|국가/구분||United States(US) Patent 등록|
|우선권정보||FR-13 62430 (2013-12-11)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 11|
A system for regulating the flow rate of a propellant fluid for an electrical thruster of a space vehicle, the vehicle including a tank of propellant fluid and a flow rate regulator connected to the outlet of said tank; the flow rate regulator including a heater element controlled by a computer and adapted to heat the propellant fluid and to modify its physical properties so as to vary the flow rate of propellant fluid leaving the tank; said system being characterized in that the computer also includes a plurality of empirical calibration curves that hav...
1. A system for regulating a flow rate of a propellant fluid of a space vehicle, said system comprising: an electrical thrustera tank of propellant fluid anda flow rate regulator connected to an outlet of said tank;wherein said flow rate regulator further includes a heater element controlled by a computer and configured to heat said propellant fluid and modify said propellant fluid physical properties to vary said flow rate of said propellant fluid leaving said tank;wherein said computer further includes a storage memory having loaded therein a plurality...