Some Near- and Far-Field Noise Measurements for Rocket Engines Operating at Different Nozzle Pressure Ratios [PDF]
, 1958 W. H. Mayes
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Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine. [PDF]
Sci Rep, 2023 Yu N +5 more
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Plume flowfield analysis of the shuttle primary Reaction Control System (RCS) rocket engine [PDF]
A solution was generated for the physical properties of the Shuttle RCS 4000 N (900 lb) rocket engine exhaust plume flowfield. The modeled exhaust gas consists of the five most abundant molecular species, H2, N2, H2O, CO, and CO2.
Brock, F. J., Hueser, J. E.
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Advancements and Limitations in 3D Printing Materials and Technologies: A Critical Review. [PDF]
Polymers (Basel), 2023 Iftekar SF, Aabid A, Amir A, Baig M.
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Cf/SiC Ceramic Matrix Composites with Extraordinary Thermomechanical Properties up to 2000 °C. [PDF]
Nanomaterials (Basel), 2023 Park MS +5 more
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A Combustion Research Facility for Testing Advanced Materials for Space Applications [PDF]
The test facility presented herein uses a groundbased rocket combustor to test the durability of new ceramic composite and metallic materials in a rocket engine thermal environment.
Bur, Michael J.
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Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis [PDF]
, 2004 Ten-See Wang
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Experimental demonstration of tractor millimeter wave beam propulsion. [PDF]
Sci RepTakahashi M +4 more
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Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]
F1000Res, 2023 Navalino R, Muda N, Hafizah M, Ruyat Y.
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Nuclear thermal rocket nozzle testing and evaluation program [PDF]
Performance characteristics of the Nuclear Thermal Rocket can be enhanced through the use of unconventional nozzles as part of the propulsion system. The Nuclear Thermal Rocket nozzle testing and evaluation program being conducted at the NASA Lewis is ...
Davidian, Kenneth O. +1 more
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