reused in other shuttles, then underwent an international tour visiting France, Germany, Italy, the United Kingdom, Canada, and the U.S. states of California, Alabama, and Louisiana (during the 1984 Louisiana World Exposition). It was also used to fit-check the never-used shuttle launch pad at Vandenberg AFB, California. Finally, on November 18, 1985, Enterprise was ferried to Washington, D.C., where it became property of the Smithsonian Institution.
Post-Challenger
After the Challenger disaster, NASA considered using Enterprise as a replacement. However refitting the shuttle with all of the necessary equipment needed for it to be used in space was considered, but instead it was decided to use spares constructed at the same time as Discovery and Atlantis to build Endeavour.
Post-Columbia
In 2003, after the breakup of Columbia during re-entry, the Columbia Accident Investigation Board conducted tests at Southwest Research Institute, which used an air gun to shoot foam blocks of similar size, mass and speed to that which struck Columbia at a test structure which mechanically replicated the orbiter wing leading edge. They removed a fiberglass panel from Enterprise's wing to perform analysis of the material and attached it to the test structure, then shot a foam block at it. While the panel was not broken as a result of the test, the impact was enough to permanently deform a seal. As the reinforced carbon-carbon (RCC) panel on Columbia was 2.5 times weaker, this suggested that the RCC leading edge would have been shattered. Additional tests on the fiberglass were canceled in order not to risk damaging the test apparatus, and a panel from Discovery was tested to determine the effects of the foam on a similarly-aged RCC leading edge. On July 7, 2003, a foam impact test created a hole 41 cm by 42.5 cm (16.1 inches by 16.7 inches) in the protective RCC panel. The tests clearly demonstrated that a foam impact of the type Columbia sustained could seriously breach the protective RCC panels on the wing leading edge.
The board determined that the probable cause of the accident was that the foam impact caused a breach of a reinforced carbon-carbon panel along the leading edge of Columbia's left wing, allowing hot gases generated during re-entry to enter the wing and cause structural collapse. This caused Columbia to spin out of control, breaking up with the loss of the entire crew.
Museum exhibit
Enterprise was stored at the Smithsonian's hangar at Washington Dulles International Airport before it was restored and moved to the newly built Smithsonian's National Air and Space Museum's Steven F. Udvar-Hazy Center at Dulles International Airport, where it has been the centerpiece of the space collection. On April 12, 2011, NASA announced that Space Shuttle Discovery, the most traveled orbiter in the fleet, will be added to the collection once the Shuttle fleet is retired. When that happens, Enterprise will be moved to the Intrepid Sea-Air-Space Museum in New York City, to a newly constructed hangar adjacent to the museum. In preparation for the anticipated relocation, engineers evaluated the vehicle in early 2010 and determined that it was safe to fly on the Shuttle Carrier Aircraft once again.
John Grunsfeld, astronaut and associate administrator for the NASA Science Mission Directorate, gives remarks during a press briefing where it was announced what instruments will be carried aboard the agency’s Mars 2020 mission, Thursday, July 31, 2014 at NASA Headquarters in Washington. The new rover will carry more sophisticated, upgraded hardware and new instruments to conduct geological assessments of the rover's landing site, determine the potential habitability of the current environment, and directly search for signs of ancient Martian life -- something no previous Mars mission has done. Photo Credit: (NASA/Bill Ingalls)
PictionID:44808837 - Title:Atlas Payload Component - Catalog:14_014216 - Filename:14_014216.TIF - - - Image from the Convair/General Dynamics Astronautics Atlas Negative Collection. The processing, cataloging and digitization of these images has been made possible by a generous National Historical Publications and Records grant from the National Archives and Records Administration---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
A Kamag transporter moves the Cygnus spacecraft inside a payload fairing to the Vertical Integration Facility at Space Launch Complex 41 so the spacecraft can be lifted into place atop the waiting United Launch Alliance Atlas V rocket. Built by Orbital ATK, the Cygnus is a cargo-only spacecraft that will take about 7,300 pounds of experiments, equipment and supplies to the International Space Station. The version launching on OA-4, the fourth operational cargo resupply flight for Orbital ATK, is an enhanced Cygnus that is capable of carrying 25 percent more mass than its predecessor. Photo credit: United Launch Alliance
Oct. 26, 1998 -- STS-95 Payload Specialist John H. Glenn Jr., senator from Ohio, gives a thumbs up on his arrival at Kennedy Space Center's Shuttle Landing Facility aboard a T-38 jet. He and other crewmembers will be making final preparations for launch, targeted for liftoff at 2 p.m. on Oct. 29. The STS-95 mission includes research payloads such as the Spartan solar-observing deployable spacecraft, the Hubble Space Telescope Orbital Systems Test Platform, the International Extreme Ultraviolet Hitchhiker, as well as the SPACEHAB single module with experiments on space flight and the aging process. The mission is expected to last 8 days, 21 hours and 49 minutes, and return to KSC on Nov. 7. The other STS-95 crew members are Mission Commander Curtis L. Brown Jr., Pilot Steven W. Lindsey, Mission Specialist Scott E. Parazynski, Mission Specialist Stephen K. Robinson, Mission Specialist Pedro Duque, with the European Space Agency (ESA), and Payload Specialist Chiaki Mukai, with the National Space Development Agency of Japan (NASDA).
