Sukhoi Su-15

Airplanes

Length

19.56 m

Flat Wing Span

9.43 m

Height

4.84 m

Flat Wing Area

36.6 m²

Max Speed

2230 km/h

Max Mach

2.1 Mach

Max Ceiling

18100 m

Number of Engines

Aircraft Engine

First Flight

1962-05-30

Entry Into service

1965-01-01

Number Built

1290

Maximum Take-Off Weight

17.9 t (paragliders: kg)

Maximum Range

1380 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Sukhoi Su-15	17.9	1380

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Shenyang J-8		21.39	9.344	Compare
Saab 36	Rolls-Royce Olympus	17	9.6	Compare
SEPECAT Jaguar		16.83	8.69	Compare
North American X-10		23.4696	8.5344	Compare
English Electric Lightning		16.764	10.3632	Compare
Northrop YF-17		16.764	10.668	Compare

All data (29 fields)

Name: Sukhoi Su-15
Manufacturer: Sukhoi Civil Aircraft
Description: The Sukhoi Su-15 (NATO reporting name: Flagon) is a twinjet supersonic interceptor aircraft developed by the Soviet Union.
ICAO Code: SU15
First Flight: 1962-05-30
Entry Into service: 1965-01-01
Production End: 1979-01-01
Service End: 1996-01-01
Designer: Sukhoi Civil Aircraft
Type: Interceptor aircraft
Length (m): 19.56
Height (m): 4.84
Cockpit Crew: 1
Max Speed (km/h): 2230
Max Ceiling (m): 18100
Rate of Climb (m/s): 228
Armament: 2 × UPK-23 gun pods with 2 × 23 mm Gryazev-Shipunov GSh-23L autocannons each on fuselage pylons; 6 hardpoints
Max Mach (Mach): 2.1
National Origin: Soviet Union
Number Built: 1290
Powerplant Description: 2 × Tumansky R-13F-300 afterburning turbojet engines, 40.21 kN thrust each
Primary Users: Soviet Air Defence Forces (historical), Russian Air Force (historical) , Ukrainian Air Force (historical)
Status: Retired from military service
Wikipedia Article (URL): en.wikipedia.org/wiki/Sukhoi_Su-15
Flat Wing Span (m): 9.43
Flat Wing Area (m²): 36.6
Wake Category: M
Aircraft Engine: Tumansky R-13
Number of Engines: 2