Recent investigations have successfully demonstrated closed-form analytical solutions of spontaneous capillary flows in idealized cylindrical containers with interior corners. In this work, the theory is extended and applied to complex containers modeling spacecraft fuel tanks employing propellant-management devices (PMDs) consisting or networks of vanes. The specific problem investigated is one of spontaneous rewetting of a typical partially filled liquid-fuel/cryogen tank with PMD after thrust resettling. The transients of this flow impact the logistics of orbital maneuvers and potentially tank thermal control. The general procedure to compute the initial condition for the closed-form transient flows is first outlined and then solved for several 'complex' cylindrical tanks exhibiting symmetry. The utility and limitations of the technique as a design tool are discussed in a summary, which also highlights comparison with NASA flight data of a model propellant tank with PMD.
Capillary rewetting of vaned containers: Spacecraft tank rewetting following thrust resettling
Transiente Kapillarströmung an den Leitblechen und Wänden des Treibstofftanks eines Raumfahrzeugs nach Abschaltung des Triebwerks
AIAA Journal ; 42 , 12 ; 2551-2561
2004
11 Seiten, 21 Bilder, 5 Tabellen, 18 Quellen
Aufsatz (Zeitschrift)
Englisch