[Reports] / Amer.inst.of aeronautics and astronautics. N 89-2682 : Rapid methodology for design and performance prediction of integrated SCRAMJET/hypersonic vehicle : Rep. presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf.,Monterey(Ca),July 10-12,1989 / H.Ikawa, 1989. - 12 p. - Текст : непосредственный.