Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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-50
Part of RDMT engine series
NII Mash N2O4/UDMH rocket engine. Kosmos satellites. In Production. Low-thrust attitude control thruster.

Status: In Production. Thrust: 50 N (11 lbf). Unfuelled mass: 1.00 kg (2.20 lb). Specific impulse: 255 s.

Engine: 1.00 kg (2.20 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 5.09.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. 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
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use