发明名称 Solar-thermal drive unit for rocket propulsion system has hollow chamber body and heating channel system
摘要 <p>The drive unit has a hollow chamber body (4) with an aperture (16) to receive solar radiation (12) and an inner chamber wall (14) to convert it into the thermal energy. The heating channel system (30) acts with the hollow chamber body to heat the propulsion gas. The system includes at least one heating channel (13) which runs spirally around the longitudinal axis (17) of the body.</p>
申请公布号 DE10350734(B3) 申请公布日期 2005.03.17
申请号 DE2003150734 申请日期 2003.10.30
申请人 EADS SPACE TRANSPORTATION GMBH 发明人 MENNE, STEFAN;BICHLER, PETER;KEERL, PETER NIKOLAUS;LUGER, PETER;SPERBER, FRANZ;WAGNER, ADALBERT
分类号 B64G1/40;B64G1/44;F02K99/00;F03G6/06;F24J2/07;(IPC1-7):F02K9/42;F02K9/94;F02K11/00 主分类号 B64G1/40
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