Results 241 to 250 of about 10,802 (309)

Study on rheological properties of composite propellant slurry in the mixing process by using experimental and numerical simulation. [PDF]

RSC Adv
Guo Z, Fu X, Rossi R.
europepmc   +1 more source

Research on Curing Reaction Kinetics and Curing Process of Nitrate Ester Plasticized Polyether (NEPE) Propellants. [PDF]

Polymers (Basel)
Wu Y, Guo Z, Yu H, Fu X.
europepmc   +1 more source

UV-Assisted Material Extrusion Additive Manufacturing of Double-Base Propellant. [PDF]

Polymers (Basel)
Li M, Gao Y, Wang Q, Yang W, Gao GL, Jiang Z.   +5 more
europepmc   +1 more source

Construction of Covalent Triazine Framework-Supported MnCo₂O_4.5 Nanoneedles via Enhanced Dispersion Strategy to Promote Ammonium Perchlorate Thermal Decomposition. [PDF]

Nanomaterials (Basel)
Kou B, Gao B, Chen X, Chen W, Tan L.
europepmc   +1 more source

Effective Performance Modifications for a Composite Rocket Propellant via Coagglomerates of Cyclic Nitramines. [PDF]

ACS Omega
Patil VB, Lewczuk R, Sazeček F, Paziewska P, Stojan P, Bělina P, Zeman S.   +6 more
europepmc   +1 more source

Numerical simulation of stability of diffusion depth of deterrents into cylindrical nitrocellulose composite under different conditions. [PDF]

BMC Chem
Al-Hetty HRAK, Al-Dulaimi AA, Saleem HM, Kianfar E.   +3 more
europepmc   +1 more source

Amine-AlH₃ Adducts as Energetic Materials for a New Generation of Solid Fuels. [PDF]

Chemistry
Liu X, Ortmeyer J, Bodach A, Petersen H, Felderhoff M.   +4 more
europepmc   +1 more source

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Combustion of a Composite Solid Propellant with Addition of Boron Powder

Combustion, 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 ...
V A Poryazov, K M Moiseeva, A Yu Krainov
exaly   +3 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

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, G. Marra, GALFETTI, LUCIANO, DE LUCA, LUIGI, F. Severini, S. Inchingalo   +5 more
openaire   +2 more sources