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Results of the Mission Profile Life Test first test segment - Thruster J1A series of long term test segments of 30 cm diameter mercury bombardment thrusters is being conducted as the Mission Profile Life Test. The first 4000 hour segment has been completed with the J series thruster, J1. Thruster and power processing units were controlled by computer with software algorithms governing normal functions of startup, throttle, and shutdown as well as automatically handling a variety of off-normal conditions. Thruster operation includes a discussion of the test chronology describing notable events and their significance. Post-test examination provides insight into thruster lifetime. Results are consistent with mission requirements of 15,000 hours at 2A
Document ID
19810045148
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
James, E. L.
(Xerox Electro-Optical Systems Pasadena, Calif., United States)
Bechtel, R. T.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 81-0716
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: April 21, 1981
End Date: April 23, 1981
Sponsors: Japan Society for Aeronautical and Space Sciences, AIAA, DGLR
Accession Number
81A29552
Funding Number(s)
CONTRACT_GRANT: NAS3-20399
Distribution Limits
Public
Copyright
Other

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