| CPC B64G 1/00 (2013.01) | 18 Claims |

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1. A propellant management system, comprising:
a propellant management device (PMD) configured to reduce or prevent liquid propellant from entering a thruster manifold or gas venting manifold while allowing propellant vapor and/or gas to pass through the PMD to allow for thrust or venting, wherein
the PMD comprises a junction on the inside of the tank, the junction being constructed with hydrophobic material, and the junction connecting entry ports of the thruster manifold and the gas venting manifold.
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