Title:

UNH SEDS Hybrid Rocket System

Poster

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Abstract

The goal of this project was to build a hybrid rocket, powered by paraffin wax and nitrous oxide, capable of launching a 9 pound payload to 10,000 feet and participating in the Spaceport America challenge. To manage the many requirements for a successful rocket the team was split into four sections - Avionics, Frame, Propulsion, and Recovery. The rocket was completed on time, but with less thrust than would allow it to reach 10,000 feet and with a simple “deadweight” payload. The project will be continued next year, and that year’s team will be able to build on the current rocket in order to launch at Spaceport America.

Authors

First Name Last Name
Alice Wade
Alec Ross
Cornelis Plomp
Maddy Pitre
Tom Pare
Casimir Guida
Jeffrey Grant
Tyler Dubien
Samantha Cuozzo
Alex Chesley
Dawson Buchanan

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Submission Details

Conference URC
Event Interdisciplinary Science and Engineering (ISE)
Department Mechanical Engineering (ISE)
Group Competition and Club Teams
Added April 17, 2022, 10:09 p.m.
Updated April 17, 2022, 10:09 p.m.
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