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Discharge Chamber Optimization of the SERT II ThrustorOptimum discharge chamber configuration of permanent magnet mercury-bombardment thrustor for SERT II mission
Document ID
19670059973
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Bechtel, R. T.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-668
Report Number: AIAA PAPER 67-668
Accession Number
67A38702
Distribution Limits
Public
Copyright
Other
Keywords
OPTIMIZATION
THRUSTOR
ROCKET CHAMBER
SPACE ELECTRIC ROCKET TEST /SERT/
ION ENGINE

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