Results 91 to 100 of about 25,713 (266)
The Size Optimization of the Liquid Helium Pressurant Tank for Liquid Propellant Rocket
, 2005 Youn Mi Park +2 more
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State of the art in the theoretical study of the high-frequency stability of working processes in liquid-propellant rocket combustion chambers [PDF]
, 2020 O.V. Pylypenkо +4 more
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Proposals for Improving the Efficiency and Durability of the Turbines of Turbo-Pump Assemblies in Liquid-Propellant Rocket Engines by Using Double-Sided Crest-Type Radial Labyrinth Seals [PDF]
, 2019 V S Vasiliev +3 more
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A Reliable Method for Predicting the Specific Impulse of Chemical Propellants
Journal of Aerospace Technology and Management, 2018 The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust.
Dany Frem
doaj
Innovative methodology for calculation and design of liquid-propellant rocket engine combustion chamber [PDF]
, 2016 О.В. Короткая +1 more
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Comparison of Different Aspect Ratio Cooling Channel Designs for a Liquid Propellant Rocket Engine
, 2007 M. E. Boysan +3 more
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