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
Aerojet 2
Aerojet N2O4/MMH rocket engine. In Production. Mixture Ratio(O/F): 1.65.

Status: In Production. Thrust: 2.00 N (0.40 lbf). Unfuelled mass: 0.27 kg (0.59 lb). Specific impulse: 265 s.

Engine: 0.27 kg (0.59 lb). Area Ratio: 150. Thrust to Weight Ratio: .75.



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

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use