Description: The F118 was developed utilizing the same core design of the F101 engine.
The F118 has different fan and afterburner packages to tailor engine performance compared with the F101.
The F118-GE-101 has been designed to re-engine the U-2R high-altitude reconnaissance aircraft, U-2R with -101 engines are designated U-2S.
The -101 engine increases U-2's ceiling, range, safety and ease of flight.
Fan Diameter: 1,190 millimeter
Length: 2.79 meter
Dry Weight: 1,429 kilogram (3,150 pound)
Thrust: 17,000 pound (7,711 kilogram)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
There is 1 news
on 22 Jan 2008
Operators & Related Equipment
F118-GE-101 Links & Resources
Copyright © 2003-2015 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.