Keywords: موشک کامپوزیت; Ammonium nitrate; Ammonium perchlorate; Iron oxide; Composite propellant; Burning characteristics; Thermal decomposition;
مقالات ISI موشک کامپوزیت (ترجمه نشده)
مقالات زیر هنوز به فارسی ترجمه نشده اند.
در صورتی که به ترجمه آماده هر یک از مقالات زیر نیاز داشته باشید، می توانید سفارش دهید تا مترجمان با تجربه این مجموعه در اسرع وقت آن را برای شما ترجمه نمایند.
در صورتی که به ترجمه آماده هر یک از مقالات زیر نیاز داشته باشید، می توانید سفارش دهید تا مترجمان با تجربه این مجموعه در اسرع وقت آن را برای شما ترجمه نمایند.
Keywords: موشک کامپوزیت; Ammonium perchlorate; Composite propellant; Burn rate; Copper chromite; Iron oxide;
Keywords: موشک کامپوزیت; Ammonium perchlorate; Hydroxyl-terminated polybutadiene; Planar laser-induced fluorescence; Burning rate; Flame structure; Composite propellant;
Keywords: موشک کامپوزیت; Composite propellant; Nano-catalyst; Planar laser-induced fluorescence; Flame structure; Burning rate;
Keywords: موشک کامپوزیت; Ammonium perchlorate; Composite propellant; Diatomaceous earth; Low-thermal-conductivity material; Burning characteristics; Thermal decomposition
An effective method to embed catalyst on AP and its effect on the burn rates of aluminized composite solid propellants
Keywords: موشک کامپوزیت; Ammonium perchlorate; Catalyst embedded AP; Burn rate; Composite propellant; Iron oxide;
Experimental and numerical investigations on the decomposition and combustion characteristics of composite propellant with Mg/Al particles additives
Keywords: موشک کامپوزیت; Composite propellant; Mg/Al particles additives; Two-phase flow; Computational fluid dynamics;
Influence of strain rate on the compressive yield stress of CMDB propellant at low, intermediate and high strain rates
Keywords: موشک کامپوزیت; Composite propellant; Intermediate strain rate; Compression; Yield behaviour; Properties and characterisation;
Thermo-damage-viscoelastic constitutive model of HTPB composite propellant
Keywords: موشک کامپوزیت; Viscoelastic; Relaxation test; Constitutive model; Damage; Composite propellant
Influences of particle size and content of HMX on burning characteristics of HMX-based propellant
Keywords: موشک کامپوزیت; Cyclotetramethylene tetranitramine; Composite propellant; Burning characteristics
The diffusion flame structure of an ammonium perchlorate based composite propellant at elevated pressures
Keywords: موشک کامپوزیت; Ammonium perchlorate; Hydroxyl-terminated polybutadiene; Planar laser induced fluorescence; Composite propellant; Flame structure
Development of an eco-friendly method to convert life expired composite propellant into liquid fertilizer
Keywords: موشک کامپوزیت; CP; composite propellant; HTPB; hydroxyl terminated polybutadiene; AP; ammonium perchlorate; ICP-AES; inductively coupled plasma-atomic emission spectrometry; IC; ion chromatography; NC; nitrocellulose; NPK; nitrogen-phosphorous-potassium; WAO; wet ai
An experimental study of the effects of catalysts on an ammonium perchlorate based composite propellant using 5 kHz PLIF
Keywords: موشک کامپوزیت; Ammonium perchlorate; Hydroxyl-terminated polybutadiene; Planar laser induced fluorescence; Ignition delay; Catalyst; Composite propellant
Experimental observation of the flame structure of a bimodal ammonium perchlorate composite propellant using 5 kHz PLIF
Keywords: موشک کامپوزیت; Ammonium perchlorate; Hydroxyl-terminated polybutadiene; Planar laser induced fluorescence; Composite propellant; Ignition delay; Particle size
Thermal decomposition behaviors and burning characteristics of ammonium nitrate/polytetrahydrofuran/glycerin composite propellant
Keywords: موشک کامپوزیت; Ammonium nitrate; Polytetrahydrofuran; Composite propellant; Burning characteristics; Binder