“…Based on the experience with a water-cooled 15-kW laboratory thruster, 3 a 5-20-kW radiation cooled arcjet thruster was developed and tested with hydrogen, simulated hydrazine, and ammonia as propellants. 3 Operation characteristic with the two latter propellants are well known. However, the highest specific impulse can be achieved with pure hydrogen, because the molecular weight and the frozen flow losses are the lowest with pure hydrogen.…”