Results 211 to 220 of about 1,546,701 (274)

Polymethylhydrosiloxane-Coated Ammonium Dinitramide: A Simple Strategy to Moisture-Resistant and Insensitive Energetic Microspheres. [PDF]

ACS Omega
Bui AT, Pham QH, Pham VT, Vu MT, Cao HT.
europepmc   +1 more source

Preparation of Inverse-Loaded MWCNTs@Fe₂O₃ Composites and Their Impact on Glycidyl Azide Polymer-Based Energetic Thermoplastic Elastomer. [PDF]

Polymers (Basel)
Pang S, Lv Y, Liu S, Sang C, Jin B, Luo Y.   +5 more
europepmc   +1 more source

Advances in PBT Binder and Its Application in Propellants. [PDF]

Polymers (Basel)
Zhang N, Gao X, Luo Y, Zhang W, Xin Y, Zhang K, Xue C, Zhang H, Wei J, Wang H.   +9 more
europepmc   +1 more source

Study on elongation master curve of thermal aging composite modified double base propellant. [PDF]

Sci Rep
Zheng J, Liu J, Deng H, Dang J, Yang C, Sun Z, Guo Z, Xu J, Chen X.   +8 more
europepmc   +1 more source

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INVESTIGATION OF SOLID PROPELLANT MICROTHRUSTERS

International Journal of Computational Engineering Science, 2003
A novel micropropulsion system is described for high-accuracy station keeping, attitude control and speed adjusting of microspacecraft. The proposed solid propellant microthruster is composed of two layers bonded together. One layer is a silicon layer, which contains a microchamber, a micronozzle and a 30-micron slot.
K. L. Zhang, S. K. Chou, Simon S. Ang, X. S. Tang, J. S. Phang   +4 more
openaire   +1 more source

Solid-propellant erosive burning

Journal of Propulsion and Power, 1987
A modeling approach based on experimental verification for the erosive burning of ammonium perchlorate composite propellants is proposed. It retains the idea that erosive burning is due to the penetration of the flow turbulence within the flame height and to the consequent enhancement of the transport coefficients and of the heat flux to the surface ...
J. GODON, J. DUTERQUE, G. LENGELLE
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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

Stability of Solid Propellant Combustion

Physical Review Letters, 1994
The 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.
, Bychkov, , Liberman
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Ignition and Combustion of Solid Propellants

1961
Abstract : A model for the ignition response of solid propellants is presented, which predicts ignition behavior with respect to pressure and surface heat flux in qualitative agreement with experimental measurements. Surface regression is treated and a steady-state burning model is employed, which assumes equlibrium vaporization at the surface and a ...
Norman W. Ryan, Alva D. Baer, John A. Keller, Rex C. Mitchell   +3 more
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Adiabatic pyrolysis of solid propellants

35th Aerospace Sciences Meeting and Exhibit, 1997
Several one-step, irreversible, zero-order pyrolysis models (Arrhcnius, KTSS, and Merzhanov Dubovitskii high activation energy pyrolysis), commonly used to study adiabatic burning of energetic materials with arbitrary pressure and initial temperature, are revisited.
DE LUCA, LUIGI, VERRI, MAURIZIO, COZZI, FABIO, COLOMBO, GIOVANNI, E. Volpe   +4 more
openaire   +1 more source