公开(公告)号：US6079202A

公开(公告)日：2000-06-27

申请号：US62384

申请日：1998-04-17

申请人： Anthony J. Cesaroni ,  Scott Bartel ,  Korey R. Kline

发明人： Anthony J. Cesaroni ,  Scott Bartel ,  Korey R. Kline

IPC分类号： F02K9/24 ,  F02K9/32 ,  F02K9/34

CPC分类号： F02K9/24 ,  F02K9/32 ,  F02K9/343

摘要： A modular rocket motor having a cylindrical housing with one end having an inwardly curved rim and the other end having internal threads. A heat-resistant plastic liner and a threaded nozzle cap are slidingly insertable with the cylindrical housing, with the threaded nozzle cap mating with the internal threads of the cylindrical housing. The motor is threaded into a rocket frame. A nozzle cap with liner attached thereto for a modular rocket motor that is colour coded to indicate the performance classification of the rocket motor.

摘要翻译： 一种具有圆柱形壳体的模块化火箭发动机，其一端具有向内弯曲的边缘，另一端具有内螺纹。 耐热塑料衬套和螺纹喷嘴盖可与圆柱形壳体滑动插入，螺纹喷嘴盖与圆柱形壳体的内螺纹配合。 电机穿入火箭架。 具有连接到其上的衬垫的喷嘴盖，用于模块化火箭发动机，其被颜色编码以指示火箭发动机的性能分类。