发明名称 UNIVERSAL LAUNCH VEHICLE PAYLOAD ADAPTER
摘要 A universal adapter system and method for coupling payloads and launch vehicles are disclosed to provide optimum payload configurability. A modular bulkhead panel may be used that can support a plurality of payload platforms such that the layout of the plurality of payload platforms on the bulkhead panel can be altered without requiring structural redesign. A carbon composite honeycomb structural frame panel may be used. Multiple bulkhead panels can be stacked to handle larger payload weights. Hollow hexagonal keyways can be used to permit cable access to and from a missile deployment module. Hexagonal payload adapter platforms may be used to join the payload to the honeycomb bulkhead panel.
申请公布号 US2008135687(A1) 申请公布日期 2008.06.12
申请号 US20060608231 申请日期 2006.12.07
申请人 THE BOEING COMPANY 发明人 PENZO LEONARD A.
分类号 B64G1/22 主分类号 B64G1/22
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