发明名称 System and methods for integrating a payload with a launch vehicle
摘要 A system for providing an interface between a launch vehicle and a payload of the launch vehicle includes payload integration points of the launch vehicle that remain unchanged relative to different payload configurations, such that a payload is configurable apart from the launch vehicle. The system makes it possible to de-couple payload installation and launch vehicle turnaround operations. Payloads can be configured off-line from launch vehicle processing, thus making it possible to accommodate unique payloads while reducing wear and tear on the launch vehicle.
申请公布号 US2004016852(A1) 申请公布日期 2004.01.29
申请号 US20020201620 申请日期 2002.07.23
申请人 BLACKWELL-THOMPSON JUDITH C.;GRAVES JOHN A.;GALE ANITA E. 发明人 BLACKWELL-THOMPSON JUDITH C.;GRAVES JOHN A.;GALE ANITA E.
分类号 B64C1/20;B64D9/00;B64G1/00;B64G1/14;B64G1/64;(IPC1-7):B64G1/22 主分类号 B64C1/20
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