Catalytic ignition of the [BMIM]DCA-H<sub>2</sub>O<sub>2</sub> propellant with the Cu(vim)<sub>2</sub>(DCA)<sub>2</sub> complex. [PDF]
Zhang Y, Yao Y, Dou P, Cheng Q, Zhang Y.
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Segmented Therapeutic Delivery via Acoustic Microbubble Relay
An acoustically driven, modular segmented delivery system is presented to overcome mechanical limitations of conventional microcatheters. Oscillating microbubbles generate directional streaming that enables continuous, targeted transport across open, angled segments.
Lei Wang +6 more
wiley +1 more source
Synthesis and UV-Curing Modification of the High cis-1,4-Hydroxyl-Terminated Polybutadiene Binder Suitable for Ultra-Low Temperature Applications. [PDF]
Lyu H +10 more
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Preparation Technology, Reactivity and Applications of Nano-Aluminum in Explosives and Propellants: A Review. [PDF]
Guo H, Zhang W, Pang W.
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Research on curing reaction kinetics and curing process of hydroxy-terminated polybutadiene (HTPB) propellants. [PDF]
Guo Z +7 more
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Modeling fatigue damage evolution in CMDB propellant based on dynamic modulus. [PDF]
Yao L +4 more
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Surface-Coated Nano-Sized Aluminum Powder's Applications in Explosives and Propellants: A Review. [PDF]
Zhang W, Guo H, Pang W.
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Stability of Solid Propellant Combustion
Physical Review Letters, 1994The stability of a combustion wave is one of the most important problems in combustion theory. The solution of the problem can be essentially simplified if the characteristic scales of the processes governing the combustion are small in comparison with the characteristic dimensions of the problem.
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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.
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