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Specifications
of F-22 (F/A-22)
Following information
and some graphics from F22 Virtual Resource
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Wing
Area:
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840 sq
ft
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Engine
Thrust Class:
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35,000
lb
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Level Speed:
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921 mph
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Total Length:
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62.08
ft
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Wing
Span:
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44.5 ft
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Horizontal
Tail Span:
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29ft
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Tail Span:
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18'10"
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Total Height:
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16.67ft
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Track
Width:
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10.6ft
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Engines:
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Pratt
& Whitney F-119
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Max. Takeoff Weight:
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60,000 lb (27,216 kg)
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Max. External Stores:
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5,000 lb (2,270 kg)
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Weight Empty:
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31,670 lb (14,365 kg)
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Ceiling:
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50,000 ft (15,240 m)
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Crew:
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1
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G Limit:
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+9 G
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First Flight:
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September 7th
1997
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| Outer Surface Components |
| 39% Titanium |
| 24% Composite |
| 16% Aluminum |
01%
Thermo-plastic
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The F22 Raptor’s airframe is comprised mainly of four (4) large “chunks”,
or pieces that are produced by separate companies (see illustration below for
part and manufacturer).
 Click
Here to view a Technical Diagram click
here to view a three view diagram of the F-22
*The engines (PW-F119-100) are delivered and
manufactured by Pratt and Whitney
*The Aft Fuselage, main wing structures, power
generation units, fire protection system, and other various parts, mostly found
in the main fuselage. Boeing also manages many of the subsystems dealing with
fuel, electrical components, and engine operation.
*Lockheed Marietta produces and manages the
fins, flaps, ailerons, production of the forward fuselage, and joining the large
chunks of the aircraft together.
*Lockheed Ft. Worth manages and oversees the
production and assembly of the main fuselage, or the mid area of it. This job is
possibly the most difficult of all, because of the aircraft’s size, and the
fact that most of the wiring, tubing, and systems run through this portion of
the aircraft.
"The structural loads of the F-22 are mostly absorbed by 5 titanium bulkheads."
from F22Virtual Resource (No longer On-line).
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The F-22 has large area wings which allow it to perform well in high speeds. They
also double as a fuel tank. The leading edge flaps (located at the wings'
front edges) serve as a method of achieving high Angles of Attack (AOA) of over
60 degrees when traveling at lower speeds.
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The "fins" of the aircraft are divided into two types: the horizontal
(which control vertical movement) and the vertical (which control the horizontal
movement). The horizontal fins (located at the rear of the aircraft)
not only provide the plane with extra maneuverability etc... , but also act as a
heat shield for the exhaust of the engines, so the thermal trace of the F22 is
at a minimum. The vert. fins are angled in the similar fashion of the
F-22's body, to help reduce its radar signal. These also contain many
internal antennas inside the body of the fin itself, as a way to conceal them
and help maintain the stealth abilities of the aircraft.
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The weapon bays are all internally concealed (much like a stealth bomber).
On the low bottom left and right sides of the aircraft, underneath its wings,
are the bays were Aim 9's wind other missiles. The missiles are ejected
out by a special mechanism. See weapons . An
F/A-22C is being currently produced to hold larger weapons in the internal bays,
thus being a more bomber proned aircraft. Naval versions of the F-22 are
also coming.
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The landing gear is produced by Menasco. The landing gear mechanism is a retractable tricycle type, stressed for no-flare
landings of up to 3.05m/s downward speed. The measurement of the nose wheel tire
is 23.5 x 7.5-10 and the 2 main wheel tires measure 37 x 11.5-18.
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One of the F-22's distincitive features are the air intakes, which are located to the sides
of the main "cockpit area" ( the narrower part of the fighter's nose).
Once air has been channeled into the intakes, it winds up the internal tubes,
winding up and around the engine. Extra intakes are above these intakes,
which can be opened (they are closed to maintain stealth) when extra thrust is
needed.
Learn about the engines
Click On the Picture above to SEE the F22's inner structure
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