Reaction Engines Scimitar

From Wikipedia, the free encyclopedia
Jump to: navigation, search

The Reaction Engines Scimitar is a derivative of the SABRE engine technology, but intended for airliners (the Reaction Engines A2 concept), rather than space launch applications. Consequently, most of the Scimitar engine technology is similar to Sabre but designed for much longer life.[1] Both engines are designed around existing gas turbine, and ramjet technology, but the Scimitar engine lacks the rocket features and has high bypass features for greater efficiency. The engines burn hydrogen as fuel.[2]

The incorporation of lightweight heat exchangers in the main thermodynamic cycles of these engines is a new feature to aerospace propulsion.[citation needed] Similar studies of intercoolers used on jet engines show significant improvement of efficiency.[3]

References[edit]