North American F-107

Airplanes

Length

18.85 m

Flat Wing Span

11.15 m

Height

5.89 m

Flat Wing Area

35 m²

Max Speed

2084.101 km/h

Max Mach

2 Mach

Max Ceiling

16220 m

Number of Engines

Aircraft Engine

First Flight

1956-09-10

Number Built

Maximum Take-Off Weight

18.841 t (paragliders: kg)

Maximum Range

3885 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
North American F-107	18.841	3885

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Yakovlev Yak-141		18.36	10.105	Compare
Dassault Mirage F2	Pratt & Whitney TF30	17.6	10.5	Compare
Saab 37 Viggen		16.4	10.6	Compare
Yakovlev Yak-201	Saturn AL-31	19	11.7	Compare
McDonnell F3H Demon		17.9832	10.668	Compare
CAMS 120		17.3	11.6	Compare

All data (24 fields)

Name: North American F-107
Manufacturer: North American Aviation
Description: The North American F-107 is a prototype aircraft that was North American Aviation's entry in a United States Air Force tactical fighter-bomber design competition of the 1950s, based on the F-100 Super Sabre.
First Flight: 1956-09-10
Service End: 1957-11-25
Designer: North American Aviation
Type: Fighter-bomber
Length (m): 18.85
Height (m): 5.89
Max Speed (km/h): 2084.101
Max Ceiling (m): 16220
Rate of Climb (m/s): 203
Armament: 4x 20 mm Pontiac M39 cannon OR 1x 20 mm, 6 barrel M61 Vulcan autocannon; 10,000 lb (4,500 kg) on 5 hardpoints; 2 under each wing, 1 semi-recessed ordnance station under fuselage centerline. Wide variety of ordnance, including tactical nuclear weapons
Max Mach (Mach): 2
National Origin: United States of America
Number Built: 3
Powerplant Description: 1 × Pratt & Whitney YJ75-P-9 turbojet, 109 kN thrust each
Primary Users: United States Air Force, NACA
Status: Canceled
Wikipedia Article (URL): en.wikipedia.org/wiki/North_American_F-107
Flat Wing Span (m): 11.15
Flat Wing Area (m²): 35
Aircraft Engine: Pratt & Whitney J75
Number of Engines: 1