NASA NTRS · 19790043645
Space Shuttle - Bringing cryohydrogen technology down to earth
Abstract
The External Tank must provide a safe storage container for both LH2 and LO2, a means of maintaining propellant quality in order to meet the engine pump net positive suction pressure requirements, and a structural strong-back for the Space Shuttle system, all at the minimum recurring cost and weight, while maintaining quality and reliability. The present paper summarizes External Tank design features and discusses the advantages of using LH2 and LO2 for the Space Shuttle system.
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Odom, J. B.. 1978-01-01. Space Shuttle - Bringing cryohydrogen technology down to earth. https://ntrs.nasa.gov/citations/19790043645
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