Hobby Master HA4446 USAF Lockheed-Martin F-35A Lightning II Joint Strike Fighter - 18-5343, 20th Operations Group, 20th Fighter Wing, Alaska, 2020s [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 attached to the 20th Operations Group, 20th Fighter Wing, then deployed to Alaska during the 2020s.
Now in stock!
Dimensions:
Wingspan: 5-3/4-inches
Length: 8-1/2-inches
Release Date: July 2025
Historical Account: "White Wedding Day" - The 20th Operations Group (20 OG) is the flying component of the 20th Fighter Wing, assigned to the United States Air Force Air Combat Command. It is stationed at Shaw Air Force Base, South Carolina. It is a successor organization of the 20th Pursuit Group, one of the 15 original combat air groups formed by the U.S. Army before World War II.
During World War II the 20th Fighter Group was an Eighth Air Force fighter unit stationed in the United Kingdom. It arrived at RAF Kings Cliffe in 1943. It was the oldest USAAF group to be assigned to the Eighth Air Force for an extended period, flying 312 combat missions. It was awarded a Distinguished Unit Citation for a sweep over Germany on April 8th, 1944.
Today the group mobilizes, deploys, flies, and fights approximately 80 F-16CJ Fighting Falcon fighter aircraft. It can carry out conventional air-to-surface, air superiority, suppression of enemy air defenses, destruction of enemy air defenses and maritime operations.
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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