File:Turbine Based Combined Cycle (TBCC) engine integration.svg

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English: Schematic diagram for a Turbine Based Combined Cycle (TBCC) engine. 1) low speed inlet 2) high speed inlet 3) turbojet 4) dual-mode scramjet flowpath 5) high speed nozzle 6) low speed nozzle
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Source Own work based on diagram found at http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060055388_2006256613.pdf (page 2)
Author NASA Langley Research Center

This is a derivative work of an image licensed with PD-USGov-NASA

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Public domain This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)
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Date/TimeThumbnailDimensionsUserComment
current18:19, 21 July 2011Thumbnail for version as of 18:19, 21 July 2011889 × 163 (19 KB)Nubifer (talk | contribs){{Information |Description ={{en|1=Schematic diagram for a Turbine Based Combined Cycle (TBCC) engine. 1) low speed inlet 2) high speed inlet 3) turbojet 4) dual-mode scramjet flowpath 5) high speed nozzle 6) low speed nozzle}} |Source =Own wor

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