Minimum impulse tests of 0.45-N liquid hydrazine catalytic thrustersAn exploratory test series was conducted on three types of 0.45-N (0.1 lbf) liquid hydrazine thrusters to ascertain the minimum impulse bit capability for this class of engine. The test series is described and the results are presented. The testing was performed at 21 and 145 C (70 and 300 F) while maintaining nominal 0.45 N (0.1 lbf) upstream conditions. Valve on-times as low as 0.008 sec were applied. Impulse bits were observed for thruster temperatures of 21 and 145 C (70 and 300 F), respectively.
Document ID
19720021301
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moynihan, P. I. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)