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PROPELLANT TRANSFER

PROPELLANT TRANSFER: explore 1 source-linked works published from 1963 to 1963, with original documents and citations.

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Includes records with this source-supplied label or an explicit phrase match in their metadata. Matches indicate a mention, not proof that a paper uses a method or tests a material. Source versions are consolidated by DOI.

Sources: nasa. Collection updated 2026-09-16. Counts describe this index, not the complete source archives.

NASA NTRS1963

The Development of A Heated-Hybrid Generated Gas Pressurization System for Propellant Tanks

One of the most important considerations in the design of liquid fueled rockets is the method utilized to transfer the propellants from the propellant tanks to the rocket engine. Use of storable liquid propellant propulsion systems, particularly those employing hydrazine as a fuel, facilitates the attractive possibility of employing the monopropellant virtues of the fuel in order to generate gases for pressurization of the propellant tanks.

GAS PRESSURE↗

Compare source metadata on this page

Work	Published	Source identifier	Source
The Development of A Heated-Hybrid Generated Gas Pressurization System for Propellant Tanks	1963-02-15	19630004607	nasa

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