Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF / / H. Douglas Perkins, Scott R. Thomas, and William D. Pack

• Autore: Perkins H. Douglas
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996
• Descrizione fisica: 1 online resource (13 pages) : illustrations
• Soggetto topico: Flexibility; Engine tests; Hypersonic speed; Hypersonic wind tunnels
• Persona (resp. second.): ThomasScott R.; PackWilliam D.
• Note generali: Title from title screen (viewed Aug. 3, 2016).; "December 1996"--Report documentation page.; "Prepared for the 35th Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-10, 1997."; "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.; "AIAA-97-0565."
• Nota di bibliografia: Includes bibliographical references (pages 6-7).
• Altri titoli varianti: Mach five to seven rocket based combined cycle propulsion system testing at NASA Lewis Research Center hypersonic tunnel facility
• Titolo autorizzato: Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910707307103321
• Lo trovi qui: Univ. Federico II