Accession Number:
AD0818904
Title:
IMPULSE BIT TESTING OF A THERMAL-STORAGE RESISTANCE-HEATED NITROGEN-PROPELLED THRUSTOR.
Descriptive Note:
Technical rept. Jan-Apr 66,
Corporate Author:
AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OH
Personal Author(s):
Report Date:
1967-05-01
Pagination or Media Count:
44.0
Abstract:
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
Descriptors:
Subject Categories:
- Aircraft
- Unmanned Spacecraft