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AGM-84 Harpoon
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| Primary
Function: |
Air-to-surface
anti-ship missile |
| Mission |
Maritime
ship attack |
| Targets |
Maritime
surface |
| Service |
Navy and
Air Force |
| Contractor: |
Boeing [ex
McDonnell Douglas] |
| Power Plant: |
Teledyne
Turbojet and solid propellant booster for surface and submarine launch |
|
sea-launch |
air-launch |
SLAM |
SLAM-ER |
| First capability |
1977 |
1979 |
|
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| Thrust: |
660 lbs |
| Length: |
15'
(4.55 m) |
12', 7"
(3.79 m) |
14',8"
(4.49 m) |
| Weight: |
1,470 lbs
(661.5 kg) |
1,145 lbs
(515.25 kg) |
1,385 lbs
(629.55 kg) |
| Diameter: |
13.5"
(34.29 cm) |
| Wingspan: |
3' (91.44
cm) |
| Range: |
Greater
than 60 NM |
150+ NM |
| Speed: |
855 km/h |
| Guidance
System: |
Sea-skimming
cruise with mid-course guidance monitored by radar altimeter, active seeker
radar terminal homing |
Inertial navigation system with GPS, infrared terminal guidance |
| Warheads: |
Penetration
high-explosive blast (488 lbs) |
| Explosive |
Destex |
| Fuze |
Contact |
| Quantity |
Navy: 5,983;
Air Force: 90 |
| Platforms |
A-6, F/A-18,S-3,P-3,B-52H, ships |

From the Federation of American Scientists Military Analysis Site:
"The Harpoon missile provides the Navy and the Air Force with a common missile for air, ship, and submarine launches.
The weapon system uses mid-course guidance with a radar seeker to attack surface ships. Its low-level, sea-skimming cruise
trajectory, active radar guidance and warhead design assure high survivability and effectiveness. The Harpoon missile and
its launch control equipment provide the warfighter capability to interdict ships at ranges well beyond those of other
aircraft.
The Harpoon missile was designed to sink warships in an open-ocean environment. Other weapons (such as the Standard
and Tomahawk missiles) can be used against ships, but Harpoon and Penguin are the only missiles used by the United States
military with anti-ship warfare as the primary mission. Once targeting information is obtained and sent to the Harpoon missile, it
is fired. Once fired, the missile flys to the target location, turns on its seeker, locates the target and strikes it without further
action from the firing platform. This allows the firing platform to engage other threats instead of concentrating on one at a time.
An appropriately configured HARPOON can be launched from an AERO-65 bomb rack, AERO-7/A bomb rack, MK 6 canister, MK 7 shock resistant
canister, MK 12 thickwall canister, MK 112 ASROC launcher, MK 8 and MK 116 TARTAR launcher, or submarine torpedo tube launcher.
Submarines fire a capsule containing the Harpoon from their torpedo tubes. When the capsule breaches the surface, the top is blown off
and the missile is launched. Aircraft launched Harpoons do not require a Booster. Depending upon launch conditions, the Harpoon
engine generally will not start until after the missile is dropped from the wing. This allows firing from higher altitudes and longer range flights.
The Guidance Section consists of an active radar seeker and radome, Missile Guidance Unit (MGU), radar altimeter and antennas, and power
converter. The MGU consists of a three-axis attitude reference assembly (ARA) and a digital computer/power supply (DC/PS). Prior to launch, the DC/PS
is initialized with data by the Command Launch System. After launch, the DC/PS uses the missile acceleration data from the ARA and altitude data from the
radar altimeter to maintain the missile on the programmed flight profile. After seeker target acquisition, the DC/PS uses seeker data to guide the missile to the target.
The Warhead Section consists of a target-penetrating, load-carrying steel structure containing 215 lbs of high explosive (DESTEX) and a safe-and-arm/contact
fuze assembly. The safe-and-arm/contact fuze assembly ensures the warhead will not explode until after the missile is launched. It is designed to explode the warhead
after impacting the target. The warhead section can be replaced by an exercise section which transmits missile performance data for collection and analysis.
The Sustainer Section consists of a fuel tank with JP-10 fuel, air inlet duct, and a jet engine. This provides the thrust to power the missile during sustained flight.
The Sustainer Section has four fixed fins which provide lift.
The Control Section consists of four electromechanical actuators which use signals from the Guidance Section to turn four fins which control missile motion.
The Booster Section consists of a solid fuel rocket and arming and firing device. Surface and submarine platforms use a booster to launch Harpoon and propel it to a speed at which
sustained flight can be achieved. The Booster Section separates from the missile before sustained flight begins.
The Harpoon missile was developed in the early 1970s. Numerous upgrades have kept it at the forefront of missile capabilities, including the Block 1 introduced in 1978,
and the Block 1B introduced in 1981. Today, the latest variant developed in 1982 called Block 1C is deployed by the United States military (Navy and Air Force) as well as US allies.
New developments are constantly being evaluated. Although originally planned to be in use until 2015, there is no plan to develop a replacement by the USN. There are continuing, extensive efforts
(testing and analysis) to ensure no detrimental effects of missile aging. With budget constraints projected into the future, Harpoon will be employed past 2015."
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