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Adiabatic flame temperature in the chamber for different fuel/oxidant mixtures as a function of O/F ratio
scorpaena Hybrid Rocket Propellants 9
propellant impulse oxidant temperature K
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50 wt.% Additive - 50 wt.% DC
scorpaena Performance of Metal Hydride Fuel Additives for Rocket Propellant Applications 0
oxidant fuel specific impulse dicyclopentadiene s m/s K
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Dataset 1
nomad-vagabond Standard Atmosphere 5
standard atmosphere atmosphere parameters ft m K ◦C m/s ft/s kt
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