General electrothermal propulsion test facility was designed for testing experimental thrust devices on vacuum environment with high level of accuracy in measurement of desired performance parameters; system used to measure thrust from 1 to 600 g vacuum of few millimeters of mercury is described; intermediate power electrothermal propulsion test facility includes two space simulation test chambers, associated instrumentation including thrust meas-
Electrothermal propulsion testing techniques
AIAA -- Tech Paper
Meeting of the AIAA -- Space Simulation Testing Conference ; 1964 Electric propulsion
AIAA -- Technical Papers ; 3 , n 6 ; p 197-201
1964
5 pages
Conference paper
English
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