Su-15 Flagot Interceptor. First flight: 1963 © Konstantinos Panitsidis

Photos from the personal collection of Kostas Panitsidis


 Technical specifications      Photos      Video

 

 

Mission: Interceptor of airborne assets of offence. Chief designers: E.A. Ivanov, N.P. Polenov

Delivered by Novosibirsk aircraft plant in 1966-1971. In service with Soviet Air Defence Aviation in 1967-1993. 

Exhibited is a prototype (designated in Design Bureau as T58L) involved in the test program to develop take-off and landing techniques for the aircraft with ski landing gear operated on soft airfields. 

Aircraft versions: Su-15T, Su-15TM, Su-15U.

 


THREE-VIEW DRAWING

 


TECHNICAL SPECIFICATIONS

DESIGNER
OKB Sukhoi
COUNTRY
Russia
TYPE
Interceptor
CREW
1
POWER-PLANT
Two jet engine R-13F2-300
Thrust, kgf
2 x 6.600
DIMENSIONS
 
Length, m
21,41
Height, m
4,84
Wing span, m
9,34
Wing area, m2
36,60
WEIGHT
 
Empty aircraft, kg
10.760
Normal take-off, kg
17.200
Maximum take-off, kg
17.900
Internal fuel, kg
6.460
PERFORMANCE
 
Maximum speed, km/h
2.230
Max speed in low height, km/h
1.300
Range, km
2.500
Combat range, km
1.250
Service ceiling, m
18.500
ARMAMENT 2 x R-98 and 4xR-60M or K-8.  
2 x pods UPK-23-250 with 23 (30) mm cannons GSh-23L (250 rounds). Two bombs FAB-250.

 


PHOTOS  Su-15