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The RBCC, or rocket-based combined cycle propulsion system, was one of the two types of propulsion systems that may have been tested in the Boeing X-43 experimental aircraft. The RBCC, or strutjet as it is sometimes called, is a combination propulsion system that consists of a ramjet, scramjet, and ducted rocket, where all three systems use a shared flow path.
A TBCC, or turbine-based combined cycle propulsion system, is a turbine engine combined with a ramjet and scramjet.
A TRCC, or turbo rocket combined cycle propulsion system, is another combination propulsion system that combines an afterburning turbine engine with a RBCC propulsion system.
See also
- SABRE (Synergistic Air Breathing Rocket Engine), a pre-cooled air-breathing rocket/RAM-jet engine based on General Dynamics' exploration of LACE concepts (Liquid Air Cycle Engine) by Reaction Engines, UK.
References
- Sketch of a RBCC propulsion system (scroll down to 7th picture)
- Sketch of a TBCC propulsion system (scroll down to 5th picture)
- Sketch of a TRCC propulsion system (scroll down to 9th picture)
- "Archived copy" (PDF). Archived from the original (PDF) on 2015-04-02. Retrieved 2015-02-27.
{{cite web}}: CS1 maint: archived copy as title (link)
External links
- Performance Evaluation of the NASA GTX RBCC Flowpath - Glenn Research Center - NASA
- Parametric Study Conducted of Rocket-Based, Combined-Cycle Nozzles - Glenn Research Center - NASA
- Aerojet Successfully Tests RBCC Single Thruster, Demonstrating Tri-Fluid Rocket Injector Capabilities - SpaceRef
- Hypersonic inlet studies for a small-scale rocket-based combined-cycle engine, Journal of propulsion and power, 2007, vol. 23, no6, pp. 1160–1167, AIAA.
- Rocket-Based Combined-Cycle Engine (RBCC): Ramrocket, University of Toronto, High-Speed Vehicle Propulsion Systems Group.
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