Results 181 to 190 of about 52,081 (256)

Preparation of Polydopamine Functionalized HNIW Crystals and Application in Solid Propellants. [PDF]

Polymers (Basel)
Zhu F, Liu C, Yang D, Li G.
europepmc   +1 more source

Research on Crack Propagation of Nitrate Ester Plasticized Polyether Propellant: Experiments and Simulation. [PDF]

Materials (Basel)
Liu H, Wang J, Fu X.
europepmc   +1 more source

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

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

Reliability analysis of the solidification cooling of solid rocket motor grain material. [PDF]

PLoS One
Du J, Li Y, He Y.
europepmc   +1 more source

Energetic Nitrate-Based Polymer-Bonded Explosives Derived from Sustainable Aza-Michael Reactions. [PDF]

ACS Omega
Sheela G, Periya VK, Gopalakrishnan S, Sasidharakurup R.   +3 more
europepmc   +1 more source

UV-Assisted Material Extrusion Additive Manufacturing of Double-Base Propellant. [PDF]

Polymers (Basel)
Li M, Gao Y, Wang Q, Yang W, Gao GL, Jiang Z.   +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
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Combustion of AP/HTPB laminate propellants

37th Joint Propulsion Conference and Exhibit, 2001
The combustion of AP/HTPB laminate propellants has been investigated experimentally and theoretically. The experiments used simultaneous UV emission and transmission imaging to obtain information about the flame structure and the burning surface profile.
M. Brewster, G. Knott, B. Chorpening
openaire   +1 more source