Results 121 to 130 of about 370 (179)

Combustion experiments of HTPB/RFNA mixed hybrid propellants

Indian Journal of Science and Technology, 2011
openaire   +2 more sources

Research on Passivation Simulation of Plasticizer N-Butylnitroxyethylnitramine (BuNENA) in Hydroxy-Terminated Polyether (HTPE) Propellants. [PDF]

Polymers (Basel)
Guo Z, Rossi R, Deng R, Wu Y, Liu H, Hao L, Fu X.   +6 more
europepmc   +1 more source

Study on rheological properties of composite propellant slurry in the mixing process by using experimental and numerical simulation. [PDF]

RSC Adv
Guo Z, Fu X, Rossi R.
europepmc   +1 more source

PAH Induction upon Pyrolysis of Hydroxyl-Terminated Polybutadiene-Based Solid Rocket Fuels. [PDF]

J Phys Chem A
Karpovych V, Haiduk N, Oga E, Bala N, Kubátová A, Kozliak E, Sulkes M.   +6 more
europepmc   +1 more source

Molecular Dynamics Simulation of Interfacial Effects in PBT-Based Azide Propellants Under Tensile Deformation. [PDF]

Polymers (Basel)
Liao H, Lv J, Cao P, Cao L, Huang R, Tang X.   +5 more
europepmc   +1 more source

Advances in Structural Reliability Analysis of Solid Propellant Grain: A Comprehensive Review. [PDF]

Polymers (Basel)
Tang C, Qiang H, Geng T, Wang X, Zhang F.   +4 more
europepmc   +1 more source

Effect of Octa(perfluorodecyl)-Type Polyhedral Oligomeric Silsesquioxanes on Combustion Characteristics of the Mixed Nitrate Ester Gun Propellant. [PDF]

ACS Omega
Du X, Liu X, Zhao L, Wang X, Li G.
europepmc   +1 more source

Damage characteristics and failure mechanism analysis of NEPE propellant at high strain rates. [PDF]

Sci Rep
Sun Z, Xu J, Zhou C, Chen X, Guo Z, Song Q.   +5 more
europepmc   +1 more source

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HTPB Propellant Aging

Journal of Spacecraft and Rockets, 1981
Three HTPB propellants, varying in solids loading from 88% to 91%, were selected and developed for evaluation studies including aging. The 88%-solids propellant was verified to fit a previously developed aging model. The aging model has been further successfully applied to the measured mechanical-property aging data for the higher-solids propellants ...
A.G. Christiansen, L.H. Layton, R.L. Carpenter   +2 more
openaire   +1 more source

HNF/HTPB BASED COMPOSITE PROPELLANTS

International Journal of Energetic Materials and Chemical Propulsion, 2002
In a search for new storable high performance propellants for the European Space Agency (ESA), the solid oxidiser Hydrazinium Nitroformate (HNF) was identified as a very promising ingredient for a new storable composite propellant. Two distinct advantages of HNF based propellants over presently used Ammonium Perchlorate (AP) based propellants rvere the
Heijden, A.E.D.M. van der, Keizers, H.L.J., Veltmans, W.H.M.   +2 more
openaire   +2 more sources