Photo credit: NASA
The Air Force's AEHF-4 mission, encapsulated inside a 5-meter payload fairing, is mated to its United Launch Alliance (ULA) Atlas V booster inside the Vertical Integration Facility (VIF) at Cape Canaveral's Space Launch Complex-41. Photo credit: United Launch Alliance
“Jet Propulsion Laboratory (JPL) technicians reposition and level the Cassini orbiter in the Payload Hazardous Servicing Facility at KSC in July after stacking the craft’s upper equipment module on the propulsion module. A four-year, close-up study of the Saturnian system, the Cassini mission is scheduled for launch from Cape Canaveral Air Station in October 1997. It will take seven years for the spacecraft to reach Saturn. Scientific instruments carried aboard the spacecraft will study Saturn’s atmosphere, magnetic field, rings, and several moons. JPL is managing the Cassini project for NASA.”
The Callisto demonstration payload is a partnership between Lockheed Martin, Amazon and Cisco. The Callisto technology demonstration will be integrated into NASA's Orion spacecraft for the Artemis I, uncrewed mission to the Moon. Callisto uses Amazon Alexa and Webex by Cisco to test and demonstrate commercial technology for deep space voice, video and whiteboarding communications.
"In the summer of 1984, following the cancellation of Mission 41F, Karol “Bo” Bobko (front left) received a French payload specialist, with Patrick Baudry (front right) and Jean-Loup Chretien (back right) selected to train for the position. Behind Bobko is Dave Griggs. All four men are framed by the side hatch of the shuttle simulator."
I was looking for a photo for Jean-Loup Chretien to sign and came across this interesting picture, from the training of Mission 51E.
Slated to fly aboard Challenger in 1985, the flight was canceled a week before launch, owing to a problem with one of the satellites manifested for the mission.
Chretien, as noted, was the backup payload specialist to Patrick Baudry. Chretien would finally get his own shuttle flight, STS-86/Atlantis, a rendezvous with the Russian space station Mir, in 1997.
Earlier, in 1977-78, Chretien was appointed Deputy Commander of the South Air Defense Division in Aix en Provence, and he served in this position until his selection as a cosmonaut in June 1980.
He remained a French Air Force officer but was placed on detachment to CNES for his space flight activities ensuring his availability for future flights with the Shuttle (NASA), Mir (Soviet Union) or Spacelab (ESA).
A veteran of three space flights, Chretien was the 10th Intercosmos cosmonaut, and has spent a total of 43 days, 11 hours, 18 minutes, 42 seconds in space, including an EVA of 5 hours, 57 minutes.
In April 1979, the Soviet Union offered France the opportunity to fly a cosmonaut on board a joint Soviet-French space flight, along the same lines as the agreement to fly non-Soviet cosmonauts from member countries of the Intercosmos program. The offer was accepted, and France began a cosmonaut selection program in September 1979.
Chretien was one of two finalists named on June 12, 1980. He started training at the Yuri Gagarin Cosmonaut Training Center in September 1980. The following year he was named as the research-cosmonaut for the prime crew of the Soyuz T-6 mission.
Soyuz T-6 was launched on June 24, 1982, and Chretien, Dzhanibekov and Ivanchenkov linked up with Salyut 7 and joined the crew of Berezovoi and Lebedev already on board. They spent nearly seven days carrying out a program of joint Soviet-French experiments, including a series of French echography cardiovascular monitoring system experiments, before returning to Earth after a flight lasting 7 days, 21 hours, 50 minutes, 42 seconds.
This flight made him the first Western non-American to go to space, as well as the first Western European.
Chretien made his second space flight as a research-cosmonaut on board Soyuz TM-7, which launched on November 26, 1988. Together with Volkov and Krikalev, he linked up with Mir 1 and joined the crew of Titov Manarov and Polyakov already on board.
They spent 22 days carrying out a program of joint Soviet-French experiments, including a 5 hour and 57 minute EVA by Volkov and Chretien during which the two men installed the French ERA experimental deployable structure and a panel of material samples.
In making the EVA, he became the first non-American and non-Soviet cosmonaut to walk in space. In addition, he was the first non-Soviet cosmonaut to make a second space flight aboard a Soviet spacecraft. The mission lasted 24 days, 18 hours, 7 minutes.
During 1990-93, Chretien participated in Buran spacecraft pilot training at the Moscow Joukovski Institute.
Lastly, he served on the crew of STS-86/Atlantis (September 25 to October 6, 1997) the seventh mission to rendezvous and dock with the Russian Space Station Mir.
Highlights included the delivery of a Mir attitude control computer, the exchange of U.S. crew members Mike Foale and David Wolf, a spacewalk by Scott Parazynski and Vladimir Titov to retrieve four experiments first deployed on Mir during the STS-76 docking mission, the transfer to Mir of 10,400 pounds of science and logistics, and the return of experiment hardware and results to Earth. Mission duration was 10 days, 19 hours, 21 minutes.
Chretien retired from NASA in 2001. In-person, Chester, Md., 27 Sept. 2015.
Retired Air Force Col. Karol. J. "Bo" Bobko became a NASA astronaut in September 1969. He was a crewmember on the highly successful Skylab Medical Experiments Altitude Test (SMEAT) -- a 56-day ground simulation of the Skylab mission, enabling crewmen to collect medical experiments baseline data and evaluate equipment, operations and procedures.
A veteran of three space flights, Bobko has logged a total of 386 hours in Space. He was the pilot on STS-6 (April 4-9, 1983); and was the mission commander on STS-51D (April 12-19, 1985) and STS-51J (October 3-7, 1985).
Bobko was pilot for STS-6, which launched from Kennedy Space Center, Florida, on April 4, 1983. During this maiden voyage of the spacecraft Challenger, the crew deployed a large communications satellite (TDRS) and the rocket stage (IUS) required to boost it to geosynchronous orbit.
The STS-6 crew also conducted the first shuttle spacewalk (EVA) and additionally conducted numerous other experiments in materials processing and the recording of lightning activities from space. There were also three Getaway Specials activated on the flight.
After 120 hours of orbital operations STS-6 landed on the concrete runway at Edwards Air Force Base, California, on April 9, 1983.
