NASA-457M (original) (raw)

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NASA-457M

Part of NSTAR

NASA Cleveland electric/xenon rocket engine. 50 kW Hall thruster developed 2001-on.

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.

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