At McDonnell Douglas, St. Louis, Missouri the new
F/A- 18E (Super Hornet)
was introduced.
Here are some details:
- a new F414- GE- 400 engine from General Electrics with 97.9 kN thrust
(+ 35% in comparison to Hornet C/D)
- 33% more inboard fuel than the Hornet C/D, resulting in a max. mission time
of 2h 15 min.
- length + 0.86m
- wing area + 25%, rudder area + 54%
- the Hughes APG-73 radar remains, but with better touch- on- screens
- avionics 90% identical with Hornet C/D
- mass (empty) increased to 13,864 kg
- new, even more robust gear, now enabling carrier landings without
jettison loadout
- chaff and flares amount increased to 120
- 30% fewer parts then Hornet C/D
- constructed totally with a solid- model- calculating- computer
system
- Sea tests are scheduled for January 1997
- Development costs US$ 4.88 million.
- About 27,000 employees in 3,200 companies participated in the project
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