MR-512 (original) (raw)

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

MR-512

Part of MR-500 engine series

MR-512
Credit: Aerojet Redmond

Redmond Hydrazine rocket engine. In Production. Low-voltage bus arcjet system. Input power 1780 W at 35 V DC.

Status: In Production. Thrust: 0.25 N (0.06 lbf). Unfuelled mass: 7.23 kg (15.93 lb). Specific impulse: 502 s. Burn time: 3,780,000 s. Height: 0.25 m (0.82 ft). Diameter: 0.0430 m (0.1410 ft).

Engine: 7.23 kg (15.93 lb). Restarts: 1170.

Family: Storable liquid. Country: USA. Agency: Redmond.

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