Results 91 to 100 of about 13,247 (287)
DESIGN AND ANALYSIS OF AEROSPIKE BELL NOZZLE TO IMPROVE THRUST IN ROCKET ENGINE
A J Sriganapathy +2 more
openalex +1 more source
Numerical Analysis of Side-loads Reduction in a Sub-scale Dual-bell Rocket Nozzle [PDF]
Matteo Cimini +2 more
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Development of high temperature materials for solid propellant rocket nozzle applications [PDF]
Aspects of the development and characteristics of thermal shock resistant hafnia ceramic material for use in solid propellant rocket nozzles are presented.
Lineback, L. D., Manning, C. R., Jr.
core +1 more source
Lunar landing flight research vehicle Patent [PDF]
Lunar landing flight research ...
Allen, J. G., Jr., Levin, K. L.
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Computational design exploration of rocket nozzle using deep reinforcement learning
Deep Reinforcement Learning (DRL) has emerged as a powerful tool for solving high-dimensional optimization problems in complex, unexplored domains. This study presents a novel application of DRL for computational design exploration of rocket nozzles ...
Aagashram Neelakandan +2 more
doaj +1 more source
Apparatus for changing the orientation and velocity of a spinning body traversing a path Patent [PDF]
Development of method and apparatus for spinning satellite about selected axis after reaching predetermined ...
Rosen, H. A., Williams, D. D.
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A Study on the Regenerative-Cooling Nozzle with Liquid Oxygen for Hybrid Rocket Engine - Part 1
Young Il Park +6 more
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In work methods of solution of tasks of the exception of parasitic communication channels and mixing of signals of RTS are presented on the NIP receiver entrance at tests on the starting complex Souz rocket at the spaceports the Guiana space center and ...
D.S. Klyuev +4 more
doaj
Orbital escape device Patent [PDF]
Development and characteristics of inflatable structure to provide escape from orbit for spacecrews under emergency ...
Johnson, C. C.
core +1 more source
A photomechanical investigation of the Algol solid propellant rocket motor nozzle Final report [PDF]
Photoelastic investigation on scaled models of Algol rocket engine nozzles to determine pressure and thermal ...
Becker, H., Hamilton, H.
core +1 more source

