Vapor liquid separator Patent [PDF]
, 1968 Vapor-liquid separator design with vapor driven pump for separated liquid pumping for application in propellant ...
Ward, W. D.
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Numerical Studies on Thrust Augmentation in High Area Ratio Rocket Nozzles by Secondary Injection
Journal of Applied Fluid Mechanics, 2017 Single stage to orbit propulsion devices are being developed as part of low cost access to space endeavors. Sea level operation of high area ratio rocket nozzle used in rocket engines leads to an overexpanded flow condition resulting in high side loads ...
S. Shyji +3 more
doaj
THERMO-STRENGTH ANALYSIS OF UNCOOLED COMPOSITE NOZZLE OF A LIQUID ROCKET ENGINE
, 2022 М. M. Dron’, K. I. Zharikov
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Analysis of SRM model nozzle calibration test data in support of IA12B, IA12C and IA36 space shuttle launch vehicle aerodynamics tests [PDF]
Variations of nozzle performance characteristics of the model nozzles used in the Space Shuttle IA12B, IA12C, IA36 power-on launch vehicle test series are shown by comparison between experimental and analytical data. The experimental data are nozzle wall
Baker, L. R., Jr. +2 more
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A Review of Aerospike Nozzles: Current Trends in Aerospace Applications
AerospaceThe aerospike nozzle has emerged as a revolutionary technology in rocket propulsion, overcoming the limitations of conventional nozzles by dynamically adjusting the expansion of exhaust gases according to ambient pressure.
Isaac Ramirez Cardenas +2 more
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Analytical study of nozzle performance for nuclear thermal rockets [PDF]
Nuclear propulsion has been identified as one of the key technologies needed for human exploration of the Moon and Mars. The Nuclear Thermal Rocket (NTR) uses a nuclear reactor to heat hydrogen to a high temperature followed by expansion through a ...
Davidian, Kenneth O. +1 more
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Performance of rocket nozzle materials with several solid propellants [PDF]
Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid ...
Freche, J. C. +2 more
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Theoretical Analysis and Verification on Plastic Deformation Behavior of Rocket Nozzle Using a Novel Tube Upsetting-Bulging Method. [PDF]
Materials (Basel), 2023 Chen Y, Zhao S, Wang H, Li J, Hua L.
europepmc +1 more source
Enhancement of Film Cooling Effectiveness in a Supersonic Nozzle. [PDF]
Entropy (Basel), 2023 Somasekharan N +5 more
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Computer code for the prediction of nozzle admittance [PDF]
A procedure which can accurately characterize injector designs for large thrust (0.5 to 1.5 million pounds), high pressure (500 to 3000 psia) LOX/hydrocarbon engines is currently under development.
Nguyen, Thong V.
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