Study on Rheological Properties and Pouring Process of Hydroxyl-Terminated Polybutadiene (HTPB) Propellants. [PDF]
Polymers (Basel), 2023 Wang H, Ji Y, Jiang X, Li Z.
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Defence TechnologyDuring the storage of composite propellants, the migration of plasticizers and other unbonded additives at the interfaces of liner adhesives has garnered significant attention in understanding liner failure mechanisms, aging processes, and safety ...
Jie Wang +6 more
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Transient processes in the combustion of nitramine propellants [PDF]
A transient combustion model of nitramine propellants is combined with an isentropic compression shock formation model to determine the role of nitramine propellant combustion in DDT, excluding effects associated with propellant structural properties or ...
Cohen, N. S., Strand, L. D.
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Fragmentation of Ammonium Nitrate Particles under Thermal Cycling [PDF]
, 2018 Ammonium nitrate finds application in explosives and chlorine-free slow-burning propellants. Different phases are known for this ammonium salt, each of them featured by peculiar bulk densities.
Garg, Priya, Maggi, Filippo
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Numerical Conversion Method for the Dynamic Storage Modulus and Relaxation Modulus of Hydroxy-Terminated Polybutadiene (HTPB) Propellants. [PDF]
Polymers (Basel), 2022 Ji Y, Cao L, Li Z, Chen G, Cao P, Liu T.
europepmc +1 more source
Demonstration of a sterilizable solid rocket motor system [PDF]
A solid propellant rocket motor containing 60.9 Kg (134-lb) of propellant was successfully static fired after being subjected to eight heat sterilization cycles (three 54-hour cycles plus five 40-hour cycles) at 125 C (257 F).
Lambert, W. L. +2 more
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Модель гибридного ракетного двигателя. Вычисления, проект и испытания [PDF]
, 2009 На даний час і у майбутньому ракетні двигуни будуть найголовнішими засобами виводу на орбіту космічних транспортних апаратів. В даний час найважливішою вимогою при проектуванні двигуна ракети є зменшення її вартості і максимальне збільшення енерговіддачі.
Folusiak, M. +5 more
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Nitramine smokeless propellant research [PDF]
A transient ballistics and combustion model is derived to represent the closed vessel experiment that is widely used to characterize propellants. A computer program is developed to solve the time-dependent equations, and is applied to explain aspects of ...
Cohen, N. S., Strand, L. P.
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Deep learning-assisted finite element simulation for characterizing the microstructure-dependent stress field of HTPB propellant [PDF]
AIP AdvancesThis paper proposes an end-to-end deep learning framework based on the U-Net architecture to directly map the microstructure of Hydroxyl-terminated polybutadiene (HTPB) propellant to its mesoscopic von Mises stress field.
Bin Yuan, Hongfu Qiang, Xueren Wang
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Heterogeneous fuel for hybrid rocket [PDF]
, 1996 Heterogeneous fuel compositions suitable for use in hybrid rocket engines and solid-fuel ramjet engines, The compositions include mixtures of a continuous phase, which forms a solid matrix, and a dispersed phase permanently distributed therein.
Stickler, David B.
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