MISSILE HAVING A TURBINE-COMPRESSING MEANS-UNIT
- 申请公布号：
- KR20150090868(A)
- 申请号：
- KR20150014632
- 申请日期：
- 2015.01.29
- 申请公布日期：
- 2015.08.06
- 申请人：
- BAYERN-CHEMIE GESELLSCHAFT FUR FLUGSCHEMISCHE ANTRIEBE MBH
- 发明人：
- GUIDO KURTH;CHRISTOPH BAUER
- 分类号：
- F02K3/00;F02K3/10;F02K9/28;F02K9/32;F42B15/10
- 主分类号：
- F02K3/00
- 摘要：
- <p>The present invention relates to a missile having a jet engine (2) comprising at least one turbine (3) and at least one compressing means (4), wherein gas generated from at least one gas generator (7) of the missile (1) drives the turbine (3). The compressing means (4) and the turbine (3) are adjacent to each other and are opposed to a flight direction (6).</p>
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