Volume 17, Issue 2 No AccessSCCREAM: A Conceptual Rocket-Based Combined-Cycle Engine Performance Analysis ToolJohn R. Olds and John E. BradfordJohn R. Olds Georgia Institute of Technology, Atlanta, Georgia 30332-0150Search for more papers by this author and John E. Bradford Georgia Institute of Technology, Atlanta, Georgia 30332-0150Search for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/2.5746SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byThermodynamic performance modeling, optimization and numerical simulation of RBCC ejector modePropulsion and Power Research, Vol. 14Experimental study of rocket plume expansion in the rocket-based combined-cycle engine under the ejector modeAerospace Science and Technology, Vol. 107Multidisciplinary design optimization of a wide speed range vehicle with waveride airframe and RBCC engineEnergy, Vol. 235An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit missionEnergy, Vol. 193Investigation on the performance and feasibility of RBCC-based access-to-space via multi-objective design optimizationActa Astronautica, Vol. 157Novel Inducement to Unstart of a Parallel Modular Hypersonic InletChengpeng Wang, Longsheng Xue and Keming Cheng20 December 2018 | AIAA Journal, Vol. 57, No. 2Conceptual design and optimization of scramjet engines using the exergy method7 November 2018 | Journal of the Brazilian Society of Mechanical Sciences and Engineering, Vol. 40, No. 12Effect of thermal choking on ejection process in a rocket-based combined cycle engineApplied Thermal Engineering, Vol. 116Simple Modification on Performance Prediction Model for an External Nozzle with Clustered EntranceTatsushi Isono, Noboru Sakuranaka and Sadatake Tomioka5 January 2017Performance Requirement Analysis and Weight Estimation of Reusable Launch Vehicle using Rocket based Air-breathing EngineJournal of the Korean Society of Propulsion Engineers, Vol. 19, No. 6Investigation on Effective Sampling Strategy for Multi-objective Design Optimization of RBCC Propulsion Systems via Surrogate-assisted Evolutionary AlgorithmsProcedia Engineering, Vol. 99Combined‐Cycle Engines15 December 2010Theoretical Investigation of the Compression Augmentation Effects of Variable Area EjectorsMike Koupriyanov and Jason Etele14 June 2012Experimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet Mode Takeshi Kanda , Kanenori Kato , Kouichiro Tani , Kenji Kudo and Atsuo Murakami 23 May 2012 | Journal of Propulsion and Power, Vol. 23, No. 6Hypersonic Inlet Studies for a Small Scale Rocket-Based Combined-Cycle Engine Giulio Riva , Adolfo Reggiori and Giambattista Daminelli 23 May 2012 | Journal of Propulsion and Power, Vol. 23, No. 6Conceptual Study of a Rocket-Ramjet Combined-Cycle Engine for an Aerospace Plane Takeshi Kanda , Kouichiro Tani and Kenji Kudo 23 May 2012 | Journal of Propulsion and Power, Vol. 23, No. 2Pressure Recovery Characteristics of Diverging Mixing Tubes for Ejector-JetsEijiro Kitamura, Sadatake Tomioka, Noboru Sakuranaka, Syuichi Watanabe and Goro Masuya15 June 2012Performance of a Dual-Mode Combustor with Multistaged Fuel Injection Kan Kobayashi , Sadatake Tomioka , Kanenori Kato , Atsuo Murakami and Kenji Kudo 23 May 2012 | Journal of Propulsion and Power, Vol. 22, No. 3Experimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet ModeTakeshi Kanda, Kanenori Kato, Kouichiro Tani, Kenji Kudo and Atsuo Murakami21 June 2012Pressure Recovery in Mixing Ducts of Ejector-RamjetsEijiro Kitamura, Tohru Mitani, Shenghong Huang and Goro Masuya19 June 2012Aerodynamic Experiment on an Ejector-Jet Shigeki Aoki , Jongsun Lee , Goro Masuya , Takeshi Kanda and Kenji Kudo 23 May 2012 | Journal of Propulsion and Power, Vol. 21, No. 3Performance of a Dual-Mode Combustor with Multi-Staged Fuel InjectionKan Kobayashi, Sadatake Tomioka, Kanenori Kato, Atsuo Murakami, Kenji Kudo and Tohru Mitani26 June 2012Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane Takeshi Kanda and Kenji Kudo 23 May 2012 | Journal of Propulsion and Power, Vol. 19, No. 5Experimental Investigation of an Ejector-JetShigeki Aoki, Jongsun Lee, Goro Masuya, Takeshi Kanda, Kenji Kudo and Atsuo Murakami11 November 2012A Conceptual Study of a Combined Cycle Engine for an Aerospace PlaneTakeshi Kanda and Kenji Kudo26 June 2012Rapid Prediction of Aftbody Nozzle Performance in SCCREAMJohn Bradford26 June 2012 What's Popular Volume 17, Number 2March 2001 Crossmark TopicsAircraft EnginesCombustion ChambersCombustorsEnergyEnergy ConversionEnergy Forms, Production and ConversionFuel InjectionHeat EnginesIgnition SystemsMonopropellantsNozzlesPropulsion and PowerRocket EngineRocket PropellantRocket PropulsionRocketryRockets KeywordsSimulated Combined Cycle Rocket Engine Analysis ModuleConservation of MassTrajectory OptimizationLaunch Vehicle DesignFORTRANRamjetAerodynamic DragScramjet EnginesRocketsCombustorsPDF Published online23 May 2012