Space Environment Facility for Electric Propulsion Systems Research

A facility containing 15- and 25-foot-diameter space-environment tanks and support equipment is described. The facility is designed for testing ion and plasma thrustors, 10 sub -7 spacecraft, and related components at pressures in the 10 torr range. Total pumping capacity in the 10 sub -5 torr range...

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Bibliographische Detailangaben
Hauptverfasser:	Finke, Robert C, Holmes, Arthur D
Format:	Report
Sprache:	eng
Schlagworte:	AMPTIAC COLLECTION Astrophysics CAPACITY(QUANTITY) CONDENSERS(LIQUEFIERS) COOLING Electric and Ion Propulsion ELECTRIC PROPULSION ELECTRICAL EQUIPMENT FACILITIES FEET INSTALLATION INSTRUMENTATION Jet and Gas Turbine Engines LIQUID NITROGEN PERSONNEL POWER PRESSURE PROTECTION PUMPING SPACE ENVIRONMENTS SPINNING(MOTION) SYSTEMS ANALYSIS TEST EQUIPMENT THRUSTERS
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