Encyclopedia Astronautica 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 NASA-457M Date: 2000-2004. Specific impulse: 2,326 s. In 2001, Aerojet Redmond Rocket Center was competitively selected to design a 50 kW Hall thruster as a complementary effort to NASA GRC's in-house development of the NASA-457M thruster. In FY04, following testing of the Aerojet design, the high-power Hall thruster development was refocused on the NASA-457M, 50 kW Hall thruster.
Electrical Input Power: 50.00 kW.
Country: USA. Propellants: Electric/Xenon. Agency: NASA Cleveland. 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 � 1997-2016 Mark Wade - Contact � / Conditions for Use |
