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
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DESIGNER
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OKB Sukhoi
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|---|---|
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COUNTRY
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Russia
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TYPE
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Interceptor
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CREW
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1
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POWER-PLANT
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Two jet engine R-13F2-300
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Thrust, kgf
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2 x 6.600
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DIMENSIONS
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Length, m
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21,41
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Height, m
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4,84
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Wing span, m
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9,34
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Wing area, m2
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36,60
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WEIGHT
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|
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Empty aircraft, kg
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10.760
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Normal take-off, kg
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17.200
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Maximum take-off, kg
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17.900
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Internal fuel, kg
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6.460
|
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PERFORMANCE
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|
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Maximum speed, km/h
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2.230
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Max speed in low height, km/h
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1.300
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Range, km
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2.500
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Combat range, km
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1.250
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Service ceiling, m
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18.500
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| 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
