Overview
The North American F-100 Super Sabre was the first U.S. Air Force fighter capable of sustained supersonic flight in level flight. Introduced in the 1950s, it marked a major step beyond the F-86 Sabre. The aircraft later evolved into a fighter-bomber with extensive combat service in Southeast Asia.
Live Fleet Activity (F100)
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Specifications
Units
- Engine
- 1 × Pratt & Whitney J57-P-21/21A
- Engine type
- Jet
- Thrust
- 16,000 lbf · 71 kN
- Avionics
- Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 49 ft 3 in · 15.00 m
- Tail height
- 16 ft 3 in · 4.95 m
- Fuselage diameter
- 5 ft 3 in · 1.60 m
- Wing span
- 38 ft 9 in · 11.80 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 34,800 lb · 15,800 kg
- Max landing weight
- 34,400 lb · 15,600 kg
- Max payload
- 7,050 lb · 3,200 kg
- Fuel capacity
- 2,600 gal · 9,900 L · 7,900 kg (Jet A)
- Max cruise speed
- 803 kt · 924 mph · 1,487 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 162 kt · 186 mph · 300 km/h
- Range
- 1,734 nm · 2,000 mi · 3,210 km
- Fuel burn
- —
- Ceiling
- 50,000 ft · 15,200 m
- Rate of climb
- 22,400 ft/min · 114 m/s
- Takeoff distance
- —
- Landing distance
- —
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Live fleet activity details
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