Delivering liquid propellant in a reusable booster stage

Aeronautics and astronautics – Aircraft structure – Fuel supply

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244158R, 244172, B64G 122

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active

06113032&

ABSTRACT:
A system is provided for delivering liquid propellant in a booster stage of a launch vehicle. The system includes an arrangement of tanks and valves to direct a first supply of liquid propellant during ascent of the booster stage and a second supply during descent of the booster stage. In disclosed embodiments, tanks may be arranged in series or parallel.

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