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Was Live: UC Davis APRL Mu-2B Hotfire 1 - 2025-04-06
Автор: APRL Davis
Загружено: Прямой эфир состоялся 6 апр. 2025 г.
Просмотров: 352 просмотра
Описание:
Final countdown starts at 2:07:06
Units in data overlay are psi for pressure, kgf for thrust.
This is the first hotfire attempt of Mu-2B, a bi-propellant liquid rocket engine developed by APRL at UC Davis.
Specs:
Propellants: Kero-LOX
Thrust(nominal): 660lbf
Injector type: 3D-printed triple-impinging
Chamber/Cooling: Ablative
Nozzle: Graphite
Cycle: Pressure-fed
Pressurant: N2
Target fire duration: 5s
Thanks to all our sponsors for making this hotfire possible, check them out on our website at aprl.space
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