Span : 40 ft 4 and 3/4 in
Length:56 ft
heght : 15 ft 3 and 1/2 in
wing area : 400 sq ft
Empty wgt : 23,050 lb
typical take-off wgt(fighter mission) : 36,710 lb
typical take-off wgt(attack mission) : 49,225 lb
max take-off wgt : 56,000 lb
wing loading : 92~123 lb/ft^2
power loading : 1.15~1.54 lb/lb
Max Spd : Mach 1.8 at 40,000 ft (more than)
initial climb rate : 60,000 ft/sec
service ceiling : 50,000 ft
typical combat radius (fighter mission) : 460 mile
typical combat radius (attack mission) : 660 mile
ferry range : 2,400 mile
Technical innovations:
(1) a quadruplex fly-by-wire flgight control system
(2) HOTAS (hands on throttle and stick)
(3) HUD
(4) two multi-function CRT
(5) BIT (built in test ) system
(6) an APU (auxiliary power unit)
engine : F404-GE-400 (16,000lb x 2)
radar : Hughes AN/APG-65 digital multi-mode set
Some comment on defects.
More serious was the range shortfall which, in spite of several airframe
modifications (including the filling the boundary layer slots in the LEX
and the elimination of the dog-tooth from the wing leading-edge to reduce
drag) and engine improvements to reduce specific fuel consumption, was never
fully corrected. Although the F/A-18 range remained less than specified after
all changes had been imcorporated, it was still greater in the fighter escort
role than that of the NcDonnell F-4J it repaced. In the strike role the
F/A-18 range was found to be 10 to 12 per cent shorter than that of the LTV
A-7E. Nevertheless, as in all other respects teh Hornet met or exceeded
specifications with air combat capability and weapon delivery accuracy being
particulary outstanding, the range deficiency did not prevent the Navy from
ordering the aircraft info full csale production without the need to approve
a proposed increase in internal fuel capacity through the installation of
tanks in a dorsalfairing aftof the cockpit.
(from McDonnell Douglas Aircraft, since 1920 V II, Rene J. Francillon)
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Georgia Institute of Technology *쪽~쪽~* Telephone : 404) 876 - 3542
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