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NASA NTRS ยท 19920013360

Hybrid Rocket Propulsion for Sounding Rocket Applications

Abstract

A discussion of the H-225K hybrid rocket motor, produced by the American Rocket Company, is given. The H-225K motor is presented in terms of the following topics: (1) hybrid rocket fundamentals; (2) hybrid characteristics; and (3) hybrid advantages.

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BibTeXRIS

1991-01-01. Hybrid Rocket Propulsion for Sounding Rocket Applications. https://ntrs.nasa.gov/citations/19920013360

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