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Colloid thruster technologyA program is described for attaining control, reproducibility, and predictability of operation for the annular colloid emitter. A thruster of an improved design was used for a 1000 hour test. The thruster was operated with a neutralizer for 1023 hours at 15 kV with an average thrust of 25 micropound and specific impulse of 1160 sec. The performance was stable, and the beam was vectored periodically. The clean condition of the emitter edge at the end of the test coupled with no degradation in performance during the test indicated that the lifetime could be extrapolated by at least an order of magnitude over the test time.
Document ID
19720018060
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Perel, J.
(Electro-Optical Systems, Inc. Pasadena, CA, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
REPT-4040-F
NASA-CR-122385
Report Number: REPT-4040-F
Report Number: NASA-CR-122385
Accession Number
72N25710
Funding Number(s)
CONTRACT_GRANT: NAS5-21025
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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