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Sheet1
Relations
nomad-vagabond
Test
2
aerodynamics
secs
mm
kN
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Specific impulse of the combination of the fuels with different oxidants as a function of O/F
Relations
scorpaena
Hybrid Rocket Propellants
9
propellant
impulse
oxidant
temperature
s
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Isp vs. O/F curves for selected bi-propellant fuel combinations
Relations
scorpaena
Performance of Metal Hydride Fuel Additives for Rocket Propellant Applications
10
oxidant
fuel
specific impulse
dicyclopentadiene
s
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ISP as a function of propellant mixture ratio and chamber pressure for nitrous oxide and ethanol
Relations
scorpaena
Testing of a nitrous-oxide-ethanol bi-propellant rocket engine
11
oxidant
fuel
specific impulse
ethanol
liquid rocket engine
bipropellant
chamber pressure
nitrous oxide
s
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FLAME
Relations
Serhii.K
T-MOTOR ESCs
0
drone
multirotor
fpv
fixed wing
esc
A
s
Hz
mm
grams
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Isp vs chamber pressure
Relations
scorpaena
LOX_Ethanol Liquid Rocket Engine
1
ethanol
liquid rocket engine
modeling
combustion chamber
lox
pressure
bar
s
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roztokMCkorekce
Relations
mirekmlcoch
jjxd
1
s
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Tabelle1
Relations
matthias.rudas
Testen
1
s
m/s^2
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Dataset 1
Relations
mathotina
MyFirstRepo
1
s
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