Theoretical characterization of mesoscopic structure of PBT propellant based on liquid film thickness. [PDF]
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A neural network based approach for thrust prediction in cold gas propulsion systems. [PDF]
Farhid M, Ghavidel Aghdam MR, Shameli M.
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Numerical simulation of stability of diffusion depth of deterrents into cylindrical nitrocellulose composite under different conditions. [PDF]
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Viscosity of rocket propellant (RP-1) at high temperatures and high pressures
Ilmutdin M. Abdulagatov+1 more
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Advances in Synthesis and Ignition Performance of Ionic Liquid-Hydrogen Peroxide Green Propellants. [PDF]
Zhang Y, Zhang X, Yin D, Zhang Q.
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Comparative Study on Extrusion 3D Printing of Solid Propellant Based on Plunger and Screw. [PDF]
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Reliability analysis of the solidification cooling of solid rocket motor grain material. [PDF]
Du J, Li Y, He Y.
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3 months transit time to Mars for human missions using SpaceX Starship. [PDF]
Kingdon J.
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