|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/771; 060/770; 060/767; 060/253|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 50|
A propulsion system, such as for use in a missile, includes a multinozzle grid having a pair of plates that are separably mechanically coupled together. When coupled together in a first configuration, the plates provide multiple nozzles in a first nozzle configuration (geometry). Separation of the plates, such as by separating an aft plate from a forward plate that remains with the missile, reconfigures the multinozzle grid to a second configuration that has nozzles in a second nozzle configuration (geometry). The nozzle configurations may be suitable fo...
1. A hybrid propulsion system comprising: a solid rocket motor;a ramjet; anda reconfigurable multinozzle grid;wherein the solid rocket motor and the ramjet both pass pressurized gas through the reconfigurable multinozzle grid;wherein the multinozzle grid includes: a forward plate; andan aft plate;wherein the plates are separably mechanically coupled together;wherein, when the plates are mechanically coupled together, the plates define a plurality of converge-diverge nozzles each having a first configuration;wherein, when the plates are separated, the noz...