Design of Nozzle for High-Powered Solid Rocket Propellant
This paper presents a preliminary nozzle design for a high-altitude rocket to be built by SOAR, the Society of Aeronautics and Rocketry. The equations and methods used for analysis came from professional sources via text or informational videos. The equations in focus will look at the temperature/pr...
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| Format: | Article |
| Language: | English |
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University of South Florida
2018-09-01
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| Series: | Undergraduate Journal of Mathematical Modeling: One + Two |
| Online Access: | https://scholarcommons.usf.edu/ujmm/vol9/iss1/2/ |