End Hall Thruster (original) (raw)

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End Hall Thruster

UM-NASA electric/LH2 rocket engine. 1 kW arc jet, ran on H2, N2, or a mixture, at about 12A, 1 kW, peak around 600s Isp, (20-30% efficiency).

Specific impulse: 600 s.

Electrical Input Power: 1.00 kW.

Country: USA. Propellants: Electric/LH2. Agency: UM-NASA.

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