Theoretical stress mechanism and structural integrity of viscoelastic propellant grains with variable Poisson's ratio. [PDF]
Wang X+5 more
europepmc +1 more source
The fitting of parameters of the hyperacoustic entering device and afterburning chamber of the rocket-based-combined-cycle engine [PDF]
M.A. Katrenko, G. A. Gorbenko
openalex +1 more source
Experimental Verification of High-Temperature Resistance and High Resolution of Inductive Tip Clearance Measurement System. [PDF]
Zhao Z, Zhao L, Lyu Y, Liu Z.
europepmc +1 more source
Combustion Instability of Liquid Rocket Engines [PDF]
D. K. Sung, Hwanil Huh, Chae-Hoon Sohn
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Research on the influence of loading rate on the dynamic initiation fracture toughness of CMDB propellant. [PDF]
Zheng J+5 more
europepmc +1 more source
Advances in PBT Binder and Its Application in Propellants. [PDF]
Zhang N+9 more
europepmc +1 more source
Effects of NO in oxidant and initial temperature on working characteristics of MON-X/MMH liquid space thruster. [PDF]
Zhou YH+5 more
europepmc +1 more source
Liquid Carbon-Boron Cluster Additives for Mixed Amine-50. [PDF]
Mu X, Wang S, Yang F, Li H.
europepmc +1 more source
Sensors Layout Optimization Design of Rocket Sled Test System. [PDF]
Qian H, Wang W, Zhao X, Jiang Y.
europepmc +1 more source
Maintenance Decision-Making Using Intelligent Prognostics Within a Single Spare Parts Support System. [PDF]
Zhang B, Hu C, Zheng J, Pei H.
europepmc +1 more source