SM98-118/353 The Use of RTM Technology to Manufacture Interface Rings for Launchers. An Option for Structure Mass Optimization

Details SM98-118/353 The Use of RTM Technology to Manufacture Interface Rings for Launchers. An Option for Structure Mass Optimization SM98-118/353 The Use of RTM Technology to Manufacture Interface Rings for Launchers. An Option for Structure Mass Optimization

Feb 1999

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1999esasp.428..377d&link_type=gif

Spacecraft structures, materials and mechanical testing, Proceedings of a European Conference held at Braunschweig, Germany, 4-

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