发明名称 |
AIRCRAFT WITH HYBRID AERODYNAMIC AND SPACE FLIGHT, AND ASSOCIATED FLIGHT CONTROL METHOD |
摘要 |
<p>An aircraft having propulsion units for both conventional aircraft flight in the atmosphere and for high-altitude operation as a rocket. The aircraft is divided into a payload compartment and a compartment containing rocket propulsion unit propellant or fuel, and includes a long transverse wing with a small back-sweep to favor lift in the dense layers of the atmosphere and to thus make it possible to climb to high altitudes at a subsonic speed before using the rocket propulsion units. The return flight portion is performed by gliding or controlled as for a conventional aircraft.</p> |
申请公布号 |
EP2081828(B1) |
申请公布日期 |
2011.11.30 |
申请号 |
EP20070821478 |
申请日期 |
2007.10.17 |
申请人 |
ASTRIUM SAS |
发明人 |
CHAVAGNAC, CHRISTOPHE;BERTRAND, JEROME;LAPORTE-WEYWADA, HUGUES;POULAIN, OLIVIER;MATHARAN, PHILIPPE;LAINE, ROBERT |
分类号 |
B64G1/00;B64C30/00;B64D27/02;B64G1/14 |
主分类号 |
B64G1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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