Results 21 to 30 of about 1,905,870 (344)
Proceedings, 2023 Composite propellants used in solid-fuel rockets commonly consists of an oxidizer, the most used being ammonium perchlorate, fuels such as powdered aluminum, compounds that control the burn rate (catalysts or inhibitors), and various other additives [...]
Sorin-Viorel Dolana +8 more
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Noncrystalline Binder Based Composite Propellant [PDF]
ISRN Aerospace Engineering, 2013 This study reports on propellants based on cross-linked HTPE binder plasticized with butyl nitroxyethylnitramine (BuNENA) as energetic material and HP 4000D as noncrystalline prepolymer. This binder was conducted with solid loading in the 85%. The results showed an improvement in processability, mechanical properties and burning rate.
Mohamed Abdullah +2 more
openaire +1 more source
Combustion and Propulsion Research [PDF]
, 1963 Combustion chemistry is one of the oldest branches of chemical science. Among its pioneers must be counted Lavoisier, Bunsen, and others whose names belong among those of the founders of chemical science.
Penner, S. S.
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Ferrocene-fullerene dyad as a novel burn rate modifier for propellants
Energetic Materials FrontiersThe burn rate of composite rocket propellants serves as a critical ballistic parameter in the construction of a rocket engine. Due to their large surface areas, carbon-based materials such as carbon nanotubes, graphene, and fullerene have demonstrated ...
Shrutika Sriramrao +3 more
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Cu–Co–O nano-catalysts as a burn rate modifier for composite solid propellants
Defence Technology, 2016 Nano-catalysts containing copper–cobalt oxides (Cu–Co–O) have been synthesized by the citric acid (CA) complexing method. Copper (II) nitrate and Cobalt (II) nitrate were employed in different molar ratios as the starting reactants to prepare three types
D. Chaitanya Kumar Rao +2 more
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Research progress in data-driven constitutive modeling of composite solid propellants
AIP AdvancesWith the continuous advancement of technology, composite solid propellants play an increasingly widespread and crucial role in fields such as aerospace and military applications.
Bin Yuan, Hongfu Qiang, Chunguo Yue
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Numerical Analysis of Solid Rocket Motor Instabilities With AP Composite Propellants [PDF]
, 1999 A non-steady model for the combustion of ammonium perchlorate composite propellants has been developed in order to be incorporated into a comprehensive gasdynamics model of solid rocket motor flow fields.
Beddini, Robert A. +3 more
core
On the combustion of heterogeneous AP/HTPB composite propellants: A review
Fuel, 2019 The combustion of ammonium perchlorate (AP) in a polymer binder matrix of hydroxyl-terminated-polybutadiene (HTPB) is reviewed, covering the experimental and modeling approaches explored for over a half-century.
Claresta N. Dennis, Brian T. Bojko
semanticscholar +1 more source
Molecular Oncology, EarlyView.Pharmacologic ascorbate (vitamin C) increases ROS, disrupts cellular metabolism, and induces DNA damage in CRPC cells. These effects sensitize tumors to PARP inhibition, producing synergistic growth suppression with olaparib in vitro and significantly delayed tumor progression in vivo. Pyruvate rescue confirms ROS‐dependent activity.
Nicolas Gordon +13 more
wiley +1 more source
Properties of high-energy propellants based on oxygen-enriched thermoplastic elastomer binders
FirePhysChemComposite propellants are widely used in applications ranging from gas generators and small rockets to large rocket systems in space programs. This study presents a novel thermoplastic elastomer (TPE) binder system based on oxygen-enriched polyether ...
Vladica S Bozic
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