|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 22|
An apparatus and method to control ignition, combustion burn rate, extinguishment, and reignition of solid propellant is provided.
What is claimed is: 1. A precision control solid propellant thruster comprising: a thruster body containing a solid propellant having an end face at which thrust is developed, said solid propellant being disposed between at least two electrodes, wherein the solid propellant ignites to produce a thrust exhaust only with the application of a specified ignition level of electrical power to the solid propellant; a source of electrical power in electrical communication with said at least two electrodes; and a control system to control at least one of the qua...