Turbo-Union RB199
Military aircraft turbofan jet engine

The Turbo-Union RB199 is a turbofan jet engine designed and built in the early 1970s by Turbo-Union, a joint venture between Rolls-Royce, MTU and Aeritalia.
The only production application was the Panavia Tornado, but it was used in the British Aerospace EAP whose 1st flight was on 8 August 1986 from Warton, without use of a spare engine on its total 259 flights, and is now in RAF Cosford Museum. It was also used in the first two Prototypes of the Eurofighter Typhoon, whose 1st flight, by DA1, was from Manching, Bavaria on 27 March 1994, and for a further two years before the EJ200 engines were installed - good reliability meant the spare RB199 engine supplied was never used.
Design and development
The RB199 originated with a requirement, in 1969, to power a new European multirole combat aircraft (MRCA) called the Panavia MRCA. The engine requirements to meet the Panavia MRCA specification were significant advances over current engines in thrust-to-weight ratio, fuel consumption and size. The final selection of the engine for the MRCA was made between a new European collaboration, Turbo Union, with the RB199, and Pratt & Whitney who proposed the JTF16. The Panavia MRCA would later be called the Panavia Tornado.
Advanced engine studies at Bristol Siddeley had already been done to support the BAC/Dassault AFVG and were based on the Pegasus two-spool arrangement. At Rolls-Royce, where the three-shaft RB211 engine was in development, three shafts were considered better. Rolls-Royce took over Bristol Siddeley in 1966 so the configuration for the RB199 was decided, a three-shaft engine, but fundamentally to Bristol's design and Bristol's higher technology.
The overall design concept for the international collaborative program, three shafts was decided by Rolls-Royce.
“Turbo-Union RB199” enters the record as military aircraft turbofan jet engine. Crown Archives preserves that source wording while asking what Turbo-Union, RB199 and Military can confirm, complicate or overturn.
Why this record matters
“Turbo-Union RB199” is worth following because a concise public description often conceals a longer documentary argument. Here, Turbo-Union, RB199 and Military provides the most credible route into that argument.
Named sources, stable identifiers and responsible institutions provide the strongest route from overview to verifiable evidence. The source revision retrieved here is dated Sep 9, 2026. The linked authority identifier is Q1810931. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1986, 1994, 1969 and 1966.
Overview language is designed for orientation and should not be treated as a substitute for the evidence cited beneath it. The lead is largely declarative, so disagreement and counter-evidence require a deliberate search beyond the opening account. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.
How to read it
Use the entry as an orientation point, then follow its citations and revision history. Names, dates and institutional relationships should be checked against the original record.
- Subject orientation
- Search vocabulary
- Locating named sources
The closest primary source, responsible institution and strongest cited specialist reference.
Three-step research path
- Establish the record: confirm the title “Turbo-Union RB199”, its source revision and the description used here.
- Expand the search: follow Turbo-Union RB199 primary sources, Turbo-Union RB199 archive and Turbo-Union research across catalogues and specialist indexes.
- Test the account: compare the strongest cited source with the responsible institution’s current record and note any disagreement.
Questions for further research
- Which source most directly establishes the central claim about “Turbo-Union RB199”?
- What terminology or title could unlock a more precise catalogue search?
- Which institution is responsible for the underlying evidence?
Search terms from this dossier
This entry incorporates text from “Turbo-Union RB199” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.