Results 241 to 250 of about 2,217 (308)

Modeling Calculations for HMX Composite Propellants

AIAA Journal, 1982
HMX (cyclotetramethyline tetranitramine) composite propellants burn at rates significantly lower than HMX monopropellant. To model the behavior of these propellants, a new model was developed within the framework of the Beckstead-Derr-Price (BDP) modeling approach.
M W Beckstead
exaly   +2 more sources

Detonability of Solid Composite Propellants

ARS Journal, 1961
The thin film pla t inum resistance thermometer (heat flux gage) has been successfully applied to measurement of heat fluxes from initiators for solid propellants. Hea t fluxes measured were as high as 1000 Btu/ft-sec from hot, particleladen reaction products of pyrotechnic igniters.
Andersen, W. H., Chaiken, R. F.
openaire   +2 more sources

Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants [PDF]

open access: yesCombustion Science and Technology, 2016
Several industrial- and research-type composite solid propellants containing different nano metric metal oxide catalysts (Fe2O3, Co3O4, CuO, and PbO) with similar nominal composition, were prepared and experimentally analyzed.
Weiqiang Pang   +2 more
exaly   +2 more sources

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