|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/229; 60/251; 60/257|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 24 인용 특허 : 3|
This propulsion system of a rocket motor assembly includes an array of attitude-control rocket engines, one or more oxidizer-fluid sources, one or more ignition-fluid sources, and, optionally, one or more primary rocket engines. Each of the attitude-control rocket engines has a respective combustion chamber and is offset from the longitudinal axis of the rocket motor assembly so that when a selected one or group of the attitude-control rocket engines is fired, the flight path of the assembly is diverted and/or the rocket assembly spins. The oxidizer-flui...
1. A rocket motor assembly having a longitudinal axis and comprising a propulsion system, said propulsion system comprising: an array of eccentric rocket engines offset from the longitudinal axis of said rocket motor assembly to permit attitude control of said rocket motor assembly by independent firing of a selected one or group of said eccentric rocket engines, said eccentric rocket engines each comprising a respective combustion chamber; one or more oxidizer-fluid sources in operative communication with said eccentric rocket engines to permit oxidize...