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RD-56M LNG
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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-56M LNG Part of RD-56 Isayev LOx/LNG rocket engine. Vozdushnyy Start stage 2. Developed 1996-. Variant of RD-56M using liquid natural gas in place of hydrogen. First engine tests performed in 1998.
AKA: KVD-1M LNG. Status: Developed 1996-. Date: 1996-. Thrust: 73.50 kN (16,523 lbf).
Country: Russia. Propellants: Lox/LNG. Agency: Isayev bureau. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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