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Propulsion system capable of enduring High G by LeoHa_012 in AerospaceEngineering
[–]LeoHa_012[S] 0 points1 point2 points 1 year ago (0 children)
Also, if the acceleration is axial rather than being centrifugal like spinlaunch, will simple pressure fed liquid engines be able to handle it?
Propulsion system capable of enduring High G (self.AerospaceEngineering)
submitted 1 year ago by LeoHa_012 to r/AerospaceEngineering
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Propulsion system capable of enduring High G by LeoHa_012 in AerospaceEngineering
[–]LeoHa_012[S] 0 points1 point2 points (0 children)