IMPULSE BIT TESTING OF A THERMAL-STORAGE RESISTANCE-HEATED NITROGEN-PROPELLED THRUSTOR.
Technical rept. Jan-Apr 66,
AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OH
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This report summarizes the results of an experimental study to investigate the impulse-bit characteristics of a low-power, thermal-storage, resistance-heated thrustor operating on gaseous nitrogen propellant. Impulse bits were generated in the range of 12000 to .01 lb sub f-sec at propellant temperatures from 530 R to nearly 2400 R. Author
- Unmanned Spacecraft