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Space Shuttle Main Engine nozzle thermal protection system

20th Thermophysics Conference, 1985
Two of the three Space Shuttle Main Engine (SSME) nozzles are exposed to significant reentry aeroheating loads. To ensure reusability of the Nozzle Assembly, the nozzle primary structure must not exceed specific temperature limits. Due to the thermal, pressure, and dynamic flexing of the nozzle during a mission cycle, an appropriate insulating system ...
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An advanced nozzle for space motor

16th Joint Propulsion Conference, 1980
P. DONGUY, R. ELLIS
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Effect of Nozzle Spacing in Supersonic Twin Impinging Jets

AIAA Journal, 2022
Yogesh Mehta   +4 more
openaire   +1 more source

Outflow of Supersonic Gas Jets from Axisymmetric Nozzle into a Space with a High Nozzle Pressure Ratios

Russian Aeronautics, 2023
D. O. Bogdaniuk   +3 more
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SPACE OPTIMIZATION THROUGH THE USE OF DE-LAVAL NOZZLE AND BELL NOZZLE AND ITS THEORY

IAENG Transactions on Engineering Sciences, 2016
OMKAR N. DESHPANDE, NITIN NARAPPANAWAR
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Development of Magnetic Nozzle Simulations for Space Propulsion Applications

2017
In order for human kind to expand our reach beyond the Earth, and create a meaningful human presence throughout the solar system, it is almost certain that the current means of propelling spacecraft will be insufficient. With current propulsion systems that derive their energy from chemical reactions, there is an upper limit to how energetic a chemical
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Effect of Nozzle Geometry on the Space-Time Emission of Screech Tones

AIAA AVIATION 2021 FORUM, 2021
David Morata, Dimitri Papamoschou
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An Experimental Investigation into the Effect of Nozzle Spacing in Supersonic Twin Jets

AIAA Scitech 2021 Forum, 2021
Yogesh Mehta   +3 more
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