File:Turbine Based Combined Cycle (TBCC) engine integration.svg
_engine_integration.svg){kind=small}
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Summary
| Description |
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 |
| Date | |
| 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
Licensing
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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/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 18:19, 21 July 2011 | | 889 × 163 (19 KB) | Nubifer | {{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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_engine_integration.svg){kind=link}