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LH2-80k


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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 LH2-80k Notional LOx/LH2 rocket engine. Study 1959. Used on Nova 4L launch vehicle.

Status: Study 1959. Thrust: 355.70 kN (79,965 lbf). Unfuelled mass: 1,438 kg (3,170 lb). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 656 s.

Thrust (sl): 256.100 kN (57,574 lbf). Thrust (sl): 26,117 kgf. Engine: 1,438 kg (3,170 lb). Chamber Pressure: 30.00 bar. Area Ratio: 28. Thrust to Weight Ratio: 25.22.

Country: USA. Launch Vehicles: Nova 4L. Propellants: Lox/LH2. Stages: Nova 59-4-3, Nova 59-4-4. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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