The 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.
The Development of Staging Mechanisms for the Japanese Satellite Launcher Mu-3SII
01.08.1985
Aufsatz (Konferenz)
Keine Angabe
Englisch
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