Rocket-based combined cycle

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by 66.8.150.109 (talk) at 20:44, 19 July 2020 (added past tense). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

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.[1]

It has been speculated that aerospace engineer Richard Foster originally introduced the term RBCC into the aerospace nomenclature.[citation needed]

A TBCC, or Turbine Based Combined Cycle propulsion system, is a turbine engine combined with a ramjet and scramjet.[2]

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.[3]

See also

External links

References

  1. ^ Sketch of a RBCC propulsion system (scroll down to 7th picture)
  2. ^ Sketch of a TBCC propulsion system (scroll down to 5th picture)
  3. ^ Sketch of a TRCC propulsion system (scroll down to 9th picture)
  4. ^ "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)