Design of a cold gas propulsion nozzle for microsatellites using computational fluid dynamics and response surface optimization
In this paper, the process of designing, validating, and testing the nozzle of a cold gas thruster will be described. The thruster in question is meant to reduce the rotational velocity of a 50kg microsatellite after its deployment by repeatedly unloading propellant to generate thrust. The key desig...
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| Main Authors: | , , , |
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| Format: | text |
| Published: |
Animo Repository
2019
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| Subjects: | |
| Online Access: | https://animorepository.dlsu.edu.ph/faculty_research/1206 https://animorepository.dlsu.edu.ph/context/faculty_research/article/2205/type/native/viewcontent |
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| Institution: | De La Salle University |