A380 spec's

That is one mother of an engine!

"Colin W Kingsbury" wrote in message
nk.net...
Worth noting that the 777 engines are actually quite a bit larger with
100,000+lb thrust capability:
http://www.geae.com/engines/commercial/ge90/index.html

Of course it mounts only two so total thrust is quite a bit less...
-cwk.

"Dave" wrote in message
...
Trents are Rolls Royce, it is the Trent 900 details are
Engine certification was achieved on schedule in October 2004 through
the
new European Aviation Safety Agency. Even though it will operate
initially
at a maximum take-off thrust of 70,000lb, the Trent 900 is cleared at an
80,000lb rating, allowing margin for future growth. It reached thrusts
in
excess of 90,000lb during early test bed running.

With a fan diameter of 116 inches, the Trent 900 is physically the
largest
engine ever built by Rolls-Royce. It is also the world's cleanest large
turbofan engine, measured by emissions per pound of thrust.

"Cockpit Colin" wrote in message
...
That is one mother of an engine!

"Colin W Kingsbury" wrote in message
nk.net...
Worth noting that the 777 engines are actually quite a bit larger with
100,000+lb thrust capability:
http://www.geae.com/engines/commercial/ge90/index.html


http://www.turbokart.com/about_ge90.htm

General Electric GE90-115B High Bypass Turbofan


a.. Type: Ultra High Bypass Ratio Dual Shaft Turbofan
b.. Bypass Ratio: 9:1
c.. Low Pressure Compressor: Single Stage fan, followed by 4 stage axial
booster
d.. High Pressure Compressor: 9 stage axial flow compressor
e.. Burner: Double annular through-flow combustor
f.. Turbine: Dual spool, 2 stage axial high pressure turbine, 6 stage
axial low pressure turbine
g.. Exhaust: Coaxial core and bypass jet exhaust
h.. Thrust Rating: 115,300 lbs. of thrust
i.. Weight: 18,260 lbs.
j.. Thrust/weight: 6.3:1
k.. Air mass flow: Approximately 3,000 lbs/sec
l.. Fan Pressure Ratio: 2:1
m.. Overall Pressure Ratio: 42:1
n.. Maximum Turbine Inlet Temperatu 2,700F+
o.. Specific Fuel Consumption: .25 lb/lbt/hr
p.. Fuel Burn at takeoff: 3,750 gallons/hr

"Cockpit Colin" wrote in message
...
That is one mother of an engine!

http://www.turbokart.com/about_ge90.htm

(See below)

the
new European Aviation Safety Agency. Even though it will operate
initially
at a maximum take-off thrust of 70,000lb, the Trent 900 is cleared at
an
80,000lb rating, allowing margin for future growth. It reached thrusts
in
excess of 90,000lb during early test bed running.

With a fan diameter of 116 inches, the Trent 900 is physically the
largest
engine ever built by Rolls-Royce. It is also the world's cleanest
large
turbofan engine, measured by emissions per pound of thrust.

General Electric GE90-115B High Bypass Turbofan
Type: Ultra High Bypass Ratio Dual Shaft Turbofan
* Bypass Ratio: 9:1
* Low Pressure Compressor: Single Stage fan, followed by 4 stage axial
booster
* High Pressure Compressor: 9 stage axial flow compressor
* Burner: Double annular through-flow combustor
* Turbine: Dual spool, 2 stage axial high pressure turbine, 6 stage axial
low pressure turbine
* Exhaust: Coaxial core and bypass jet exhaust
* Thrust Rating: 115,300 lbs. of thrust
* Weight: 18,260 lbs.
* Thrust/weight: 6.3:1
* Air mass flow: Approximately 3,000 lbs/sec
* Fan Pressure Ratio: 2:1
* Overall Pressure Ratio: 42:1
* Maximum Turbine Inlet Temperatu 2,700F+
* Specific Fuel Consumption: .25 lb/lbt/hr
* Fuel Burn at takeoff: 3,750 gallons/hr