Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [PDF]
, 2013 С.С. Гаврюшин +4 more
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IT modeling technologies of credible rocket propellants in liquid rocket engines processes [PDF]
, 2013 Р.Р. Назырова +1 more
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Recoverable single stage spacecraft booster Patent [PDF]
, 1967 Recoverable, reusable single stage booster capable of injecting large payloads into circular earth ...
Bono, P.
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Boundary layer integral matrix procedure: Verification of models [PDF]
The three turbulent models currently available in the JANNAF version of the Aerotherm Boundary Layer Integral Matrix Procedure (BLIMP-J) code were studied.
Bonnett, W. S., Evans, R. M.
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Thermal Insulative Elastomers for Clustered Large Liquid Propellant Rocket Engines [PDF]
As thrust levels increase and as rocket engines fire for longer periods of time, the difficulties encountered in the protection of critical components from the effects of excessively high temperatures greatly increase.
Peters, S. T.
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An Experimental and Analytical Study of High-Energy-Density Propellants for Liquid Rocket Engines
, 2005 Timothy S. Kokan, John Olds
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AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312
Journal of Aerospace Technology and Management, 2012 This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the
Pedro Luiz Kaled Da Cás +3 more
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Coil-On-Plug Ignition for Oxygen/Methane Liquid Rocket Engines in Thermal-Vacuum Environments [PDF]
, 2017 John C. Melcher +5 more
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Calculation of initial dynamically unstabilized sections in the elements of liquid rocket engines turbopump units [PDF]
, 2021 Andrey Zuev +4 more
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Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine [PDF]
, 2020 Jianxiu Qin, Huiqiang Zhang
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