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Filtering by: Creator Brady, Kyle B. Academic Affiliation Mechanical, Industrial, and Manufacturing Engineering Non-Academic Affiliation Oregon State University. Honors College

Testing and design procedures for electric propellant pumps for suborbital bi-propellant rockets

Creator:

Verna-Ketel, Dominic

Abstract:

An electrically driven propellant pump (HALE E-Pump) was analysed and tested to determine its viability for use in a bi-propellant launch vehicle for the High-Altitude Liquid Engine (HALE) student rocket team at Oregon State University (OSU). The pump, manufactured in 2022 by students in OSU machine shops, was hydrostatically tested...

Resource Type:

Honors College Thesis

Full Text:

Suborbital Bi-propellant Rockets Abstract approved: Kyle Niemeyer An electrically driven propellant pump

ScholarsArchive@OSU

Testing and design procedures for electric propellant pumps for suborbital bi-propellant rockets

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