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Sea Dragon-1 engine


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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 Sea Dragon-1 engine Aerojet LOx/Kerosene rocket engine. Design, 1962. Truax pressure fed design. Thrust, chamber pressure varied during ascent.

AKA: Sea Dragon-1. Status: Design, 1962. Thrust: 356,900.00 kN (80,234,300 lbf). Specific impulse: 290 s. Specific impulse sea level: 200 s. Burn time: 81 s. Diameter: 21.50 m (70.50 ft).

Country: USA. Propellants: Lox/Kerosene. Stages: Sea Dragon-1. Agency: Aerojet. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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