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Solid boost thrust decay control for stage separation.Solid booster thrust decay control for payload or upper stage separation, noting inert slivers with auxiliary retrorockets as separation control
Document ID
19670033564
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Majoros, J.
Sarlat, I. M.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-971
Report Number: AIAA PAPER 66-971
Accession Number
67A12293
Funding Number(s)
CONTRACT_GRANT: NAS8-11370
Distribution Limits
Public
Copyright
Other
Keywords
THRUST CONTROL
SOLID PROPELLANT ROCKET ENGINE
STAGE SEPARATION

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