A passive propellant acquisition and feed system is disclosed which acquires and feeds gas-free propellant in low or zero-g environments during orbital maneuvers and retains this propellant under high axially directed acceleration such as may be experienced during launch of a space vehicle and orbit-to-orbit transfer is described. The propellant system includes a dual compartment propellant tank with independent surface tension acquisition channels in each compartment to provide gas-free flow of pressurized liquid propellant from one compartment to the other in one direction only.
Passive propellant system
1979-09-25
Sonstige
Keine Angabe
Englisch
NTRS | 1978
|NTIS | 1978
|NTIS | 1978
|Criteria for passive propellant control schemes
AIAA | 1969
|Criteria for passive propellant control schemes
AIAA | 1970
|