发明名称 FLY BACK BOOSTER
摘要 A reusable first stage (100) includes a booster engine system (102) for providing thrust during launch, a structural assembly (108), canards (118), jet engines (122), wings (124), elevons (126) and retractable landing gear (130). After separation, the jet engines (122) and aerodynamic control surfaces are used to return the first stage to a landing strip. The booster system (102) includes a structurally stable outer skin system such as an isogrid structure. The first stage (100) is thereby adapted for controlled descent and recovery with minimal structural enhancement or added mass.
申请公布号 EP1328439(A2) 申请公布日期 2003.07.23
申请号 EP20000959141 申请日期 2000.05.24
申请人 LOCKHEED MARTIN CORPORATION 发明人 GREENWOOD, JAMES, R.;LAINTZ, DANIEL, J.;MEGNA, THOMAS, D.;SPENCER, ROBERT, B.
分类号 B64G1/00;B64G1/14;(IPC1-7):B64G1/00 主分类号 B64G1/00
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