Grumman G-118

Source: Wikipedia, the free encyclopedia.
G-118
Role Fighter aircraft
Manufacturer Grumman
Status Not built[1]
Primary user United States Navy (intended)

The Grumman G-118 (sometimes called the XF12F, though this was never official

F-14 Tomcat
, ordered in 1968.

Design

The Grumman Design 118 was a two-seat,

supersonic fighter aircraft. It had a 45° swept wing, a "T-tail" empennage, two small folding ventral fins, and a landing gear of tricycle configuration. For ejection, the tandem crew were encapsulated and ejected downwards. It also featured a boundary layer control system
to improve low speed handling.

The G-118 was to be powered by two J79-GE-3 engines, with accommodations for the more powerful

J79-GE-207 engines each producing 18,000 lbf of afterburning thrust. Similar to the contemporary Vought XF8U-3 Crusader III, it was designed with an additional throttleable liquid-fueled rocket engine using a mixture of JP-4 fuel and hydrogen peroxide oxidizer which produced 5,000 lbf of thrust.[3]

Armament stores would have been under the fuselage in two semi-recessed hardpoints for the AIM-7 Sparrow air-to-air missile and an internal weapons bay for an additional AIM-7 or three AIM-9 Sidewinder missiles.

Specifications (G-118, as designed)

Data from [1] and Standard Aircraft Characteristics[3]

General characteristics

  • Crew: 2
  • Length: 57 ft 7 in (17.55 m)
  • Wingspan: 43 ft 11.69 in (13.4033 m)
  • Height: 14 ft 10 in (4.52 m)
  • Wing area: 595 sq ft (55.3 m2)
  • Empty weight: 26,355 lb (11,954 kg)
  • Gross weight: 37,366 lb (16,949 kg)
  • Max takeoff weight: 51,216 lb (23,231 kg)
  • Powerplant: 2 × J79-GE-3 after-burning turbojet engines, 10,000 lbf (44 kN) thrust each dry, 15,600 lbf (69 kN) with afterburner
  • Powerplant: 1 × throttleable rocket engine, 5,000 lbf (22 kN) thrust

Performance

  • Maximum speed: Mach 2
  • Range: 1,352 nmi (1,556 mi, 2,504 km)
  • Service ceiling: 60,000 ft (18,288 m)
  • Wing loading: 62.8 lb/sq ft (307 kg/m2)

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ a b Angelucci, 1987. p. 251.
  2. ^ Buttler p. 126
  3. ^ a b "Standard Aircraft Characteristics: Design 118" (PDF). Grumman. 12 December 1955. Retrieved 22 December 2018.

Bibliography

External links