Turbojet 1000daN

Turbojet 1000daN
Maximum thrust (daN)	1000
Engine diameter (mm)	567
Operating speed (Ma)	0 - 0.95
Engine length (mm) (excluding nozzle)	1140
Fuel consumption rate (kg/(daN·h))	1.04
mass(kg)	185
Operating altitude (m)	0 - 18000
Thrust-to-weight ratio	4.55

All specifications are approximate. Specifications are subject to change without notice.

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Turbojet 1000daN