On his second mission Bobko was the commander of STS-51-D/Discovery which launched from Kennedy Space Center, Florida, on April 12, 1985.
The mission was to deploy two communications satellites, perform electrophoresis and echocardiograph operations in space, in addition to accomplishing other experiments. When one of the communications satellites malfunctioned, a daring attempt was made to activate the satellite which required an additional EVA, rendezvous, and operations with the remote manipulator arm.
After 168 hours of orbital operations Discovery landed on Runway 33 at Kennedy Space Center on April 19, 1985.
Bobko was next commander of STS-51-J, the second Space Shuttle Department of Defense mission, which launched from Kennedy Space Center, Florida, on October 3, 1985. This was the maiden voyage of the Atlantis.
After 98 hours of orbital operations, Atlantis landed on Edwards Air Force Base Lakebed Runway 23 on October 7, 1985.
In 1988, Bobko retired from NASA and the Air Force to join the firm of Booz Allen & Hamilton Inc., in Houston, Texas.
Bobko was born in New York, and was living in Seaford at the time of his selection as an astronaut. His parents used to own a soda distributorship on Sunrise Highway, he told me.
Even though I had a signed crew (launch) photo of the 51J mission, I like getting in-person signed photos of the astronauts I have met - and even though I'm sure of the authenticity of the 51J photo, I had bought that on the secondary market. (This in-person signature replaces an in-person portrait shot that I obtained myself - I rarely have more than one signed photo of a particular astro/cosmonaut.) In-person, Titusville, Fl., as part of the Atlantis 30th anniversary celebration, 3 Oct. 2015.
Inside the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, preparations are underway to encapsulate a Cygnus cargo spacecraft in its payload fairing. The Cygnus will be launched to the International Space Station on the upcoming Orbital ATK Commercial Resupply Services-6 mission. The spacecraft is scheduled to deliver hardware and supplies to the orbiting outpost.
Photo credit: NASA/Ben Smegelsky
The N-1 was a heavy lift rocket intended to deliver payloads beyond low Earth orbit, acting as the Soviet counterpart to the NASA Saturn V rocket. This heavy lift booster had the capability of lifting very heavy loads into orbit, designed with manned extra-orbital travel in mind. Its first stage is the most powerful rocket stage ever built.
The N1-L3 version was developed to compete with the United States Apollo Saturn V to land a man on the Moon.
N1-L3 was under-funded and under-tested, and started development in October 1965, almost four years after the Saturn V. The project was badly derailed by the death of its chief designer Sergei Korolev in 1966. After four failed launch attempts, the program was suspended in 1974, and in 1976 was officially cancelled.
I will compare with a photo of the real thing.
It is a photograph taken from the height of the eyes of people.
Payloads for this model (all mine, none adapted from BrickBuff).
Top row, left to right: telescope, mobile lab, tool rack, tools that go in cabinet inside tool rack.
Middle row, left to right: gardening toolbox, planter box, bounding boxes for front, middle, and aft cargo areas (red, yellow, blue), airlock module with inner doors on the left and outer door on bottom.
Bottom row, left to right: small tool rack, airlock module with inner doors on the left and outer doors on the right, removable interior divider module, rover, trailer with crates, removable bed with coffee maker.
The payload fairing containing the Orbital ATK Cygnus pressurized cargo module is mated to the Centaur upper stage, or second stage, of the United Launch Alliance (ULA) rocket in the Vertical Integration Facility at Space Launch Complex 41 at Cape Canaveral Air Force Station in Florida. The Orbital ATK CRS-7 commercial resupply services mission to the International Space Station is scheduled to launch atop the Atlas V from pad 41. Cygnus will deliver 7,600 pounds of supplies, equipment and scientific research materials to the space station. Photo credit: United Launch Alliance
+++ 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 Messerschmitt Me 262 F was a series of multi-purpose jet planes designed by Messerschmitt for the Luftwaffe that entered service during the final phase of the Second World War in Europe. The aircraft’s design was begun in the summer of 1943 under the project handle P.1099, intended as an improvement to the successful Messerschmitt Me 262 jet fighter and also as a replacement for the Arado Ar 234 bomber/reconnaissance aircraft. The primary focus was on more payload, being either usable for more fuel (since early jet engines had poor mileage and therefore range and endurance) or for weapons, including bombs in an internal bomb bay that would enable the aircraft to fulfil a similar tactical role as the British de Havilland Mosquito. Beyond this high-speed bomber (Schnellbomber) variant, the P.1099 would also be a suitable basis for a fast reconnaissance plane, interceptors and night fighters, and trainer versions were also planned.
The Messerschmitt P.1099 was a 12 m long, conventional-looking aircraft with a wingspan of 12.6 m. It had a much wider fuselage than the Messerschmitt Me 262. It had a circular shape with a diameter of 1.7m (5 ft 6¾ in) and the cockpit was now moved closer to the aircraft’s nose, above the front landing gear well. The baseline aircraft featured a side-by-side cockpit for a crew of two, even though different layouts were envisioned for the specialized variants, including single-seaters. To save development time and to use existing jigs and tools as much as possible, the P.1099 retained the wings and the tail section of the Me 262A-2a. Despite a higher total weight (the P.1099’ MTOW was about 3 tons higher), the planned powerplants were initially two uprated Junkers Jumo 004 turbojet engines, later to be replaced by more powerful Heinkel HeS 011 turbojets.
