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RDMT-200K


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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 RDMT-200K Part of RDMT engine series NII Mash GOX/Kerosene rocket engine. Buran. Out of Production. Low-thrust attitude control thruster. Mass in ref. NIIMash 95 given as only 2.5 kg.

Status: Out of Production. Thrust: 200 N (40 lbf). Unfuelled mass: 5.50 kg (12.10 lb). Specific impulse: 265 s.

Engine: 5.50 kg (12.10 lb). Thrust to Weight Ratio: 3.63.

Country: Russia. Propellants: GOX/Kerosene. Agency: NII Mash. Bibliography: 336. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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