Research on the influence of loading rate on the dynamic initiation fracture toughness of CMDB propellant. [PDF]
Zheng J +5 more
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This review provides a bottom‐up evaluation of sodium‐ion battery safety, linking material degradation mechanisms, cell engineering parameters, and module/pack assembly. It emphasizes that understanding intrinsic material stability and establishing coordinated engineering control across hierarchical levels are vital for preventing degradation coupling ...
Won‐Gwang Lim +5 more
wiley +1 more source
Simulation of Aging and Bonding Properties of the Matrix/Filler Interface in Particle-Reinforced Composites. [PDF]
Chen Z, Wang X, Zou Z, Qiang H, Fu X.
europepmc +1 more source
Design and Manufacturing of Experimental Solid Propellant Rocket Motor Cases Made of Carbon Composite Materials. [PDF]
Baiserikov B +7 more
europepmc +1 more source
Facile synthesis and decomposition kinetics of novel green energetic molecular perovskite based on nitrate group DAN-4 as an alternative for ammonium nitrate oxidizer. [PDF]
Yehia M +6 more
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Plasticizer-Enabled Solvent-Free Curing of Self-Healing Binder System for Energetic Materials. [PDF]
Zhang M +9 more
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Molecular Dynamics Simulation of Interfacial Effects in PBT-Based Azide Propellants Under Tensile Deformation. [PDF]
Liao H +5 more
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Influence of Titanium Content on the Microstructure and Tensile Behavior of Cold-Spray Additively Manufactured Copper-Titanium Composites. [PDF]
Cheng J +6 more
europepmc +1 more source
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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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Nano-composites for rocket solid propellants
Composites Science and Technology, 2005Aim of this work is the study of different components (binder and aluminum powders) of solid propellants used for rocket propulsion to improve ballistic performance. New propellant formulations have been tested and characterised. Combustion residues were collected by a proprietary method and analyzed both from the morphological and chemical point of ...
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