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Showing content from http://www.astronautix.com/c/../r/../r/rdmt-08.html below:

RDMT-0.8


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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-0.8 Part of RDMT engine series Status: In Production. Thrust: 0.80 N (0.17 lbf). Unfuelled mass: 0.10 kg (0.22 lb). Specific impulse: 70 s.

Engine: 0.10 kg (0.22 lb). Thrust to Weight Ratio: .81.

Family: Cold Gas. Country: Russia. Propellants: Nitrogen+Helium. 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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