Results 201 to 210 of about 2,146 (234)
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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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A Study of a Novel Additive for HTPB Propellant
1976Abstract : Experimental studies were conducted to define the utility regimes of graphite linters (chopped graphite fiber ranging from 50 to 200 micrometers) with respect to burn rate augmentation, acoustic stabilization and processing improvement in HTPB composite propellant. Linter utility regimes were defined with respect to burn rate reproducibility
M. W. Beckstead +2 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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A model of AP/HTPB composite propellant combustion
38th Aerospace Sciences Meeting and Exhibit, 2000Weidong Cai, Vigor Yang
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Estimation of burning characteristics of AP/HTPB composite solid propellant using a sandwich model
Combustion and Flame, 2020Chaitanya Vijay
exaly
A Model of AP/HTPB Composite Propellant Combustion in Rocket-Motor Environments
Combustion Science and Technology, 2008Vigor Yang
exaly