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-500 engine series



Subtopics

MR-510 Redmond Hydrazine rocket engine. In Production. Arcjet system.

MR-502 Redmond hydrazine monopropellant rocket engine. Communications satellite N-S stationkeeping, MMAS 5000. In Production. First flight 1991.

MR-512 Redmond Hydrazine rocket engine. In Production. Low-voltage bus arcjet system. Input power 1780 W at 35 V DC.

MR-508 Redmond hydrazine monopropellant rocket engine. Communications satellite N-S stationkeeping, MMAS 7000. In Production. First flight 1993.

MR-509 Redmond Hydrazine rocket engine. In Production. Low-power arcjet system. Input power 1800 W at 65 V DC.

MR-501B Redmond Hydrazine rocket engine. BSAT-2 communications satellite. In Production. Electrothermal hydrazine thruster (EHT). 493 W input power at 24 V DC.



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