Results 241 to 250 of about 2,217 (308)
Flexible Three-Dimensional Stress Sensor for Embedded Monitoring of Solid Rocket Propellant. [PDF]
Shi Y, Lü X, Ren K, Zhu W.
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Research on Passivation Simulation of Plasticizer N-Butylnitroxyethylnitramine (BuNENA) in Hydroxy-Terminated Polyether (HTPE) Propellants. [PDF]
Guo Z +6 more
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Research on Curing Reaction Kinetics and Curing Process of Nitrate Ester Plasticized Polyether (NEPE) Propellants. [PDF]
Wu Y, Guo Z, Yu H, Fu X.
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Comparative Study on Extrusion 3D Printing of Solid Propellant Based on Plunger and Screw. [PDF]
Song S +5 more
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Modeling Calculations for HMX Composite Propellants
AIAA Journal, 1982HMX (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
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Detonability of Solid Composite Propellants
ARS Journal, 1961The 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.
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Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants [PDF]
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
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