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SERT II experimental thrustor system.Space electric rocket test /SERT/ II thrustor system, discussing flight worthiness and mercury bombardment discharges
Document ID
19670059999
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Byers, D. C.
Kerslake, W. R.
Staggs, J. F.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-700
Report Number: AIAA PAPER 67-700
Accession Number
67A38728
Distribution Limits
Public
Copyright
Other
Keywords
THRUSTOR
PROPULSIVE EFFICIENCY
ELECTRIC PROPULSION
SPACE ELECTRIC ROCKET TEST /SERT/

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