In January 1944 the P.1099 was accepted by the RLM and received, despite the aircraft’s different structure, the designation “Me 262 F”. The first variant, the Me 262 F-1 (internally designated P.1099A), was the baseline aircraft under the handle “Jäger I”, a jet-powered single seat daytime fighter. There were three planned versions, differing mainly in armament: Version F-1a was armed with four MK 108 30 mm cannon in the lower fuselage, comparable with the earlier Me 262 A fighter, just with more fuel and ammunition. Version F-1b carried two MK 103 30 mm cannon with longer range, firepower and ammunition supply, and Version F-1c was a heavy daytime fighter with two MK 108 and two MK 103 cannon in the nose.
In parallel the Me 262 F-2 was developed as a more heavily armed and armored variant, as a dedicated heavy bomber interceptor (“Pulkjäger” or “Zerstörer”) under the handle “Jäger II”. Again, three versions were foreseen: Version F-2a would be armed with a single MK 108 cannon and a heavy MK 112 55 mm cannon in the nose. Version F-2b was the same, but it was armed with a MK 114 50 mm cannon instead of the Mk 112. Both were single seaters with a heavily armored cockpit and canopy.
The F-2c was a more thoroughly modified two-seater version; it was armed with a single MG151/20 in a small nose turret, a pair of Mk 103 in the rear of the cockpit firing up- and backwards and two defensive MG 131 in remote-controlled FDL 151 barbettes in the tail. Due to the significant changes this model had the internal project designation P.1099B.
Another two-seater, the F-2d, remained very close to the original baseline aircraft with a crew of two in a side-by-side cockpit. This aircraft was armed with the standard four MK 108 in the nose, plus one launch rail under each wing for Ruhrstahl X-4 guided missiles, which were launched and steered by the second crewman via a wire connection with the mothership. This variant did not come to fruition, however, after the X-4 missile project had been cancelled in early 1945.
All P.1099 fighters also had hardpoints under the outer wings for racks with twelve 55mm R4M unguided air-to-air missiles each, a detail taken over from the Me 262 A, even though the fuel load had to be reduced to carry them. The radio equipment of all these versions would be a FuG 16, Peil G6, FuG 101 radio altimeter, FuBl 2 blind landing equipment, as well as the FuG 25a Erstling identification friend or foe transceiver.
Beyond these initial day fighter variants, further types based on the P.1099 airframe were envisioned, too. The F-3 was a dedicated night fighter version, developed in parallel to the Me 262 G. It was based on the F-2a heavy day fighter, but it carried a crew of two (the pilot and a rearward-facing radar operator) and was equipped with a FuG 240 “Berlin” radar set and a rotating dish antenna under a streamlined plywood cover in the nose. The armament consisted of four MK 108 under the nose, similar to the F-1a day fighter, plus two additional, upward-firing MK 108 cannon (“Schräge Musik”) in the rear fuselage.
Other proposed variants (with less priority, though) were the F-4 and the F-5, which were to become the basis for fast bombers and reconnaissance aircraft with only light defensive armament, typically only a pair of MG 131 in remote-controlled tail barbettes was to be carried. The F-4 resembled the baseline P.1099A, with two bomb bays in front of and behind the main landing gear wells and a crew of two seated side-by-side in a pressurized cockpit. Two MK 108 were carried in the nose, plus the MG 131 tail barbettes. The F-5 was similar but featured a glazed bomb aimer/navigator station in the nose instead of the MK 108’s and the glazing above the pilot’s station was reduced and asymmetrical. In both bomber variants the fuselage tanks were re-arranged to make room for a single SC 1.200 in the front bomb bay, but combinations of smaller bombs could be carried, too. Alternatively, mounts for up to three cameras or a 1.350 l auxiliary tank for extended range could be carried in the bays, too.
Initial flight tests of the Me 262 F in late 1944 showed severe directional instability: especially after fuel and ammunition had been depleted and the center of gravity shifted the aircraft tended to become nose-heavy and ditch down if it was not carefully monitored and trimmed by the pilot. To cope with this problem, the engine mounts were modified, so that the CoG was shifted back. Compared with the original Me 262 the engines were placed roughly 900 mm (35.5 in) further back under the wings. The emptying sequence of the fuselage tanks was also changed, and this mostly mended the problems. Another measure to mend the directional instability issues was the enlargement of the tail surfaces, even though later production aircraft frequently had smaller Me 262 A stabilizers fitted due to material shortages and simple lack of parts.- However, due to the higher weight the Me 262 F’s handling and agility were very limited – but most of its intended roles rather relied on speed, anyway, so that dogfights could be avoided.
From 1944 on the war situation worsened considerably, and production of the new Me 262 F superseded the A variant only on selected production lines. A disused mine complex under the Walpersberg mountain was adapted for the production of complete aircraft. These were hauled to the flat top of the hill where a runway had been cleared and flown out. Between 20 and 30 Me 262 Fs were built here until early 1946, primarily fighters, the underground factory being overrun by Allied troops before it could reach a meaningful output. Wings were produced in Germany's oldest motorway tunnel at Engelberg, to the west of Stuttgart. At B8 Bergkristall-Esche II, a vast network of tunnels was excavated beneath St. Georgen/Gusen, Austria, where fully equipped fuselages for the Me 262 at a planned monthly rate of 450 units on large assembly lines were to be produced from early 1945.
After the type’s introduction to frontline units in early 1945 further handling problems arose through the aircraft’ weight, resulting from its high wing load. Both starting and landing run were excessive, so that the number of airfields from which it could be operated was relatively small. No real short-term solution could be found without fully re-designing the wings, so that RATO bottles were frequently used to get a fully loaded Me 262 F up into the air from standard airfields. These were typically fitted to racks which were mounted under the fuselage, flanking the rear bomb bay.
The Me 262 F’s landing speed was dangerously high, too. A retrofittable brake parachute, housed in a simple tubular fairing under the tail, was developed to reduce the landing distance and save brakes, which frequently overheated and could set the landed aircraft aflame.
