Possibility of increasing a specific pulse of liquid-propellant rocket engine through addition of inert helium gas into the combustion chamber [PDF]
С.А. Орлин, С.А. Орлин
openalex +1 more source
Theoretical characterization of mesoscopic structure of PBT propellant based on liquid film thickness. [PDF]
Shen YW +8 more
europepmc +1 more source
Fault Detection and Isolation Based on Structural Analysis: Application to a Multi-Engine Propulsion Cluster. [PDF]
Murata R +4 more
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Integrated Experimental-Numerical Analysis of HTPB Propellant Casting Optimization and Droplet Dynamics. [PDF]
Guo Z, Rossi R, Xue Y, Wu Y, Fu X.
europepmc +1 more source
Preparation Technology, Reactivity and Applications of Nano-Aluminum in Explosives and Propellants: A Review. [PDF]
Guo H, Zhang W, Pang W.
europepmc +1 more source
Investigation of aluminum agglomeration characteristics in solid propellants with Al/Mg particle additives. [PDF]
Zhang L +5 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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3 months transit time to Mars for human missions using SpaceX Starship. [PDF]
Kingdon J.
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