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RDMT-2600


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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-2600 Part of RDMT engine series NII Mash GOX/Alcohol rocket engine. Developed 1980's. Experimental low-thrust thruster.

Status: Developed 1980's. Thrust: 2.60 kN (585 lbf). Unfuelled mass: 5.00 kg (11.00 lb). Specific impulse: 270 s.

Engine: 5.00 kg (11.00 lb). Thrust to Weight Ratio: 53.

Country: Russia. Propellants: GOX/Alcohol. 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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