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The Development of Staging Mechanisms for the Japanese Satellite Launcher Mu-3SIIThe staging mechanisms of the Japanese satellite launch vehicle Mu-3SII involving a unique separation and jettison mechanism for the nose fairing are described. The design requirements, the design features and the development problems are presented together with their solutions.
Document ID
19850025215
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Onoda, J. (Tokyo Univ.)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Publication Information
Publication: NASA. Ames Research Center 19th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
85N33528
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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