Results 141 to 150 of about 12,705 (201)

Combustion experiments of HTPB/RFNA mixed hybrid propellants

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

Development of low viscosity prepolymer with ring strained side chains to enhance binder stability and explosive power. [PDF]

Sci Rep
Kim D, Moon Y, Kim MI, Kim H, Jung IH.
europepmc   +1 more source

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

Study on the Rheological Properties of BGAP Adhesive and Its Propellant. [PDF]

Molecules
Shao Y, Xu S, Xu H, Xie W, Zhang Z, Yao E, Jiang H.   +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

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

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

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

Accelerated Aging Tests of HTPB-Based Propellants

, 2018
In the late twentieth century, liquid and solid propulsion technologies have been integrated into hybrid engines currently apllied in propulsion launch vehicles and missiles. The reaction of polyol (HTPB) and diisocyanate (IPDI) provides the most versatile of the binders in the production of solid propellants due to its ability to withstand high loads ...
Roberta Jachura Rocha
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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