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FLIGHT PERFORMANCE OF THE REIMEI MICROSATELLITE ATTITUDE DETERMINATION SYSTEM
2001-01-0143 Study on Lean Burn Gas Engine Using Pilot Oil as the Ignition Source
Effects of Particle Size on Microstructure of the Matrix Alloy in Aluminium Matrix Composites
Electro Magnetic Formation Flight for LEO Satellites
Study on lean burn gas engine using pilot oil as the ignition source
Experimental investigation on the crushing properties of carbon fibre braided composite tubes