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W (watt)
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mm (millimeter)
V (volt)
N*m (meter * newton)
N (newton)
G (gauss)
G/W (gauss / watt)
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mAh (milliampere-hour)
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Dataset 1
Relations
nomad-vagabond
Test
SC-Legacy
8
aerodynamics
mm
m^2
kg
N
degrees
%
mm, mm
MPa
m/s
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LOx/Ethanol Global Specific Impulse vs Chamber Pressure. ROF curves for Pe = 5kPa
Relations
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
Relations
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
Relations
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
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Dataset 1
Relations
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
Relations
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
Relations
sarveshigu
SKTest
SC-Legacy
0
m/s
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