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Measurement of Impulsive Thrust from a Closed Radio Frequency Cavity in VacuumA vacuum test campaign evaluating the impulsive thrust performance of a tapered RF test article excited in the TM212 mode at 1,937 megahertz (MHz) has been completed. The test campaign consisted of a forward thrust phase and reverse thrust phase at less than 8 x 10(exp -6) Torr vacuum with power scans at 40 watts, 60 watts, and 80 watts. The test campaign included a null thrust test effort to identify any mundane sources of impulsive thrust, however none were identified. Thrust data from forward, reverse, and null suggests that the system is consistently performing with a thrust to power ratio of 1.2 +/- 0.1 mN/kW.
Document ID
20170000277
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
White, Harold
(NASA Johnson Space Center Houston, TX, United States)
March, Paul
(NASA Johnson Space Center Houston, TX, United States)
Lawrence, James
(NASA Johnson Space Center Houston, TX, United States)
Vera, Jerry
(NASA Johnson Space Center Houston, TX, United States)
Sylvester, Andre
(NASA Johnson Space Center Houston, TX, United States)
Brady, David
(NASA Johnson Space Center Houston, TX, United States)
Bailey, Paul
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
January 4, 2017
Publication Date
January 1, 2016
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JSC-CN-37435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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