Results 121 to 130 of about 13,247 (287)
Reliability of solid rocket motor cases and nozzles [PDF]
A recent article in Aerospace America claims that 'the average success ratio of the current U.S. stable of launch vehicles, including upper stages, is about 92 percent (without upper stages it is close to 95 percent).
Crose, James G.
core +1 more source
New class of thermosetting plastics has improved strength, thermal and chemical stability [PDF]
New class of thermosetting plastics has high hydrocarbon content, high stiffness, thermal stability, humidity resistance, and workability in the precured state.
Burns, E. A. +2 more
core +1 more source
Rocket Engine Vacuum Nozzle 3D Printing: Manufacturing, Weight, and Cost Savings [PDF]
Nikolaos D. Alexopoulos +10 more
openalex +1 more source
The rotating detonation engine (RDE) is an innovative pressure-gain combustion device that harnesses detonation waves for efficient fuel combustion.
Guining Liu +6 more
doaj +1 more source
Study on CerAMfacturing of Novel Alumina Aerospike Nozzles by Lithography-Based Ceramic Vat Photopolymerization (CerAM VPP). [PDF]
Schwarzer-Fischer E +6 more
europepmc +1 more source
Nozzle fabrication technique [PDF]
This invention relates to techniques for fabricating hour glass throat or convergent divergent nozzle shapes, and more particularly to new and improved techniques for forming rocket nozzles from electrically conductive material and forming cooling ...
Wells, Dennis L.
core +1 more source
Vortex servovalve for fluidic or electrical input [PDF]
Proportional-pressure control servovalve consisting of fluid amplifier bellows-driven jet-pipe and two vortex valves operating in push-pull, with a pair of bellows for pressure feedback is tolerant to comtaminant particles and meets minimum standby flow ...
Honda, T. S.
core +1 more source
Estimation of Hybrid Rocket Nozzle Throat Erosion History
Yuji Saito +5 more
openalex +2 more sources
Lightweight RepVGG-Based Cross-Modality Data Prediction Method for Solid Rocket Motors. [PDF]
Yang H, Zheng S, Wang X, Xu M, Li X.
europepmc +1 more source
Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is an innovative extension of after burners. This technique finds application in single stage to orbit propulsion devices, where the nozzle has to work at ...
G. Anugrah +3 more
doaj

