Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber
32nd Joint Propulsion Conference and Exhibit ; 1996 ; Lake Buena Vista , FL , U.S.A.
1996-01-01
Conference paper
Electronic Resource
English
Automatic Landing of a High-Aspect-Ratio Aircraft without Using the Thrust
Springer Verlag | 2015
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