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发明名称
Half rotationally symmetrical supersonic air inlet for reaction jet engines, especially for ram jet rocket engines powered by solid fuel
摘要
申请公布号
DE3142464(C1)
申请公布日期
1983.07.07
申请号
DE19813142464
申请日期
1981.10.27
申请人
MESSERSCHMITT-BOELKOW-BLOHM GMBH, 8000 MUENCHEN, DE;DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT E.V., 5000 KOELN, DE
发明人
POHL, WULF-DIETER, DIPL.-ING., 8011 ZORNEDING, DE;KROHN, ERNST-OTTO, DIPL.-ING., 5204 LOHMAR, DE
分类号
F02C7/04;(IPC1-7):F02C7/04
主分类号
F02C7/04
代理机构
代理人
主权项
地址
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