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| BASIC
CHARACTERISTICS |
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| Role |
Multi-role
fighter |
| Crew |
One
or two |
| First
Flight |
December
1976 |
| Entered
Service |
January
1979 |
| Manufacturer |
General
Dynamics |
|
and
Lockheed |
|
Cost (A/B) |
$14.6
million |
|
Cost (C/D) |
$18.8
million |
| Inventory |
1,268 |
| Speed |
1,500
mph |
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| DIMENSIONS |
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| Length |
49
feet, 5 in. |
| Wingspan |
32
feet, 8 in. |
| Height |
16
feet |
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| COOL
FACT |
In addition to the U.S. Air Force's
inventory of versatile Fighting Falcons,
about 1,300 of the planes are flown by
other nations, including (but not limited
to): Greece (135), China (150), Turkey
(200-plus), Norway (70); South Korea
(120)Singapore (71).
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Although the
F-16 is officially known as the "Fighting
Falcon," the more popular unofficial name for the
fighter is "Viper," apparently based on a
spacecraft that appeared in the hit TV show, Battlestar
Galatica."
Mission
The F-16 Fighting Falcon is a
compact, multi-role fighter aircraft. It is highly
maneuverable and has proven itself in air-to-air combat
and air-to-surface attack. It provides a relatively
low-cost, high-performance weapon system for the United
States and allied nations.
Features
In an air combat role, the F-16's maneuverability and
combat radius (distance it can fly to enter air combat,
stay, fight and return) exceed that of all potential
threat fighter aircraft. It can locate targets in all
weather conditions and detect low flying aircraft in
radar ground clutter. In an air-to-surface role, the
F-16 can fly more than 500 miles (860 kilometers),
deliver its weapons with superior accuracy, defend
itself against enemy aircraft, and return to its
starting point. An all-weather capability allows it to
accurately deliver ordnance during non-visual bombing
conditions.
In designing the F-16, advanced aerospace science and
proven reliable systems from other aircraft such as the
F-15 and F-111 were selected. These were combined to
simplify the airplane and reduce its size, purchase
price, maintenance costs and weight. The light weight
of the fuselage is achieved without reducing its
strength. With a full load of internal fuel, the F-16
can withstand up to nine G's -- nine times the force of
gravity -- which exceeds the capability of other
current fighter aircraft.
The cockpit and its bubble canopy give the pilot
unobstructed forward and upward vision, and greatly
improved vision over the side and to the rear. The
seat-back angle was expanded from the usual 13 degrees
to 30 degrees, increasing pilot comfort and gravity
force tolerance. The pilot has excellent flight control
of the F-16 through its "fly-by-wire" system.
Electrical wires relay commands, replacing the usual
cables and linkage controls. For easy and accurate
control of the aircraft during high G-force combat
maneuvers, a side stick controller is used instead of
the conventional center-mounted stick. Hand pressure on
the side stick controller sends electrical signals to
actuators of flight control surfaces such as ailerons
and rudder.
Avionics systems include a highly accurate inertial
navigation system in which a computer provides steering
information to the pilot. The plane has UHF and VHF
radios plus an instrument landing system. It also has a
warning system and modular countermeasure pods to be
used against airborne or surface electronic threats.
The fuselage has space for additional avionics systems.
Background
The F-16A, a single-seat model, first flew in December
1976. The first operational F-16A was delivered in
January 1979 to the 388th Tactical Fighter Wing at Hill
Air Force Base, Utah.
The F-16B, a two-seat model, has tandem cockpits that
are about the same size as the one in the A model. Its
bubble canopy extends to cover the second cockpit. To
make room for the second cockpit, the forward fuselage
fuel tank and avionics growth space were reduced.
During training, the forward cockpit is used by a
student pilot with an instructor pilot in the rear
cockpit.
All F-16s delivered since November 1981 have built-in
structural and wiring provisions and systems
architecture that permit expansion of the multi-role
flexibility to perform precision strike, night attack
and beyond-visual-range interception missions. This
improvement program led to the F-16C and F-16D
aircraft, which are the single- and two-place
counterparts to the F-16A/B, and incorporate the latest
cockpit control and display technology. All active
units and many Air National Guard and Air Force Reserve
units have converted to the F-16C/D.
The F-16 was built under an unusual agreement creating
a consortium between the United States and four NATO
countries: Belgium, Denmark, the Netherlands and
Norway. These countries jointly produced with the
United States an initial 348 F-16s for their air
forces. Final airframe assembly lines were located in
Belgium and the Netherlands. The consortium's F-16s are
assembled from components manufactured in all five
countries. Belgium also provides final assembly of the
F100 engine used in the European F-16s. Recently,
Portugal joined the consortium. The long-term benefits
of this program will be technology transfer among the
nations producing the F-16, and a common-use aircraft
for NATO nations. This program increases the supply and
availability of repair parts in Europe and improves the
F-16's combat readiness.
USAF F-16 multi-mission fighters were deployed to the
Persian Gulf in 1991 in support of Operation Desert
Storm, where more sorties were flown than with any
other aircraft. These fighters were used to attack
airfields, military production facilities, Scud
missiles sites and a variety of other targets.
Most recently in the Spring of 1999 during Operation
Allied Force, USAF F-16 multi-mission fighters flew a
variety of missions to include suppression of enemy air
defense, offensive counter air, defensive counter air,
close air support and forward air controller missions.
Mission results were outstanding as these fighters
destroyed radar sites, vehicles, tanks, MiGs and
buildings.
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