From the Me 262 F-2a “Pulkzerstörer I”, only a small number were built and eventually entered service. Its main armament, the MK 112, was a heavy German machine cannon produced by Rheinmetall-Borsig from 1945 on – in fact, the MK 112 was basically a scaled-up MK 108, a very compact weapon with relatively low weight. The MK 112 had a caliber of 55 mm and thus fired much larger shells than the 30 mm MK 108, but the rate of fire was significantly lower (300 rounds / min compared to about 600-660 rounds / min of the MK 108). This large-caliber gun was designed primarily to combat heavy bombers, its rate of fire would have been too slow for effective aerial battles with escort fighters – but the Me 262 F would not have been a dogfighter, anyway, so that the “hit-and-run” mission profile suited the aircraft well. Fire tests showed that a single MK 112 hit with mine grenades could destroy a bomber, and with a rate of fire of five shells per second this weapon could inflict considerably higher losses on the incoming streams of Allied bombers compared to other on-board weapons used on the German side. Only the unguided R4M missiles were as effective, but the MK 112 offered considerably higher accuracy and the opportunity to execute more than just a single attack run on an incoming bomber formation.
The MK 112 was mounted in the lower starboard section of the Me 262 F-2a’s nose, its barrel protruded more than 2 m (7 ft) from its nose. The gun’s drum magazine with sixty rounds partly took up the rear space of the cockpit behind the pilot and the gun mount even used up space of the weapon bay on port side, so that only a single MK 108 with 100 rounds as an additional weapon was mounted in the lower port side weapon bay.
Its sister, the Me 262 F-2b, remained on the drawing board, because its main weapon, the 50 mm MK 114 autocannon that had been derived from the 5 cm Pak 38 anti-tank gun, had turned out to be over-complicated, overweight and unreliable. A refined version was developed as the MK 214A, though, but after flight test from February 1945, but the weapon was not deployed operationally.
Only a handful Me 262 F-2a Pulkzerstörer were eventually fielded and operated before the end of hostilities – beyond the low production numbers the lack of fuel and loss of suitable airfields highly limited the aircraft’s potential. Probably less than ten were used by operational units, including JG 53 “Pik As”, in which they served alongside other interceptors, including other Me 262 variants. Typically, bomber formations were approached from the side of a bomber formation, where their silhouettes were widest, and while still out of range of the bombers' machine guns. This broadside-attack tactic was very effective, and the aircraft’s high speed allowed the interceptors to turn around 180° and make at least a second attack run from the opposite side, before the machines dashed off and returned to their bases.
General characteristics
Crew: One
Length: 14,32 m (46 ft 11 in) overall
12,00 m (39 ft 3¾ in) fuselage only, w/o brake parachute housing
Wingspan: 12,61 m (41 ft 3¾ in)
Height: 4,43 m (14 ft 6 in)
Wing area: 24,2 m² (236 sq ft)
Empty weight: 5.061 kg (11,148 lb)
Loaded weight: 8.762 kg (19,300 lb)
Max. take-off weight: 10.062 kg (22,163 lb)
Powerplant:
2× Junkers Jumo 004 C turbojets with 12 kN (2,697 lb st) each
Performance
Maximum speed: 930 km/h (577 mph, 505 kn)
Cruising speed: 805 km/h (500 mph, 438 kn) at 6.500 m (21,290 ft)
Range: 1.340 km (830 ml, 728 nm) at 6000 m with internal fuel only
Service ceiling: 11,450 m (37,570 ft)
Rate of climb: 18 m/s (3,540 ft/min) at max. weight
Armament:
1× 55 mm (1.96 in) MK 112 machine cannon with 60 rounds
1× 30 mm (1.18 in) MK 108 machine cannon with 100 rounds
Hardpoints under the outer wings for racks with twelve 55mm R4M unguided air-to-air missiles
The kit and its assembly:
This became a submission to the late 2021 “Gunships” group build at whatifmodellers.com – what would such a competition be without at least one gun-toting German Luft ’46 interceptor? The Messerschmitt P.1099 lent itself for such a build. Since 1996 Revell offers a 1:72 IP model kit of this paper aircraft, depicting more or less the two planned versions: a basic single-seat day fighter and a heavy two-seater Zerstörer, both based on the same basis.
This what-if model was based on Revell’s interpretation of the P.1099A, and the kit goes together well. Fit is very good, even though some designs are IMHO a bit dubious. The kit’s weakest point: Revell unfortunately missed the important detail of the modified engine nacelles: the kit comes with standard Me 262 wings and engines, but due to CoG reasons the P.1099 would have had its engines moved back by about 900 mm, as mentioned in the background. I corrected this on this build with some PSR – sounds simple, but since the nacelles are not expected to be stuck to the wings in their new position roughly 1 cm further back, some serious bodywork had to be done.
Otherwise the kit was basically built OOB. I just left away the inner wheels from the main landing gear because I found the twin wheels to be “too much” for this upgraded Me 262. The P.1099 might have been heavier than the Me 262, but…? And the wheels’ tractor-like tread design looks IMHO out of place, too, so that I replaced them with a pair of MiG-21 wheels, left over from a KP kit.
The cockpit was taken OOB, even though I have doubts concerning the canopy. And when you look at mockup pictures of the P.1099 you realize that cockpit access had been facilitated through a side door at starboard, similar to the D. H. Mosquito. The cockpit tub does not consider this hatch at all, and the engraved door on the fuselage (it’s actually there!) is so tiny that only a Halfling might use it?
