Results 151 to 160 of about 967 (177)
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Development of a N2O/HTPB hybrid rocket motor
33rd Joint Propulsion Conference and Exhibit, 1997Experiments were performed as a part of the Hybrid Propulsion Demonstration Program (HPDP) in order to demonstrate a N2O/HTPB hybrid sounding rocket. Multiple hybrid motors have been tested at Environmental Aeroscience Corporation in order to develop a high performance hybrid flight system.
J. Arves +11 more
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Evaluation of tg data of htpb-based polyurethanes
Journal of Thermal Analysis and Calorimetry, 2004Thermogravimetry (TG) was used to provide some new information on some polybutadiene-based polyurethanes. The results showed two main mass decomposition stages, from 230 to 564°C. The first mass loss stages were used to quantify the hard segments of the polymers. The results correlated well with the ASTM methodology.
E. F. S. Vieira +3 more
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41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005
Moshe Kivity +2 more
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Moshe Kivity +2 more
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Accelerated Aging Tests of HTPB-Based Propellants
2018In the late twentieth century, liquid and solid propulsion technologies have been integrated into hybrid engines currently apllied in propulsion launch vehicles and missiles. The reaction of polyol (HTPB) and diisocyanate (IPDI) provides the most versatile of the binders in the production of solid propellants due to its ability to withstand high loads ...
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HTPB propellant aging and service life
16th Joint Propulsion Conference, 1980A. CHRISTIANSEN, L. LAYTON, R. CARPENTER
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A study on the decomposition pathways of HTPB and HTPE pyrolysis by mass spectrometric analysis
Journal of Analytical and Applied Pyrolysis, 2023Zhandong Wang, Liangyuan Jia, Liu Peiqi
exaly
Development of HTPB binder for solid propellant
24th Joint Propulsion Conference, 1988KATSUAKI KOSAKA +4 more
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