Adour UETF

Introduction

The Adour Uninstalled Engine Test Facility (UETF) is operated by S & C Thermofluids on behalf of the Defence Science and Technology Laboratory (Dstl), an agency of the Ministry of Defence.

The laboratory offers a low cost propulsion research capability at large scale.

The Adour engine is manufactured by jointly by Rolls-Royce and Turbomeca and variants of the engine are used in the Hawk, Jaguar and Mitsubishi F-1 and T-2 aircraft.

The UETF is capable of operating both the Mk.151 (Hawk) and Mk.104 (Jaguar) engines.

In dry mode, the Adour is capable of producing around 23.5kN of thrust. The Adour 104 has reheat capability which can take the thrust to 37.5kN.

In the UETF, the Mk.104 engines are used and these are run in the dry mode.

Cutaway of the Adour engine core

Reheat nozzle of the Adour Mk.104 engine

Dstl's Adour Uninstalled Engine Test Facility operated by S & C

The key features of the 104 engine are as follows:

  • Bypass ratio 0.75-0.8
  • Two shaft
  • Five stage axial compressor
  • Two stage turbine
  • Mass flow approximately 40kg/s
  • Thrust 23.5kN (sea level static - dry)
  • Exhaust temperature up to 750 ºC
  • NPR up to 2.0 (sea level static)
  • Fuel - AVTUR

The engine is mounted on a support frame which is housed within a dedicated hush-house to reduce noise levels during engine test.

 

Back to Experimental page

 

Jaguar aircraft powered by two Rolls-Royce Adour Mk.104 engines

 

 

 

 

 

Engine test facility control panel

Adour Mk.104 engine mounted in the UETF



© S & C Thermofluids Ltd 2024

S & C Thermofluids Ltd

The Old Tannery, Kelston, Bath, BA1 9AN
Tel: 0117 932 7378 Fax: 0117 932 9652
Email: tony.smith@thermofluids.co.uk