Theoretical Investigation of the Bond Dissociation of Hydroxyl Terminated Polybutadiene Binder and Effect on Mechanical Properties [PDF]
Acta Chimica Sinica, 2012 Wen-Ming Wu +3 more
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Saturated hydrocarbon polymeric binder for advanced solid propellant and hybrid solid grain [PDF]
Saturated hydrocarbon polymeric binder for solid propellant and hybrid propellant ...
Potts, J. E.
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Decomposition in HTPB bonded HMX followed by heat generation rate and chemiluminescence [PDF]
, 2018 The decomposition in HTPB bonded HMX was characterized with two highly sensitive methods: heat flow microcalorimetry (HFMC) and Chemiluminescence (CL). The material is stabilized with a phenolic antioxidant. The heat generation (HFMC) rate was determined
Bohn, M., Käser, F.
core
Large-Scale Hybrid Motor Testing [PDF]
Hybrid rocket motors can be successfully demonstrated at a small scale virtually anywhere. There have been many suitcase sized portable test stands assembled for demonstration of hybrids. They show the safety of hybrid rockets to the audiences.
Story, George
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High-energy, curable polycyclopentadiene binder for solid rocket propellants [PDF]
, 1988 Diels Alder polymerization of cyclopentadiene ( CPD ) has been carried out at 170°C under inert atmosphere. The resulted polymer has a low bulk viscosity, 7.4 cps, and a number average molecular weight Mn up to 3000.
Ning, Jian guo
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Hybrid propulsion technology program: Phase 1. Volume 3: Thiokol Corporation Space Operations [PDF]
Three candidate hybrid propulsion (HP) concepts were identified, optimized, evaluated, and refined through an iterative process that continually forced improvement to the systems with respect to safety, reliability, cost, and performance criteria. A full
Schuler, A. L., Wiley, D. R.
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Combustion chemistry of solid propellants [PDF]
Several studies are described of the chemistry of solid propellant combustion which employed a fast-scanning optical spectrometer. Expanded abstracts are presented for four of the studies which were previously reported.
Baer, A. D., Ryan, N. W.
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Chemical Engineering TransactionsThis study investigates the effect of curing parameters (Rt) on the mechanical properties and bond strength of propellants and liners in rocket motors compared to the design values.
Thirapat Kitinirunkul +3 more
doaj
Hybrid Propulsion Technology Program [PDF]
Future launch systems of the United States will require improvements in booster safety, reliability, and cost. In order to increase payload capabilities, performance improvements are also desirable.
Holzman, A. L., Jensen, G. E.
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Influence of Process Aids on Solid-Liquid Interfacial Properties of Three-Component Hydroxyl-Terminated Polybutadiene Propellants. [PDF]
Polymers (Basel)Zhang X +7 more
europepmc +1 more source