Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber / / Mary F. Wadel and Michael L. Meyer

• Autore: Wadel Mary F.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1996
• Descrizione fisica: 1 online resource (10 pages) : illustrations
• Soggetto topico: Rocket engines; Combustion chambers; Thrust chambers; Mass flow; Liquid hydrogen; Cooling; High aspect ratio; Performance tests
• Persona (resp. second.): MeyerMichael L.
• Note generali: Title from title screen (viewed July 19, 2016).; "June 1996"--Report documentation page.; "Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996."; "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.; "AIAA-96-2584."
• Nota di bibliografia: Includes bibliographical references (page 10).
• Altri titoli varianti: Validation of high aspect ratio cooling in a 89 kN
• Titolo autorizzato: Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910707356003321
• Lo trovi qui: Univ. Federico II