Burn rate of a novel boron-AN-water green solid propellant
FirePhysChem, 2022 A novel composition of green solid rocket propellant has been suggested and examined. Boron powder was chosen to serve as fuel, for its very high energetic potential, which exceeds that of other common metals, as well as that of fossil fuels.
Adi Zamostianu, Yinon Yavor
doaj
Evaluation of on-board hydrogen storage methods for hypersonic vehicles [PDF]
Hydrogen is the foremost candidate as a fuel for use in high speed transport. Since any aircraft moving at hypersonic speeds must have a very slender body, means of decreasing the storage volume requirements below that for liquid hydrogen are needed. The
Adeyiga, A. A. +4 more
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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 +2 more
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Solid-Fueled Rocket Structural Integrity Assessment [PDF]
, 2010 Bentham Science Publisher Bentham Science Publisher
openalex +1 more source
A hierarchy of Eulerian models for trajectory crossing in particle-laden turbulent flows over a wide range of Stokes numbers [PDF]
, 2013 With the large increase in available computational resources, large-eddy simulation (LES) of industrial configurations has become an efficient and tractable alternative to traditional multiphase turbulence models.
Chalons, Christophe +5 more
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Numerical Studies of Solid Rocket Propellant PMMA-PBAN-ALF3-Nitrocellulose-Difluoramine
Journal of Physics: Conference SeriesThe aim of the new investigation is the evaluation of solid rocket Propellant. In which performing numerical analysis of solid rocket propellant and calculating the constraints involved as derived from thrust i.e.
Sachin Srivastava +6 more
semanticscholar +1 more source
Rocket having barium release system to create ion clouds in the upper atmosphere [PDF]
, 1974 A chemical system for releasing a good yield of free barium atoms and barium ions to create ion clouds in the upper atmosphere and interplanetary space for the study of the geophysical properties of the medium is ...
Lewis, B. W. +3 more
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Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner
International Journal of Aerospace Engineering, 2012 Ballistic characterization of an extended group of innovative HTPB-based solid fuel formulations for hybrid rocket propulsion was performed in a lab-scale burner. An optical time-resolved technique was used to assess the quasisteady regression history of
Luciano Fanton +2 more
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Hybrid propulsion technology program. Volume 1: Conceptional design package [PDF]
A concept design study was performed to configure two sizes of hybrid boosters; one which duplicates the advanced shuttle rocket motor vacuum thrust time curve and a smaller, quarter thrust level booster.
Holzman, Allen L. +5 more
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The Three-Dimensional Transient Simulation of Cross-Shaped Grains in Hybrid Rocket Motors
AerospaceThe 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 +5 more
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