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Isp(O/F) - 700 psi
scorpaena Testing of a nitrous-oxide-ethanol bi-propellant rocket engine
oxidant fuel specific impulse ethanol liquid rocket engine bipropellant chamber pressure nitrous oxide 1 : s
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Bmax(Hmax) - rolling direction - 0°
nomad-vagabond Magnetic Materials Measurements
magnetic material magnetization magnetic properties dc magnetic properties A/m : T
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Delivery Head vs. Q - MA type 7
nomad-vagabond Magnetically Coupled Centrifugal Pumps
sondermann magnetically coupled pump centrifugal pump magson m^3/h : 1
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T(H)
nomad-vagabond Standard Atmosphere
standard atmosphere atmosphere parameters m : K
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20x12@10000 RPM - Pe vs Velocity
nomad-vagabond APC Propellers Test Data
propeller mph : 1
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N2O4+CH6N2 - Isp vs O/F
scorpaena Catalyst for Highly Concentrated Hydrogen Peroxide
hybrid rocket engine hydrogen peroxide catalytic decomposition swirl injection combustion efficiency
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Engine mass (Pc)
scorpaena LOX_Ethanol Liquid Rocket Engine
ethanol liquid rocket engine modeling combustion chamber lox pressure bar : kg
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Max thrust vs diameter
nomad-vagabond T-Motor Propeller Load Study
propeller drone multirotor mm : kg
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Stress vs. Strain
scorpaena Stress_strain relationship model of bamboo under axial loading
bamboo tension compression composite maerial 1 : MPa
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Data Relation 1
elenaonishhenk0 test_new
drone
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