Overview
The Grumman X-29 was an experimental aircraft developed to test forward-swept wing technology and advanced control systems. Designed as a research platform, it demonstrated innovative materials and fly-by-wire control. The aircraft provided valuable aerodynamic data during its test program.
Live Fleet Activity (X29)
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Specifications
Units
- Engine
- 1 × General Electric F404 turbofan
- Engine type
- Turbofan
- Thrust
- 16,000 lbf · 71 kN
- Avionics
- Litton LR-80 AHRS, Magnavox AN/ARC-164 UHF, Teledyne RT-1063B/APX-101V IFF/SIF
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 53 ft 10 in · 16.40 m
- Tail height
- 14 ft 3 in · 4.35 m
- Fuselage diameter
- 3 ft 7 in · 1.10 m
- Wing span
- 27 ft 2 in · 8.29 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 17,800 lb · 8,050 kg
- Max landing weight
- —
- Max payload
- 4,000 lb · 1,800 kg
- Fuel capacity
- 590 gal · 2,200 L · 1,800 kg (Jet A)
- Max cruise speed
- 956 kt · 1,100 mph · 1,771 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 350 nm · 400 mi · 650 km
- Fuel burn
- 0.45 nm/gal · 0.22 km/L
- Ceiling
- 55,000 ft · 16,800 m
- Rate of climb
- —
- Takeoff distance
- —
- Landing distance
- —
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Live fleet activity details
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