Well, I stuck with it “as is” and just added a pilot figure (specifically from a Matchbox Hawker tempest, because it is one of the rare cases that you get a WWII pilot wearing an oxygen mask) and a “barrel” behind the bulbous pilot seat because there’s a lot of free space in this single seat variant that is otherwise occupied by a rear gunner in Revell’s P.1099B kit. I also have doubts concerning the kit’s canopy, since the original P.1099 had a cockpit for two seated side-by-side, with a canopy that resembled the D.H. Mosquito’s a lot. I am also not certain about the stabilizers – the kit comes with standard Me 262 parts, but trustworthy sources I consulted suggest that not only the fin had been enlarged (depicted well in Revell’s kit), but also the stabilizers? To improve this, I implanted a pair of modified stabilizers that came from a Heller PZL P.23 light bomber. Sounds odd, but they were a very good match in size, shape and thickness!
The only major modification concerns the armament, even though it became just a “graft-on” solution. On the lower left side, the upper gun port was PSRed away. On the right side I added a bulged fairing for the MK 112. It was sculpted from a Matchbox Saab J29 drop tank and blended into the hull with PSR. Protruding spent cases fairings were added for both guns. The MK 112 gun barrel is a resin piece, left over from a ModelTrans tank conversion set and actually depicts a German 55 mm gun, so that this became a perfect donor piece.
Since the airframe still looked rather clean and boring I finally added a pair of JATO bottle racks to the rear fuselage (scratched from styrene profile but left empty) and a brake parachute fairing under the fin, carved from a piece of sprue.
Furthermore, a display adapter was installed into the fuselage for in-flight pictures.
Painting and markings:
This became a challenge, because I wanted a rather unusual livery, neither a standard RLM 81/82/76 late-war combo nor an improvised-cammo-over-bare-metal finish. After some research I settled upon something that was actually carried by some He 177 bombers around 1944: a uniform RLM 74 (Graugrün, Humbrol 245) upper surface with “cloudy” mottles in RLM 76 (Humbrol 247). This appears like a winter camouflage, but it’s actually quite effective at medium altitude, esp. over a cloudy landscape. The original bombers had light blue (RLM 65) undersides, but for the P.1099 from a later period and as a fighter I rather used a darker shade of RLM76 in the form of Tamiya XF-23 (Light Blue). The model received a black ink washing and some post-panel-shading.
The cockpit interior became RLM 66 (Schwarzgrau, Humbrol 67) while the landing gear and the well were painted in uniform RLM 02 (I used Revell 45, a slightly more greenish tone), with wheel discs in RLM 66, too.
Unit markings became minimal and quite sober. I gave the aircraft a typical late-war “Reichsverteidigung” fuselage band, and in JG 53’s case it is plain black. The black band was deliberately chosen because it is a good, much darker contrast to the murky RLM 74, so that the latter appears lighter than it actually is, lowering the contrast to the RLM 76 spots.
The decals were puzzled together from various sources. As an aircraft of the 3rd group the unit’s ID color would be yellow, reflected in the tactical code and the fin tip. For some contrast and to emphasize the long gun barrel I gave it white and black stripes – as a security measure for ground handling. For some more variety I painted one air intake in very dark grey (Revell 06, Anthracite) and the other one in steel Metallizer, simulating replacement parts. The Balkenkreuze come from various sheets – I used simplified “low viz” versions all around. The undulating yellow bar for the 3rd group comes from a TL Modellbau sheet, while the yellow “4” came from a Fw 190 A sheet from Sky Models. A small “4” on the nose was added as a wacky detail, too, the “Pik As” unit markings came IIRC from a Hobby Boss Bf 109 sheet. Since they turned out to have poor contrast/opacity I only used a few stencils from the P.1099A sheet, but due to the disruptive paint scheme this is not apparent.
Finally, the model was sealed with a coat of matt acrylic varnish (Italeri) and a wire antenna, scratched from heated black sprue material, was added between cockpit and fin.
Well, this modified Messerschmitt P.1099A looks simple, but the modified engine nacelles as well as the gun fairing under the nose called for serious PSR. The result looks quite natural, though, and AFAIK this weapon configuration was actually on German drawing boards. However, I am not certain about the cockpit canopy and other details on Revell’s kit, reference information is contradictive.
The paint scheme looks good, even though it was lent from a heavy bomber, and the poor Humbrol enamels did not yield a finish that I had hoped for – the paintwork could certainly have been better, but the overall impression of a late-war Pulkzerstörer is O.K., and this eventually counts.
The NROL-61 mission for the National Reconnaissance Office, encapsulated inside a 4-meter payload fairing, is mated to its United Launch Alliance (ULA) Atlas V booster inside the Vertical Integration Facility (VIF) at Cape Canaveral's Space Launch Complex-41. Photo credit: United Launch Alliance
When I saw this on the shores of the Moskva River in the middle of Moscow, I thought that one of the American space shuttles had ended up being displayed here. What I didn't know is that the Soviet Union had its own space shuttle program called Buran which used spacecraft that were very similar to the American space shuttles, at least from the outside.
The Soviets decided to develop their own space shuttle program in the 1980's when they realized that the American space shuttles could carry enough military payload, possibly including nuclear weapons, and deploy them over Soviet territory, that it would constitute a major threat to their security. The Buran program had no civilian objectives, only military.
The Buran experiment was limited to one orbital flight, unmanned, which took place on November 15, 1988. The flight was a success and was the only shuttle-type spacecraft to fly unmanned, including landing in full automatic mode. The program was discontinued in 1993 after the disintegration of the Soviet Union as it was deemed unnecessary since the Cold War and the military hardware competition that came with it was pretty well over. That particular spacecraft, the one that flew, was destroyed in a massive storm that caused the collapse of the hangar where it was being kept in Kazakhstan. The one photographed here is a prototype that never flew.
