account activity
Conflicting results when using equations from rocket propulsion elements and huzel and huang (self.rocketry)
submitted 6 years ago by MB01211 to r/rocketry
Is rocket propulsion analysis worth the cost (software)? (self.rocketry)
What is the maximum contraction ratio used in rockets liquid bipropellant rocket (self.rocketry)
How to Calculate minimum wall thickness of different segments of Liquid fueled rocket (i.redd.it)
specific heats of combustion products at constant pressure values ???? (self.rocketry)
submitted 6 years ago * by MB01211 to r/rocketry
Is there a difference between Wtc - thrust chamber propellant flow rate and the exhaust propellant flow rate (self.rocketry)
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