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Progress in research on composite cryogenic propellant tank for large aerospace vehicles
Composites Part A: Applied Science and Manufacturing, 2021Lijie Qu
exaly
Erosive burning of composite solid propellants
Combustion and Flame, 1966A model is proposed for erosive burning of ammonium perchlorate composite wolid propellants. It is assumed that combustion takes place in the turbulent boundary layer and that the turbulent flame consists of distorted ‘flamelets’ but otherwise retains on a molecular scale the characteristics of a laminar flame.
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Application of spherical ultrafine CuO@AP with core–shell in AP/HTPB composite solid propellant
Journal of Thermal Analysis and Calorimetry, 2023Jie Liu, Haomiao Yu, Deqi Wang
exaly
Effect of Pressure on Mechanical Properties of Composite Propellant
Propellants, Explosives, Pyrotechnics, 2021exaly
An Overview of Composite Propellant Burning
International Journal of Engineering Trends and Technology, 2015A. M Hegab, S. A Gutub
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A Model of AP/HTPB Composite Propellant Combustion in Rocket-Motor Environments
Combustion Science and Technology, 2008Vigor Yang
exaly
SYNOPTIC: Composite Propellant Combustion
AIAA Journal, 1970R. L. DERR, J. R. OSBORN
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Aging in Composite Propellant Grains
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2004Gerhard Reeling Brouwer +2 more
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