; Bench engines : Ten prototype engines were built for testing by both Rolls-Royce and Turbomeca. • Adour Mk 102 - Second production variant with the addition of part-throttle reheat. In May 2007, following the retirement of the last 16 Jaguars from
No. 6 Squadron RAF, based at
RAF Coningsby, the Adour 106 has been phased out of RAF service. • Adour Mk 801 - For
Mitsubishi F-1 &
T-2 (
JASDF) • TF40-IHI-801A - Licence-built version of Mk 801 by
Ishikawajima-Harima for Mitsubishi F-1 & T-2 (JASDF) • Adour Mk 804 - Licence-built by HAL for Indian Air Force phase 2 Jaguars • Adour Mk 811 - Licence-built by HAL for Indian Air Force phase 3 to 6 Jaguars; rated at 8400 lbs of maximum thrust. BAe-built Jaguars were initially powered with two Adour 804E turbofans. • Adour Mk 821 - Engine upgrade of Mk804 and Mk811 engines, was under development for the Indian Air Force Jaguar aircraft.
Dry (non-afterburning) • Adour Mk 151-01 Used by the Royal Air Force training aircraft fleet • Adour Mk 151-02 - Used by the
Red Arrows • Adour Mk 851 • Adour Mk 861 • Adour Mk 871 - Used by Hawk 200 • F405-RR-401 - Similar configuration to Mk 871, for US Navy T-45 Goshawk. • Adour Mk 951 - Designed for the latest versions of the
BAE Hawk and powering the
BAE Taranis and
Dassault nEUROn UCAV technology demonstrators. The Adour Mk 951 is a more fundamental redesign than the Adour Mk 106, with improved performance (rated at thrust) and up to twice the service life of the 871. It features an all-new fan and combustor, revised HP and LP turbines, and introduces Full Authority Digital Engine Control (FADEC). The Mk 951 was certified in 2005. • F405-RR-402 - Upgrade of F405-RR-401, incorporating Mk 951 technology, certified 2008. Did not enter into service due to funding issues.
Higher bypass • A high-bypass engine built around the core of the Adour and intended as a
Spey replacement was developed by Rolls-Royce in 1967 as the
Rolls-Royce RB.203 Trent. == Applications ==