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
RM-1-2
Part of RM-1-1
RM-1-2
RM-1-2
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/MMH rocket engine. Satellite Reaction Control. Pressure-fed.

Date: 1967. Thrust: 4.41 N (0.99 lbf). Specific impulse: 238 s.



Family: Storable liquid. Country: USA. Propellants: N2O4/MMH. Agency: Rocketdyne.

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