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NASA NTRS ยท 19730016795

Liquid hydrogen turbopump rapid start program

Abstract

Effort was directed toward the completion of the coated feed system testing and data analysis of both the uncoated and coated system tests. A total of 11 tests were conducted with the coated feed system during three days of testing. Chill data was acquired for thermal conditioning of the system from ambient initial conditions, using a duct inlet propellent pressure of 72 psig. After three tests to determine steady state pump performance and nominal start transient operation, three coated system turbopump starts were attempted with various degrees of prechill.

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BibTeXRIS

Wong, G. S.. 1973-05-07. Liquid hydrogen turbopump rapid start program. https://ntrs.nasa.gov/citations/19730016795

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