A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]
Sci RepLi T, He H, Yu N, Sun X, Cai G.
europepmc +1 more source
Liquid rocket combustor computer code development [PDF]
The Advanced Rocket Injector/Combustor Code (ARICC) that has been developed to model the complete chemical/fluid/thermal processes occurring inside rocket combustion chambers are highlighted.
Liang, P. Y.
core +1 more source
Liquid-propellant droplet vaporization and combustion in high pressure environments [PDF]
In order to correct the deficiencies of existing models for high-pressure droplet vaporization and combustion, a fundamental investigation into this matter is essential.
Yang, Vigor
core +1 more source
Interrelation Between Dilatation Rate and Displacement Speed in Premixed Turbulent Flames. [PDF]
Flow Turbul CombustMohan V +4 more
europepmc +1 more source
Bipropellant droplet burning rates and lifetimes in a combustion gas environment [PDF]
Liquid rocket propellant droplet burning rate and lifetimes in combustion ...
Faeth, G. M., Lazar, R. S.
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Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
PLoS OneHuang AM, Xu Y.
europepmc +1 more source
Design and Optimization of a Hybrid Gas Generator for Hydrogen Peroxide Tank Pressurization
Challenges and Issues of Modern SciencePurpose. This study develops a pressurization system for hydrogen peroxide tanks using a hybrid gas generator powered by liquid oxygen and solid fuel.
Mykhailo Vorobei, Mykola Bondarenko
doaj
Amine-AlH<sub>3</sub> Adducts as Energetic Materials for a New Generation of Solid Fuels. [PDF]
ChemistryLiu X +4 more
europepmc +1 more source
Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]
Polymers (Basel)Meiirbekov M +7 more
europepmc +1 more source
Chamber shape effects on combustion instability [PDF]
Rocket combustor shape effects on combustion ...
Bloomer, H. E. +2 more
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