发明名称 System and method for return and landing of launch vehicle booster stage
摘要 A recoverable/reusable booster stage has air-breathing jet engines mounted on the inter-tank ring in alignment with the center axis of the booster body. The jet engines provide supplemental lift on ascent, power the booster on a return flight, and hover the spent booster for a vertical, tail-down landing at the launch site.
申请公布号 US6817580(B2) 申请公布日期 2004.11.16
申请号 US20030390048 申请日期 2003.03.17
申请人 SMITH NORMAN LOUIS 发明人 SMITH NORMAN LOUIS
分类号 B64G1/14;B64G1/40;(IPC1-7):B64G1/40 主分类号 B64G1/14
代理机构 代理人
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