Rocket-based combined cycle: Difference between revisions
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''See also'': [[air-augmented rocket]] |
''See also'': [[air-augmented rocket]] |
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==External links== |
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[http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210953.pdf Performance Evaluation of the NASA GTX RBCC Flowpath] |
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[http://www.grc.nasa.gov/WWW/RT/RT1997/5000/5880steffen.htm Parametric Study Conducted of Rocket-Based, Combined-Cycle Nozzles] |
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{{DEFAULTSORT:Rocket-Based Combined Cycle}} |
{{DEFAULTSORT:Rocket-Based Combined Cycle}} |
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Revision as of 00:12, 7 April 2010
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The RBCC, or Rocket-Based Combined Cycle, is one of the two types of propulsion systems that may be used in the Boeing X-43 experimental aircraft.
It has been speculated that aerospace engineer Richard Foster originally introduced the term RBCC into the aerospace nomenclature.
A TBCC is a turbine engine with a ramming and scramming jet with ignition in 2 stages that fire on Hp mach.
See also: air-augmented rocket
External links
Performance Evaluation of the NASA GTX RBCC Flowpath Parametric Study Conducted of Rocket-Based, Combined-Cycle Nozzles
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