RM-100A

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-100A

RM-100A
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

Date: 1967. Thrust: 441 N (99 lbf). Specific impulse: 301 s.

Subtopics

RM-100B Rocketdyne Nitric acid/UDMH rocket engine. Satellite Reaction Control. Pressure-fed.

RM-100T Rocketdyne N2O4/Aerozine-50 rocket engine. Lunar Flyer. Pressure-fed.

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

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