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RB-211-22B


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RB-211-22B Rolls Royce turbofan engine. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust. Used on L1011 launch aircraft for Pegasus, Pegasus XL. First flight 1990.

Number: 117 . Thrust: 29.40 kN (6,609 lbf). Unfuelled mass: 4,180 kg (9,210 lb). Specific impulse: 9,900 s. Burn time: 4,590 s.

Thrust (sl): 26.700 kN (6,002 lbf). Thrust (sl): 2,727 kgf. Engine: 4,180 kg (9,210 lb). Thrust to Weight Ratio: .71.

Family: Turbofan. Country: UK. Launch Vehicles: Pegasus, Pegasus XL. Propellants: Air/Kerosene. Stages: L-1011. Agency: Rolls Royce. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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