End Hall Thruster

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

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).

Electrical Input Power: 1.00 kW.

Related