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A parametric investigation of a proposed Javelin split-fairing system.Rigid body ejection dynamics of split-fairing system for four-stage Javelin sounding rocket under various parameter changes
Document ID
19670041807
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hatakeyama, L. F.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Space Vehicles
Accession Number
67A20536
Distribution Limits
Public
Copyright
Other
Keywords
FAIRING
JAVELIN ROCKET
ROCKET NOSE CONE

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