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Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed


Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed
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Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed


Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed
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Author : Shaye Yungster
language : en
Publisher:
Release Date : 1999

Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed written by Shaye Yungster and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Chemical equilibrium categories.




Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed


Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed
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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher: Independently Published
Release Date : 2018-09-25

Analysis Of A New Rocket Based Combined Cycle Engine Concept At Low Speed written by National Aeronautics and Space Adm Nasa and has been published by Independently Published this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-09-25 with Science categories.


An analysis of the Independent Ramjet Stream (IRS) cycle is presented. The IRS cycle is a variation of the conventional ejector-Ramjet, and is used at low speed in a rocket-based combined-cycle (RBCC) propulsion system. In this new cycle, complete mixing between the rocket and ramjet streams is not required, and a single rocket chamber can be used without a long mixing duct. Furthermore, this concept allows flexibility in controlling the thermal choke process. The resulting propulsion system is intended to be simpler, more robust, and lighter than an ejector-ramjet. The performance characteristics of the IRS cycle are analyzed for a new single-stage-to-orbit (SSTO) launch vehicle concept, known as "Trailblazer." The study is based on a quasi-one-dimensional model of the rocket and air streams at speeds ranging from lift-off to Mach 3. The numerical formulation is described in detail. A performance comparison between the IRS and ejector-ramjet cycles is also presented. Yungster, S. and Trefny, C. J. Glenn Research Center NASA/TM-1999-209393, NAS 1.15:209393, E-11824, AIAA Paper 99-2393, ICOMP-99-05



35th Aiaa Asme Sae Asee Joint Propulsion Conference And Exhibit


35th Aiaa Asme Sae Asee Joint Propulsion Conference And Exhibit
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Author :
language : en
Publisher:
Release Date : 1999

35th Aiaa Asme Sae Asee Joint Propulsion Conference And Exhibit written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Airplanes categories.




Response Surface Modeling Of Combined Cycle Propulsion Components Using Computational Fluid Dynamics


Response Surface Modeling Of Combined Cycle Propulsion Components Using Computational Fluid Dynamics
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Author :
language : en
Publisher:
Release Date : 2002

Response Surface Modeling Of Combined Cycle Propulsion Components Using Computational Fluid Dynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with categories.




Computational Analysis Of The Combustion Processes In An Axisymmetric Rbcc Flowpath


Computational Analysis Of The Combustion Processes In An Axisymmetric Rbcc Flowpath
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Author :
language : en
Publisher:
Release Date : 2001

Computational Analysis Of The Combustion Processes In An Axisymmetric Rbcc Flowpath written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with categories.




An Air Breathing Launch Vehicle Concept For Single Stage To Orbit


An Air Breathing Launch Vehicle Concept For Single Stage To Orbit
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Author : Charles J. Trefny
language : en
Publisher:
Release Date : 1999

An Air Breathing Launch Vehicle Concept For Single Stage To Orbit written by Charles J. Trefny and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.




Institute For Computational Mechanics In Propulsion Icomp


Institute For Computational Mechanics In Propulsion Icomp
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Author :
language : en
Publisher:
Release Date : 2001

Institute For Computational Mechanics In Propulsion Icomp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with categories.




Monthly Catalog Of United States Government Publications


Monthly Catalog Of United States Government Publications
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Author :
language : en
Publisher:
Release Date : 2000

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Government publications categories.




40th Aiaa Aerospace Sciences Meeting Exhibit


40th Aiaa Aerospace Sciences Meeting Exhibit
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Author :
language : en
Publisher:
Release Date : 2002

40th Aiaa Aerospace Sciences Meeting Exhibit written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Aeronautics categories.




Astrodynamics


Astrodynamics
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Author :
language : en
Publisher:
Release Date : 2000

Astrodynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Astrodynamics categories.


Vols. 1-2, 4 contain the Proceedings of the Society's 3rd (1956)-5th (1958) annual meeting; v. 3 contains the Proceedings of the Western Regional Meeting of the AAS, Aug. 1958.