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RDMT-400


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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-400 Part of RDMT engine series NII Mash N2O4/UDMH rocket engine. Almaz, Kvant, Kristall, Spektr, Priroda. In Production. Low-thrust attitude control thruster. Used in Isayev 11D458 engine.

AKA: 11D458. Status: In Production. Thrust: 400 N (80 lbf). Unfuelled mass: 2.50 kg (5.50 lb). Specific impulse: 255 s.

Engine: 2.50 kg (5.50 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 16.4.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Proton KM-4 Briz M, Rokot-3 Briz. 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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