Sukhoi Su-7

Airplanes

Length

16.8 m

Flat Wing Span

9.31 m

Height

4.99 m

Flat Wing Area

34 m²

Max Speed

1150 km/h

Max Ceiling

17600 m

Number of Engines

First Flight

1955-09-07

Entry Into service

1959-01-01

Number Built

1847

Maximum Take-Off Weight

15.21 t (paragliders: kg)

Maximum Range

1650 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Sukhoi Su-7	15.21	1650

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
IAR 95	Tumansky R-29	16	9.3	Compare
Lockheed CL-1200 Lancer	Pratt & Whitney TF30	17.45	8.89	Compare
Vought F-8 Crusader		16.764	10.668	Compare
Douglas F5D Skylancer		16.1544	10.0584	Compare
Vought Model 1600		16	10.1	Compare
Chengdu J-10		16.9	9.8	Compare

All data (26 fields)

Name: Sukhoi Su-7
Manufacturer: Sukhoi Civil Aircraft
Description: The Sukhoi Su-7 (NATO designation name: Fitter-A) is a swept wing, supersonic fighter aircraft developed by the Soviet Union in 1955.
ICAO Code: SU7
First Flight: 1955-09-07
Entry Into service: 1959-01-01
Production End: 1972-01-01
Designer: Sukhoi Civil Aircraft
Type: Fighter and fighter-bomber / ground-attack aircraft
Length (m): 16.8
Height (m): 4.99
Cockpit Crew: 1
Max Speed (km/h): 1150
Max Ceiling (m): 17600
Rate of Climb (m/s): 160
Armament: 2 × 30 mm Nudelman-Rikhter NR-30 autocannons (70 rounds per gun, 140 rounds total); 4 × under-wing & 2 × under-fuselage stations for 2000 kg of disposable stores. 2 × reserved for 2300 L drop tanks
National Origin: Soviet Union
Number Built: 1847
Powerplant Description: 1 × Lyulka AL-7F-1 afterburning turbojet, 66.6 kN thrust each
Primary Users: Soviet Air Forces (historical), Indian Air Force (historical); North Korean Air Force
Status: In limited service with the Korean People's Army Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Sukhoi_Su-7
Flat Wing Span (m): 9.31
Flat Wing Area (m²): 34
Wake Category: M
Number of Engines: 1