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RD-0134


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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 RD-0134 Part of RD-0120 Kosberg LOx/LNG rocket engine. stage 1. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle variant of RD-0139.

Status: Developed 1998-on. Date: 1998-. Thrust: 2,038.00 kN (458,160 lbf). Unfuelled mass: 1,800 kg (3,900 lb). Specific impulse: 358 s. Specific impulse sea level: 316 s. Height: 3.50 m (11.40 ft).

Engine: 1,800 kg (3,900 lb). Thrust to Weight Ratio: 115.44.

Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau. Bibliography: 403. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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