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LOx/Ethanol Global Specific Impulse vs Chamber Pressure. ROF curves for Pe = 5kPa
scorpaena Data for Ethanol and Kerosene Propellant for Gas-Generator Fed Upper Stage Application SC-Legacy 3
ecosimpro ethanol cycle analysis gas generator liquid rocket engine rocket engine bar m/s
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50 wt.% Additive - 50 wt.% DC
scorpaena Performance of Metal Hydride Fuel Additives for Rocket Propellant Applications SC-Legacy 0
oxidant fuel specific impulse dicyclopentadiene s m/s K
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Main propellant pairs for a LPRE
scorpaena Upper Stage Liquid Propellant Rocket Engine Study SC-Legacy 10
oxidant fuel specific impulse ethanol rocket engine liquid propellant propulsion systems engineering fuel mixture ratio m/s
Dataset 1
nomad-vagabond Standard Atmosphere SC-Legacy 5
standard atmosphere atmosphere parameters ft m K ◦C m/s ft/s kt
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NACA 2412 - TR0.75 - AR9 - SweepAngle 12 deg. - Box thickness 0.5 - Shell thickness 0.25
nomad-vagabond Swept wing generated results CC-BY-4.0 5
%kg mm N MPa m/s m^2 degrees mm, mm
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Dataset 1
sarveshigu SKTest SC-Legacy 0
m/s

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