Results 211 to 220 of about 2,443,749 (274)

Combustion of a Composite Solid Propellant with Addition of Boron Powder

open access: yesCombustion, Explosion, and Shock Waves, 2022
A conjugated physical and mathematical model for the combustion of a composite solid propellant with addition of a polydisperse boron powder is presented. This model accounts for gas-dynamic processes in a two-phase, multi-rate, and multi-temperature heat-conducting medium, as well as heat transfer and reaction processes in solid propellant are taken ...
Poryazov, Vasily A.   +2 more
openaire   +3 more sources

Nanomaterials as modifier for composite solid propellants

Nano Structures Nano Objects, 2019
Abstract Propellants are the major source of chemical energy in space vehicles and missiles. The AP (Ammonium perchlorate), AN (Ammonium nitrate), RDX (Hexahydro-1, 3, 5-trinitri-1, 3, 5-triazine) and HMX (Octahydro-1, 3, 5, 7-tetranitro-1, 3, 5, 7- tetrazocine), etc are currently the most widely used energetic materials in composite solid ...
Pragnesh N Dave, Jalpa A Vara
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

Numerical Simulation of Combustion of a Composite Solid Propellant Containing Boron Powder

open access: yesCombustion, Explosion and Shock Waves, 2022
The combustion of a metallized composite solid propellant containing boron particles is numerically studied. The mathematical model is based on the approaches of two-phase reacting medium mechanics for describing processes in a two-phase flow above the ...
Vasiliy Poryazov   +2 more
exaly   +2 more sources

Nano-composites for rocket solid propellants

Composites Science and Technology, 2005
Aim 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 ...
MEDA, LUISA MARINA   +5 more
openaire   +2 more sources

Oscillatory burning of solid composite propellants

Symposium (International) on Combustion, 1963
Analytical consideration of the interaction of an oscillatory pressure disturbance with the burning zone of a composite propellant leads to the conclusion that acoustic waves induce periodic variations in the ratio of the mass release rates of composite propellant components that give rise to harmonic composition and adiabatic flame temperature ...
openaire   +1 more source

Combustion mechanisms of composite solid propellants

Symposium (International) on Combustion, 1977
By means of theoretical modeling as well as by the experimental investigation of various propellants, further elements are presented to consolidate the understanding of the combustion of ammonium perchlorate propellants. Available descriptions of A.P. combustion, binder pyrolysis and composite propellant combustion are presented and compared favorably ...
Guy Lengellé   +2 more
openaire   +1 more source

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