Trent 900 | |
---|---|
Type | Turbofan |
National origin | United Kingdom |
Manufacturer | Rolls-Royce Holdings |
First run | 18 March 2003[1] |
Major applications | Airbus A380 |
Developed from | Trent 800 |
Developed into | Trent 1000 |
The Rolls-Royce Trent 900 is a high-bypass turbofan produced by Rolls-Royce plc to power the Airbus A380, competing with the Engine Alliance GP7000. Initially proposed for the Boeing 747-500/600X in July 1996,[2] this first application was later abandoned but it was offered for the A3XX,[3] launched as the A380 in December 2000.[4] It first ran on 18 March 2003,[1] made its maiden flight on 17 May 2004 on an A340 testbed,[5] and was certified by the EASA on 29 October 2004.[6] Producing up to 374 kN (84,000 lbf) of thrust, the Trent 900 has the three shaft architecture of the Rolls-Royce Trent family with a 2.95 m (116 in) fan.[6] It has a 8.5–8.7:1 bypass ratio and a 37–39:1 overall pressure ratio.[7]
Flight20may2003
was invoked but never defined (see the help page).Flight24july1996
was invoked but never defined (see the help page).Flight26feb1997
was invoked but never defined (see the help page).CNN19dec2000
was invoked but never defined (see the help page).Airbus17may2004
was invoked but never defined (see the help page).TCDS
was invoked but never defined (see the help page).Brochure
was invoked but never defined (see the help page).