Vice President Mike Pence, right, and Rep. Robert Aderholt, R-Ala., talk with Expedition 53 crew members Joe Acaba, Randy Bresnik, and Mark Vande Hei onboard the International Space Station from the Payload Operations Integration Center (POIC) of the NASA Marshall Space Flight Center, Monday, Sept. 25, 2017 in Huntsville, Alabama. The Vice President visited the space center to view test hardware for NASA’s Space Launch System, America’s new deep space rocket and to call the crew onboard the International Space Station. Photo Credit: (NASA/Bill Ingalls)
The third BARREL balloon--detached from the payload--ended up draped over trees near Svappavaara, Sweden, about 35 miles from the original launch site. The team recovered the balloon and payload on Aug. 19, 2015, two days after its 16-hour flight.
The NASA-funded BARREL – which stands for Balloon Array for Radiation-belt Relativistic Electron Losses – measures electrons in the atmosphere near the poles. Such electrons rain down into the atmosphere from two giant radiation belts surrounding Earth, called the Van Allen belts. For its third campaign, BARREL is launching six balloons from the Esrange Space Center in Kiruna, Sweden. BARREL is led by Dartmouth College in Hanover, New Hampshire.
Credit: NASA/Dartmouth/Alexa Halford
The BARREL team carries their third balloon payload back to their vehicle. After collecting data for nearly 16 hours, the box containing the scientific instruments floated gently back to Earth. Recovery was especially important for this balloon, since it carried a student-designed magnetometer--an instrument for measuring magnetic fields--and all of its recorded data.
The NASA-funded BARREL – which stands for Balloon Array for Radiation-belt Relativistic Electron Losses – measures electrons in the atmosphere near the poles. Such electrons rain down into the atmosphere from two giant radiation belts surrounding Earth, called the Van Allen belts. For its third campaign, BARREL is launching six balloons from the Esrange Space Center in Kiruna, Sweden. BARREL is led by Dartmouth College in Hanover, New Hampshire.
Credit: NASA/Dartmouth/Alexa Halford
Locations of DNA application on the TEXUS-49 payload.a Scheme of the TEXUS-49 payload with DNA sample 1–12 application sites b Plasmid DNA samples 1–12 were applied on the outside of the TEM (TEXUS Experiment Module) EML 4 .cI DNA samples 1–4 were applied circular at 0, 90, 180, 270 degree directly on the surface of the payload. DNA samples 5–12 were also applied with a distance of 90 degree each in the screw heads of the payload .cII DNA samples 13–15 were applied directly on the payload surface at the bottom side .d DNA samples 1–4 were pipetted directly on the surface and locations were marked with a pen .e DNA samples 5–12 were applied in the grooves of the screw heads .f DNA samples 13–15 were applied directly on the payload surface on the bottom side and locations were marked with a pen.
The BARREL team prepares their fifth balloon and payload for launch. The white box in the foreground is an air traffic control transponder and positioning unit. The main payload (not visible in the picture) contains instruments to measure the number of electrons raining down from the swaths of trapped charged particles above Earth, known as the Van Allen Belts. The orange and white fabric is a parachute that will help the payload float gently to Earth after it is detached from the translucent balloon.
The NASA-funded BARREL – which stands for Balloon Array for Radiation-belt Relativistic Electron Losses – measures electrons in the atmosphere near the poles. For its third campaign, BARREL is launching six balloons from the Esrange Space Center in Kiruna, Sweden. BARREL is led by Dartmouth College in Hanover, New Hampshire.
Credit: NASA/Dartmouth/Alexa Halford
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• • • • •
See more photos of this, and the Wikipedia article.
Details, quoting from Smithsonian National Air and Space Museum | Space Shuttle Enterprise:
Manufacturer:
Rockwell International Corporation
Country of Origin:
United States of America
Dimensions:
Overall: 57 ft. tall x 122 ft. long x 78 ft. wing span, 150,000 lb.
(1737.36 x 3718.57 x 2377.44cm, 68039.6kg)
Materials:
Aluminum airframe and body with some fiberglass features; payload bay doors are graphite epoxy composite; thermal tiles are simulated (polyurethane foam) except for test samples of actual tiles and thermal blankets.
The first Space Shuttle orbiter, "Enterprise," is a full-scale test vehicle used for flights in the atmosphere and tests on the ground; it is not equipped for spaceflight. Although the airframe and flight control elements are like those of the Shuttles flown in space, this vehicle has no propulsion system and only simulated thermal tiles because these features were not needed for atmospheric and ground tests. "Enterprise" was rolled out at Rockwell International's assembly facility in Palmdale, California, in 1976. In 1977, it entered service for a nine-month-long approach-and-landing test flight program. Thereafter it was used for vibration tests and fit checks at NASA centers, and it also appeared in the 1983 Paris Air Show and the 1984 World's Fair in New Orleans. In 1985, NASA transferred "Enterprise" to the Smithsonian Institution's National Air and Space Museum.
Transferred from National Aeronautics and Space Administration
• • •
Quoting from Wikipedia | Space Shuttle Enterprise:
The Space Shuttle Enterprise (NASA Orbiter Vehicle Designation: OV-101) was the first Space Shuttle orbiter. It was built for NASA as part of the Space Shuttle program to perform test flights in the atmosphere. It was constructed without engines or a functional heat shield, and was therefore not capable of spaceflight.
Originally, Enterprise had been intended to be refitted for orbital flight, which would have made it the second space shuttle to fly after Columbia. However, during the construction of Columbia, details of the final design changed, particularly with regard to the weight of the fuselage and wings. Refitting Enterprise for spaceflight would have involved dismantling the orbiter and returning the sections to subcontractors across the country. As this was an expensive proposition, it was determined to be less costly to build Challenger around a body frame (STA-099) that had been created as a test article. Similarly, Enterprise was considered for refit to replace Challenger after the latter was destroyed, but Endeavour was built from structural spares instead.
