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