User:Oosh/sandbox

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194 centimetres (76 in)

Specifications	Trent 900	GP7000
Type	Three-shaft high bypass ratio (8.7-8.5) turbofan engine	two-spool high-bypass turbofan engine
Length	4.55 m (179 in)	4.74 m (187 in)
Diameter	2.94 m (116 in) fan tip	2.95 m (116 in) fan tip
Weight	6,271 kg (13,825 lb)	6,712 kg (14,797 lb)
Compressor	Eight-stage IP compressor, six-stage HP compressor	hollow-titanium, 24 swept wide-chord hollow titanium fan blades, by-pass ratio of 8.7:1; five-stage low-pressure axial compressor; nine-stage high-pressure axial compressor
Combustors	Tiled combustor	low-emissions single annular combustor
Turbine	Single-stage HP turbine, single-stage IP turbine, five-stage LP turbine	two-stage high pressure turbine, boltless architecture, single crystal blades, split blade cooling and thermal barrier coatings, axial flow; six-stage low-pressure axial flow
Maximum power output		36,980 kgf, 363 kN, 81,500 lbf
Overall pressure ratio	37-39	43.9
Thrust-to-weight ratio	4.93-5.63 (assuming 14,190 lb (6,440 kg) weight of engine and certified to 70,000–80,000 lbf (310–360 kN)^* of thrust)	4.73 (assuming 17,230 lbf weight of engine and 81,500 lbf of thrust)

{{SVG Chart
| XAxisText    = Year
| YAxisText    = Index
| LegendType   = none  

| XMin         = 1990
| XMax         = 2015
| YMin         = 5
| YMax         = 20
| Graph1Values =       
     1990 6.16
     2000 10.72
     2005 11.15
     2012 17.29
}}

}