نتایج جستجو برای: ریزساختار htpb
تعداد نتایج: 2554 فیلتر نتایج به سال:
The present study describes the effect of NCO/OH and triol/diol ratios on the mechanical properties of Nitro functionalized Hydroxyl-terminated polybutadiene (Nitro-HTPB) elastomers. The progress of the cure reaction of Nitro-HTPB and toluene diisocyanate (TDI) is evaluated by following up the variations in the IR absorption bands of the NCO stretching and the CO ...
A way to increase the specific impulse of solid propellants is using the energetic components as energetic binder or energetic plasticizer in the propellant formulations. Hydroxy terminated poly butadiene (HTPB) is the one of pre-polymer which was specifically synthesized for its use as a propellant. Incorporating of PEG into HTPB chains lead to increasing the polarity of binder and maybe preve...
In this paper, we use a combination of experiment and simulation to achieve enhanced levels synthetic control on the microstructure much-used binder material hydroxyl terminated polybutadiene (HTPB).
Abstract In this study, the mechanical response of HTPB propellant grain under ultra-high loads is investigated. The low, intermediate and high strain rate uniaxial compression tastings (1.7×10 −4 ~3×10 3 s −1 ) hydroxyl terminated polybutadiene (HTPB) at room temperature were carried out by using universal testing machine split Hopkinson pressure bar (SHPB) system, respectively. tests cellular...
In this article aging behavior of composite solid propellant was investigated by determining its mechanical properties at elevated temperatures. For this purpose, three HTPB samples with different microstructures were selected and composite solid propellants were prepared based on them keeping similar other components and aging was studied by accelerated method. Mechanical properties were meas...
Hypersonic air breathing propulsion system has been in the minds of human being for a very long time. Ramjet propulsion provides efficient operation along with very high specific thrust and is very attractive for gun launch ramjet projectiles, hypersonic cruise vehicles and hypervelocity missiles. In the present investigation, Zr based fuel rich propellants in NC-NG matrix and HTPB matrix were ...
This manuscript presents an ultrafast-laser-absorption-spectroscopy (ULAS) diagnostic capable of providing calibration-free, single-shot measurements temperature and CO at 5 kHz in combustion gases low high pressures. Additionally, this was extended to provide 1D, a propellant flame. A detailed description the spectral-fitting routine, data-processing procedures, determination instrument respon...
بهمنظور دستیابی به نتایج دقیق نرخ سوزش پیشرانه جامد بهروش التراسونیک، باید روابط وابستگی به فشار سرعت صوت نمونهآزمایشی، در الگوریتمهای تعیین ضخامت لحظهای اعمال گردد. در این مقاله ضمن ارائه پیشینهجامعی بر روش التراسونیک و کاربری آن در اندازهگیری نرخ سوزش، به بررسی وابستگی سرعت صوت به فشار چندین ترکیب با پایه پلیمری htpb (هیدروکسی ترمینیتد پلیبوتادین)پرداخته شده است. نمونههای پلیمری ب...
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