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Status of the 260-inch diameter solid rocket motor program.Third 260-inch diameter solid propellant rocket engine test firing
Document ID
19670051421
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ciepluch, C. C.
Date Acquired
August 3, 2013
Publication Date
June 1, 1967
Subject Category
Propulsion Systems
Accession Number
67A30150
Distribution Limits
Public
Copyright
Other
Keywords
NOZZLE GEOMETRY
TEST FIRING
MECHANICAL PROPERTY
SOLID PROPELLANT ROCKET ENGINE

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