Results 151 to 160 of about 410 (183)
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Infrared imaging of AP/HTPB laminate propellant flames
Combustion and Flame, 2008Abstract The combustion of ammonium perchlorate (AP), hydroxyl-terminated polybutadiene (HTPB) two-dimensional laminate propellants is investigated using simultaneous infrared (IR) and ultraviolet (UV) emission imaging at 1–50 atm. The IR (3300–3900 nm) measurements sense flame presence nominally via HCl rovibrational excitation and the UV (310 nm ...
R.P. Fitzgerald, M.Q. Brewster
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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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Study on the Fracture Properties of HTPB Propellant at Low Temperature
Propellants, Explosives, Pyrotechnics, 2019AbstractIn order to study the fracture behaviour of hydroxyl‐terminated polybutadiene (HTPB) propellant, the low temperature fracture toughness experiment of HTPB propellant was carried out by using centrally cracked sheet tensile specimens. The fracture toughness values of HTPB propellant with mode I crack at different temperature and loading rate ...
Bing Long +2 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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Aging Characteristics of HTPB Propellant Based on Volume Resistivity
Propellants, Explosives, PyrotechnicsABSTRACTHydroxyl‐terminated polybutadiene (HTPB) propellant faces the problem of aging from casting to use. Generally, the aging degree of HTPB propellant is evaluated by a destructive mechanical property test. Therefore, it is necessary to seek a new evaluation method. Electrical performance is a method that can achieve nondestructive testing. However,
Lina Xie +10 more
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HTPB propellant aging and service life
16th Joint Propulsion Conference, 1980A. CHRISTIANSEN, L. LAYTON, R. CARPENTER
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Development of HTPB binder for solid propellant
24th Joint Propulsion Conference, 1988KATSUAKI KOSAKA +4 more
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Effect of polyhedral oligomeric silsesquioxane on combustion performance of HTPB propellants
Combustion and Flame, 2022Hanying Du
exaly

