Pressure-Fed Cycle Based Liquid Rocket Engine integrated as a thruster.
Propellants:
Fuel : C3H8(L) 100%
Oxidizer: N20(L)
Properties:
Specific impulse (vac) : 268.45 s
Chamber Pressure : 700 psi
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Pressure-Fed Based Liquid Rocket Engine
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nyameaama/Converse-Engine
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Pressure-Fed Based Liquid Rocket Engine
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