Vai al contenuto principale della pagina

Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept / / M.M. Fazah and J.M. Cramer



(Visualizza in formato marc)    (Visualizza in BIBFRAME)

Autore: Fazah M. M. Visualizza persona
Titolo: Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept / / M.M. Fazah and J.M. Cramer Visualizza cluster
Pubblicazione: Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , May 1998
Descrizione fisica: 1 online resource (vii, 46 pages) : illustrations
Soggetto topico: Injectors
Gas-gas interactions
Rocket engines
Firing (igniting)
Engine tests
Test firing
Rocket firing
Fuel combustion
Propellant combustion
Hydrogen fuels
Note generali: "May 1998."
"Performing organization: George C. Marshall Space Flight Center"--Report documentation page.
Nota di bibliografia: Includes bibliographical references (page 46).
Altri titoli varianti: Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle
Titolo autorizzato: Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910705862403321
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui