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NASA NTRS · 19630004607

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

Donald H Lee·David D Evans
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Abstract

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.

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GAS PRESSUREPROPELLANT TRANSFERLIQUID PROPELLANTGAS EVOLUTIONFUEL TANKROCKET VEHICLE

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BibTeXRIS

Donald H Lee, David D Evans. 1963-02-15. The Development of A Heated-Hybrid Generated Gas Pressurization System for Propellant Tanks. https://ntrs.nasa.gov/citations/19630004607

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