General Dynamics–Grumman F-111B
Maximum Take-Off Weight
39.9 t (paragliders: kg)
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Aircraft Weight Variants
All data (20 fields)
- Name
- General Dynamics–Grumman F-111B
- Manufacturer
- Grumman
- Description
- The General Dynamics–Grumman F-111B is a long-range carrier-based interceptor aircraft planned as a follow-up to the McDonnell Douglas F-4 Phantom II for the United States Navy (USN).
- First Flight
- 1965-05-18
- Designer
- Grumman
- Length (m)
- 20.98
- Height (m)
- 4.8
- Cockpit Crew
- 2
- Max Speed (km/h)
- 2655
- Max Ceiling (m)
- 19800
- Rate of Climb (m/s)
- 108
- Armament
- 1× M61 Vulcan 20 mm (0.787 in) Gatling cannon (seldom fitted); 6 × AIM-54 Phoenix long range air-air missiles (four under wings, two in weapons bay); 6 underwing pylons for ordnance and external fuel tanks
- Max Mach (Mach)
- 2.5
- National Origin
- United States of America
- Number Built
- 7
- Powerplant Description
- 2 × Pratt & Whitney TF30-P-12 turbofans, 47.8 kN thrust each
- Primary Users
- United States Navy
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/General_Dynamics%E2%80%93Grumman_F-…
- Aircraft Engine
- Pratt & Whitney TF30
- Number of Engines
- 2