Service
Construction began on the first orbiter on June 4, 1974. Designated OV-101, it was originally planned to be named Constitution and unveiled on Constitution Day, September 17, 1976. A write-in campaign by Trekkies to President Gerald Ford asked that the orbiter be named after the Starship Enterprise, featured on the television show Star Trek. Although Ford did not mention the campaign, the president—who during World War II had served on the aircraft carrier USS Monterey (CVL-26) that served with USS Enterprise (CV-6)—said that he was "partial to the name" and overrode NASA officials.
The design of OV-101 was not the same as that planned for OV-102, the first flight model; the tail was constructed differently, and it did not have the interfaces to mount OMS pods. A large number of subsystems—ranging from main engines to radar equipment—were not installed on this vehicle, but the capacity to add them in the future was retained. Instead of a thermal protection system, its surface was primarily fiberglass.
In mid-1976, the orbiter was used for ground vibration tests, allowing engineers to compare data from an actual flight vehicle with theoretical models.
On September 17, 1976, Enterprise was rolled out of Rockwell's plant at Palmdale, California. In recognition of its fictional namesake, Star Trek creator Gene Roddenberry and most of the principal cast of the original series of Star Trek were on hand at the dedication ceremony.
Approach and landing tests (ALT)
Main article: Approach and Landing Tests
On January 31, 1977, it was taken by road to Dryden Flight Research Center at Edwards Air Force Base, to begin operational testing.
While at NASA Dryden, Enterprise was used by NASA for a variety of ground and flight tests intended to validate aspects of the shuttle program. The initial nine-month testing period was referred to by the acronym ALT, for "Approach and Landing Test". These tests included a maiden "flight" on February 18, 1977 atop a Boeing 747 Shuttle Carrier Aircraft (SCA) to measure structural loads and ground handling and braking characteristics of the mated system. Ground tests of all orbiter subsystems were carried out to verify functionality prior to atmospheric flight.
The mated Enterprise/SCA combination was then subjected to five test flights with Enterprise unmanned and unactivated. The purpose of these test flights was to measure the flight characteristics of the mated combination. These tests were followed with three test flights with Enterprise manned to test the shuttle flight control systems.
Enterprise underwent five free flights where the craft separated from the SCA and was landed under astronaut control. These tests verified the flight characteristics of the orbiter design and were carried out under several aerodynamic and weight configurations. On the fifth and final glider flight, pilot-induced oscillation problems were revealed, which had to be addressed before the first orbital launch occurred.
On August 12, 1977, the space shuttle Enterprise flew on its own for the first time.
Preparation for STS-1
Following the ALT program, Enterprise was ferried among several NASA facilities to configure the craft for vibration testing. In June 1979, it was mated with an external tank and solid rocket boosters (known as a boilerplate configuration) and tested in a launch configuration at Kennedy Space Center Launch Pad 39A.
Retirement
With the completion of critical testing, Enterprise was partially disassembled to allow certain components to be reused in other shuttles, then underwent an international tour visiting France, Germany, Italy, the United Kingdom, Canada, and the U.S. states of California, Alabama, and Louisiana (during the 1984 Louisiana World Exposition). It was also used to fit-check the never-used shuttle launch pad at Vandenberg AFB, California. Finally, on November 18, 1985, Enterprise was ferried to Washington, D.C., where it became property of the Smithsonian Institution.
Post-Challenger
After the Challenger disaster, NASA considered using Enterprise as a replacement. However refitting the shuttle with all of the necessary equipment needed for it to be used in space was considered, but instead it was decided to use spares constructed at the same time as Discovery and Atlantis to build Endeavour.
Post-Columbia
In 2003, after the breakup of Columbia during re-entry, the Columbia Accident Investigation Board conducted tests at Southwest Research Institute, which used an air gun to shoot foam blocks of similar size, mass and speed to that which struck Columbia at a test structure which mechanically replicated the orbiter wing leading edge. They removed a fiberglass panel from Enterprise's wing to perform analysis of the material and attached it to the test structure, then shot a foam block at it. While the panel was not broken as a result of the test, the impact was enough to permanently deform a seal. As the reinforced carbon-carbon (RCC) panel on Columbia was 2.5 times weaker, this suggested that the RCC leading edge would have been shattered. Additional tests on the fiberglass were canceled in order not to risk damaging the test apparatus, and a panel from Discovery was tested to determine the effects of the foam on a similarly-aged RCC leading edge. On July 7, 2003, a foam impact test created a hole 41 cm by 42.5 cm (16.1 inches by 16.7 inches) in the protective RCC panel. The tests clearly demonstrated that a foam impact of the type Columbia sustained could seriously breach the protective RCC panels on the wing leading edge.
The board determined that the probable cause of the accident was that the foam impact caused a breach of a reinforced carbon-carbon panel along the leading edge of Columbia's left wing, allowing hot gases generated during re-entry to enter the wing and cause structural collapse. This caused Columbia to spin out of control, breaking up with the loss of the entire crew.
Museum exhibit
Enterprise was stored at the Smithsonian's hangar at Washington Dulles International Airport before it was restored and moved to the newly built Smithsonian's National Air and Space Museum's Steven F. Udvar-Hazy Center at Dulles International Airport, where it has been the centerpiece of the space collection. On April 12, 2011, NASA announced that Space Shuttle Discovery, the most traveled orbiter in the fleet, will be added to the collection once the Shuttle fleet is retired. When that happens, Enterprise will be moved to the Intrepid Sea-Air-Space Museum in New York City, to a newly constructed hangar adjacent to the museum. In preparation for the anticipated relocation, engineers evaluated the vehicle in early 2010 and determined that it was safe to fly on the Shuttle Carrier Aircraft once again.