| End Hall Thruster |
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Engine Model: End Hall Thruster. Designer: UM-NASA. Propellants: Electric/LH2. Isp: 600 sec. Country: USA. 1 kW arcjet, ran on H2, N2, or a mixture, at about 12A, 1 kW, peak around 600s Isp, (20-30% efficiency). Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |