No AccessExperimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet ModeTakeshi Kanda, Kanenori Kato, Kouichiro Tani, Kenji Kudo and Atsuo MurakamiTakeshi KandaJapan Aerospace Exploration AgencySearch for more papers by this author, Kanenori KatoJapan Aerospace Exploration AgencySearch for more papers by this author, Kouichiro TaniJapan Aerospace Exploration AgencySearch for more papers by this author, Kenji KudoJapan Aerospace Exploration AgencySearch for more papers by this author and Atsuo MurakamiJapan Aerospace Exploration AgencySearch for more papers by this authorSession: ABP-3: Air Breathing Propulsion for High Speed FlightPublished Online:21 Jun 2012https://doi.org/10.2514/6.2006-223SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byThe overall layout of rocket-based combined-cycle engines: a review15 April 2019 | Journal of Zhejiang University-SCIENCE A, Vol. 20, No. 3Pumping Performance or RBCC Engine under Sea Level Static Condition1 Jan 2008 | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 56, No. 650Pumping Performance of RBCC Engine under Sea Level Static Condition1 Jan 2008 | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 56, No. 651 What's Popular 44th AIAA Aerospace Sciences Meeting and Exhibit 09 January 2006 - 12 January 2006Reno, Nevadahttps://doi.org/10.2514/6.2006-223 Crossmark TopicsAircraft EnginesCombustion ChambersCombustorsFuel InjectionIgnition SystemsJet EnginesPropellantPropulsion and PowerRamjetRocketryRocketsScramjet KeywordsCombustorsRocketsRocket Based Combined Cycle EnginesFuel InjectionAerodynamic TestingCombustion EfficiencyPropellantRamjetThrust AugmentationModel RocketDigital Topics Aerospace Systems, Operations and Life Cycle