Results 91 to 100 of about 105,759 (263)

Influences of B Number Effect on the Burning Rate of Solid Fuel in Single Port Hybrid Rocket [PDF]

, 2008
Jungpyo Lee
openalex   +1 more source

Experimental investigation of laboratory-scale rocket engine fed on solid polyethylene rod as fuel [PDF]

, 2007
В. В. Емец, F.P. Sanin, Ye.O. Dzhur, Mykola Masliany, Oleg Kostritsyn, Grygory Minteev, V.M. Ushkanov   +6 more
openalex   +1 more source

PROCESS MODELING ELECTRO-HYDRAULIC CONTROL SYSTEM CANCELED OR RE-LAUNCH ROCKET ENGINE SOLID FUEL

, 2015
Aleksandr Bachurin, Е. В. Стрельников, V. A. Tselischev   +2 more
openalex   +3 more sources

Global stratospheric effects of the alumina emissions by solid‐fueled rocket motors [PDF]

, 2001
M. Y. Danilin, R. L. Shia, Malcolm K. W. Ko, Debra K. Weisenstein, N. D. Sze, John J. Lamb, Tyrrel W. Smith, Peter D. Lohn, Michael J. Prather   +8 more
openalex   +1 more source

Evaluation of Marine Plastic Combustion Characteristics and Its Application as Solid Fuel for Hybrid Rockets

Aerospace
Growing demand for small satellite launches has increased the need for low-cost and environmentally sustainable propulsion systems. Hybrid rockets have garnered attention as a promising alternative, but most solid fuels are petroleum-derived ...
Moe Ohno, Yoshito Takahashi, Kenichi Takahashi, Toshifumi Sakata   +3 more
doaj   +1 more source

Ignition and combustion of high-energy materials containing aluminum, boron and aluminum diboride

MATEC Web of Conferences, 2018
Boron and its compounds are among the most promising metal fuel components to be used in solid propellants for solid fuel rocket engine and ramjet engine.
Korotkikh Alexander, Sorokin Ivan, Selikhova Ekaterina   +2 more
doaj   +1 more source

Shock Wave Processes in Umbrella Charge Channel at Solid Fuel Rocket Engine Start [PDF]

, 2021
Алексей Александрович Сятчихин, Василий Викторович Сятчихин   +1 more
openalex   +1 more source

The Three-Dimensional Transient Simulation of Cross-Shaped Grains in Hybrid Rocket Motors

Aerospace
The process of spacecraft entry, deceleration, landing, and ascent requires high specific impulse, high reliability, and high-precision thrust adjustments for the power system.
Xiangyu Meng, Huihuang Huang, Yifei Chen, Mingsen Yao, Jianyuan Wang, Hui Tian   +5 more
doaj   +1 more source

Effect of Varying Design Options on the Transient Behavior of a Hybrid Rocket Motor

Journal of Aerospace Technology and Management, 2014
Hybrid rockets provide compelling features for use in atmospheric and space rocket propulsion. One of the prominent applications of hybrid rockets which foster on its characteristics is the propulsion of micro air launch vehicles. In this paper, a set of
Raed Kafafy, Muhammad Hanafi Azami, Moumen Idres   +2 more
doaj  

Ozone depletion in the plume of a solid-fuelled rocket

, 1994
B. C. Krüger
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