|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/169 ; 244/135C ; 244/135R ; 244/172|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 24 인용 특허 : 4|
A novel propellant resupply system for, and method of recharging the propellant tanks of, the attitude control system (ACS) of a spacecraft or the like are described, comprising first and second propellant conduits respectively interconnecting the outlets of the fuel and oxidizer pump inducers of the primary propulsion system with the fuel and oxidizer tanks for the ACS thruster engines, and controller valves within each propellant conduit for controllably diverting fuel and oxidizer under pressure from the fuel and oxidizer pumps to the thruster fuel an...
In an attitude control system for a spacecraft or the like having a primary propulsion system including at least one primary engine, a source of fuel and a source of oxidizer, and separate fuel pump means and oxidizer pump means for pressurizing fuel and oxidizer for burning in said at least one primary engine, said attitude control system including at least one thruster engine and a pressurized fuel supply tank and a pressurized oxidizer supply tank for supplying fuel and oxidizer to said thruster engine, an improvement, comprising: a. first conduit mea...