发明名称 System for use of external secondary payloads
摘要 An experiment system with six different re-entry experiment locations for testing high temperature re-entry materials, creating new thermal protection systems, proving innovative new concepts for spacecraft exterior surfaces and the incremental development of next generation aerospace materials. A commercial transportation system to and from orbit provides a 24-hour return cycle for the experiments on a surface actually re-entering the earth's atmosphere. Now using existing doors, hatches and other points on the reusable launch vehicle's exterior, the actual re-entry environment is experienced by test specimens with quick turn around for a wide variety of different re-entry temperatures ranges for broad testing and development purposes. The reusable launch vehicle launches, remains in orbit for 24 hours and returns to provide an actual test environment for the exterior experiment system.
申请公布号 US7354020(B2) 申请公布日期 2008.04.08
申请号 US20030698261 申请日期 2003.10.31
申请人 KISTLER AEROSPACE CORPORATION 发明人 MUELLER GEORGE E.;LAI GARY;TAYLOR THOMAS C.
分类号 B64G1/22;B64G1/10;B64G1/14;B64G1/58;B64G1/62 主分类号 B64G1/22
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