Results 71 to 80 of about 2,824 (228)
PARALLEL UNSTEADY TURBOPUMP SIMULATIONS FOR LIQUID ROCKET ENGINES [PDF]
, 2000 Cetin C. Kiris, Dochan Kwak, W. Chan
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On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines [PDF]
, 2001 С. А. Шевченко
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Research Progress of Decommissioned Solid Rocket Motor Charge Emptying and Recycling Technology [PDF]
Hangkong bingqiAs the service life of solid rocket engines comes to an end, their operational reliability and performance stability gradually decline. Effectively disposing of large numbers of retired solid rocket engines has become a critical issue.
Zhou Yaping, Lin Zhihui, Wang Maoyu, Dong Jun, Liu Tiansheng, Qiao Haitao
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A Numerical Study on Sensitivity of Acoustic Response to Pressure Oscillations in Liquid Rocket Engine [PDF]
, 2002 Chae-Hoon Sohn
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Dynamic Pressure Characteristics of Pulse Gun Device for Combustion Stability Rating of Liquid Rocket Engines [PDF]
, 2003 Seonghyeon Seo +4 more
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A Numerical Study on the Combustion Characteristics in a Liquid Rocket Engine with Film Cooling Effect [PDF]
, 2003 Do-Yeong Byeon +2 more
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Mehran University Research Journal of Engineering and Technology, 2019 Optimum characteristic length of the combustion chamber of liquid rocket engine is very important to get higher energy from the liquid propellants. Characteristic length is defined by the time required for complete burning of fuel.
Tajwali Khan, Ihtzaz Qamar
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International Journal of Aerospace Engineering, 2012 Pressure and temperature of the liquid rocket thrust chambers into which propellants are injected have been in an ascending trajectory to gain higher specific impulse.
Bruce Chehroudi
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Trade-off analysis of a new liquid rocket engine
, 2019 When high specific impulse and storability are mission requirements, toxic bi-propellant storable couples are very often used. Typically hydrazine or one of its derivatives are used as fuels and nitrogen tetroxide as oxidizer. Maturity of bi-propellant non-toxic alternatives is still low, even though some monopropellant solutions are coming to the ...
Maggi, F. +5 more
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Designing and Testing of HDPE–N2O Hybrid Rocket Engine
Engineering ProceedingsHybrid Rocket Engines (HREs) combine the advantages of solid and liquid propellants, offering thrust control, simplicity, safety, and cost efficiency.
Triyan Pal Arora +6 more
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