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Probabilistic Damage Modeling and Thermal Shock Risk Assessment of UHTCMC Thruster Under Transient Green Propulsion Operation. [PDF]
Jindal P, Doozandeh T, Botchu J.
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About feasibility of SpaceX's human exploration Mars mission scenario with Starship. [PDF]
Maiwald V +4 more
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Novel technologies for CO2 conversion to renewable fuels, chemicals, and value-added products. [PDF]
Awogbemi O, Desai DA.
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A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors. [PDF]
Li Z, Sun D, Dong X, Sun X.
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The Legacy and Future of Aluminum Alloys: Space Exploration and Extraterrestrial Settlement. [PDF]
Tunes MA.
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Hybrid rocket engines: The benefits and prospects
Aerospace Science and Technology, 2007The review of research avenues for working processes (ignition, combustion, etc.) in hybrid rocket engines (HRE), for thermal protection and power characteristics is stated. Based on conducted design and exploratory studies and design developments, the reasonable fields of application of HRE to launch systems for orbit insertion of payload are ...
N.A. Davydenko +4 more
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Numerical investigations of hybrid rocket engines
Acta Astronautica, 2018Abstract Paper presents the results of numerical studies of hybrid rocket engines operating cycle including unsteady-state transition stage. A mathematical model is developed accounting for the peculiarities of diffusion combustion of fuel in the flow of oxidant, which is composed of oxygen-nitrogen mixture.
V B Betelin, N N Smirnov, V F Nikitin
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Thrust modulation in hybrid rocket engines
Journal of Propulsion and Power, 1988An experimental investigation of hybrid rocket engines (HRE) is performed to study the throttling performance within a thrust range of 10:1. In order to improve the throttling properties over the entire thrust range, the method of secondary gas injection (gasification) was used. The injection gases were reactive (O2) and inert (N2). High-pressure tests
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Hybrid Rocket Engines Design for Materials Characterization [PDF]
Hybrid Rocket Engines (HREs) have generated positive interest in the scientific community due to their ability to combine the special characteristics pertaining to solid and liquid propulsion I [ 1]. Eligible as promising technology enablers for the future of space industry, HREs are valuable for their safe and controlled design nature, simplified ...
Mangioni G. +5 more
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