R-15B-300 aircraft turbojet engine
It is designed of power reconnaissance aircraft MIG 25 and MIG 25RB (with long ejector doors nozzle) and interceptor MIG 25 FP (with short ejector doors nozzle) Main advantages of the R-15B-300 engine:
• High reliability, maneuverability, high combat/opera- tional ceiling
• Ease of maintenance, high efficiency of monitoringand diagnostic system
•Steady operation.
BASIC SPECIFICATIONS
Thrust, kgf ............11200
SPC kg/kgf*h ............2,7
Doors diameter, mm ............1640
Dry mass, kg
•with long ejector doors ............2772+2%
•with short ejector doors............2706 +2%
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