Hobby Master HA4405 USAF Lockheed-Martin F-35A Lightning II Joint Strike Fighter - 422nd Test and Evaluation Squadron "Green Bats", 53rd Test and Evaluation Group, Spring 2013 [Low-Vis Scheme] (1:72 Scale)
"The F-35 program executive officer, has stated that the 'F-35 enjoys a significant Combat Loss Exchange Ratio advantage over the current and future air-to-air threats, to include Sukhois, which are currently being flown by the Russian, Indian, and Chinese Air Forces.'"
- Maj Gen Charles R. Davis, USAF, the F-35 program executive officer
The Lockheed Martin F-35 Lightning II is a fifth-generation, single-seat, single-engine, stealth-capable military strike fighter, a multirole aircraft that can perform close air support, tactical bombing, and air superiority fighter missions. The F-35 has three different models; one is the conventional takeoff and landing variant, the second is short takeoff and vertical-landing variant, and the third is a carrier-based variant.
The F-35 is descended from the X-35, the product of the Joint Strike Fighter (JSF) program. Its development is being principally funded by the United States, with the United Kingdom, and other partner governments providing additional funding. It is being designed and built by an aerospace industry team led by Lockheed Martin with Northrop Grumman and BAE Systems as major partners. Demonstrator aircraft flew in 2000, with the first flight on December 15th, 2006.
The F-35A is the conventional take-off and landing (CTOL) variant intended for the USAF and other air forces. It is the smallest, lightest version and capable of 9 g, the highest of all variants.
Although the F-35A currently conducts aerial refueling via boom and receptacle method, the aircraft can be modified for probe-and-drogue refueling if needed by the customer. A drag chute pod can be installed on the F-35A, with the Royal Norwegian Air Force being the first operator to adopt it.
Pictured here is a 1:72 scale replica of a USAF Lockheed-Martin F-35A Lightning II Joint Strike Fighter that was operated by the 56th Fighter Wing, then deployed to Luke Air Force Base during March 2014.
Sold Out!
Dimensions:
Wingspan: 5-3/4-inches
Length: 8-1/2-inches
Release Date: March 2015
Historical Account: "Test Taking" - The 422d Test and Evaluation Squadron (422 TES) is a United States Air Force unit. It is assigned to the 53d Test and Evaluation Group, stationed at Nellis Air Force Base, Nevada. The squadron performs operational testing of all fighter aircraft and munitions entering and in operational use by Air Combat Command (ACC).
The unit was originally formed as the 422d Night Fighter Squadron in 1943. After training in the United States, it was deployed to Ninth Air Force in England in the spring of 1944, prior to the D-Day landings in France. During the run-up to D-Day, the squadron trained with Royal Air Force night fighter units against Luftwaffe raiders who intruded the night skies over England. It was the first American squadron in England equipped with the Northrop P-61 Black Widow night fighter. After the landings in France, the mission of the squadron became the air defense of Allied liberated territory. During the Battle of the Bulge, it also flew day and night interdiction missions against enemy troop movements, bridges and other targets of opportunity. It was inactivated shortly after the war in Europe ended.
In 1969, the squadron was re-activated at Nellis Air Force Base by Tactical Air Command to provide combat evaluation and operational testing of new USAF aircraft entering the inventory after developmental testing was completed at Edwards AFB.
General characteristics Crew: 1 - Length: 51.4 ft (15.67 m)
- Wingspan: 35 ft (10.7 m)
- Height: 14.2 ft (4.33 m)
- Wing area: 460 ft (42.7 m)
- Empty weight: 29,300 lb (13,300 kg)
- Loaded weight: 44,400 lb (20,100 kg)
- Max takeoff weight: 70,000 lb (31,800 kg)
- Powerplant: 1 Pratt & Whitney F135 afterburning turbofan
- Dry thrust: 28,000 lbf (125 kN)
- Thrust with afterburner: 43,000 lbf[256] (191 kN)
- Internal fuel: 18,480 lb (8,382 kg)
- Performance
Maximum speed: Mach 1.67 (1,283 mph, 2,065 km/h) - Range: 1,200 nmi (2,220 km) on internal fuel
- Combat radius: 610 nmi (1,110 km) on internal fuel
- Service ceiling: 60,000 ft (18,288 m)
- Rate of climb: classified (not publicly available)
- Wing loading: 91.4 lb/ft² (446 kg/m²)
- Thrust/weight:
With full fuel: 0.84; - With 50% fuel: 1.04 B:
- g-Limits: 9 g
- Armament
Guns: 1 GAU-22/A 25 mm (0.984 in) cannon internally with 180 rounds - Hardpoints: 6 external pylons on wings with a capacity of 15,000 lb (6,800 kg) and 2 internal bays with 2 pylons each[60] for a total weapons payload of 18,000 lb (8,100 kg) and provisions to carry combinations of:
- Missiles:
Air-to-air: AIM-120 AMRAAM, AIM-132 ASRAAM, AIM-9X Sidewinder, IRIS-T - Air-to-ground: AGM-154 JSOW, AGM-158 JASSM
- Bombs:
Mark 84, Mark 83 and Mark 82 GP bombs - Mk.20 Rockeye II cluster bomb
- Wind Corrected Munitions Dispenser capable
- Paveway-series laser-guided bombs
- Small Diameter Bomb (SDB)
- JDAM-series
- B61 nuclear bomb (in 2017)
- Avionics
Northrop Grumman Electronic Systems AN/APG-81 AESA radar - Differences across variants
- ^ B is the same, C: 14.9 ft (4.54 m)
- ^ C is same, B: 60,000 lb (27,000 kg)
- ^ F-35B: 14,003 lb (6,352 kg); F-35C: 20,085 lb (9,110 kg)
- ^ F-35B: 7.5 g, F-35C: 7.5 g
- ^ fitted as an external pod with 220 rounds in the F-35B and F-35C
Wingspan: 5-3/4-inches Length: 8-1/2-inches
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