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Popeye Lite (Have Lite)
A Popeye Air-to-Surface Version for Lighter Aircraft
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Popeye-Lite, a new version of the Popeye, Air-to-Surface standoff missile is adapted for lighter aircraft such as the F-16.
Have Lite is an advanced air-to-ground precision guided missile. Have Lite is marketed by PGSUS, a joint venture of Lockheed Martin and Rafael. With Have Lite, fighter aircraft can attack and destroy high-value ground and sea targets from long range, including bunkers, power plants, missile sites, bridges, and ships. Multiple guidance modes and options provide lethal accuracy, allowing a building's doorway to become a legitimate target. Accurate and cost effective, the missile system has a very high proven hit probability. Have Lite, with its flexible mission planning and significant standoff range, minimizes fighter aircraft exposure. It can be programmed to fly various horizontal and vertical trajectories and employs autonomous midcourse guidance based on GPS-aided inertial navigation. The missile then homes in on the target using a high-performance IIR or TV seeker and delivers either penetration or blast fragmentation warheads with surgical precision.
Have Lite is a reduced size and weight version of the AGM-142. It gives fighter aircraft precision standoff capability. The missile features low and high altitude launch trajectories, and is highly survivable, especially in terminal phase. The trminal man-in-the-loop control provides for pinpoint accuracy. High reliability and availability are supported by high-performance IIR and TV seekers that are line replaceable units. The blast fragmentation or penetrating warheads are effective against hard or soft targets. |
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HAVE LITE is the reduced size and weight version of the AGM-142.
Brings precision standoff capability to single seat fighter aircraft.
Terminal man-in-the-loop control ensures pinpoint accuracy, minimizing collateral damage.
High impact velocity and programmable impact angle, combined with missile accuracy, provide the highest probability of kill for hard and soft targets.
GPS-aided mid-course inertial navigation feature reduces operator workload. It also incorporates operator-selected trajectory shaping, which requires minimal crew input until final aimpoint selection in terminal mode (90 percent silent to target).
Cost encompasses missile, data link pod, and integrated logistics support.
Same aircraft interfaces as AGM-142, specifically on the B-52, F-111,F-4, and F-15. Targeted aircraft include F-16, Mirage 2000, Kfir, and A-4.
Selected by multiple world-class air forces and totally supportable via the well-established USAF integrated logistics currently in place for the AGM-142, as well as the support facilities in Israel .
Operational and maintenance training capability mirrors that of the established and proven AGM-142 capability.
Integral solid rocket motor is expended well before impact, providing low noise and low IR signature. This feature, combined with trajectory shaping, significantly enhances survivability in the terminal phase.
U.S. production capabilities at Lockheed Martin Pike County Operations in Troy , Alabama takes advantage of AGM-142's production rate of 200 weapons per year.
The PGSUS joint venture team of Lockheed Martin and Rafael combines the strength of both companies to provide a high quality system.
Low aircraft integration cost and short integration schedule on fighter aircraft.
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Main Features
Standoff ranges - effective against high value land and maritime targets
Versatile and cost effective
Pinpoint accuracy, lethal efficiency
Day, night and adverse weather operation
Battle Damage Assessment (BDA) capability
Variety of trajectories to meet weather and threat conditions.
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In 26.11.2002 the first flight of the Have-Lite (a lightweight version of the Popeye standoff precision attack missile) was successfully conducted by Lockheed Martin and RAFAEL, as a U.S. Air Force F-16 pilot launched the missile and controlled the weapon to a high precision hit, while flying the aircraft. |
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Lockheed Martin successfully conducted the first flight test of the lightweight version of the RAFAEL Popeye missile designated Have Lite, demonstrating the ability of a U.S. Air Force F-16 pilot to launch and control the weapon while also flying the aircraft. In the test, conducted at the Utah Test Range in Ogden, Utah, the missile struck a stationary target, proving it could follow a planned mission route.
"We're extremely pleased with the results of this test," said Randy Bigum, vice president of Strike Weapons at Lockheed Martin Missiles and Fire Control. "Have Lite will enable our international customers to strike high-value ground and sea targets from long range. Since Have Lite is designed to work from fighter aircraft, it opens up a heavy strike capability without the need for heavy aircraft."
In this test, the missile was launched from a single seat U.S. Air Force F-16, flying 0.7 mach at an altitude of 8,700 feet. After weapon release, the missile flew a straight path using Global Positioning System (GPS) guidance to locate the target area.
The aircraft then turned away from the target while maintaining data link with the missile. When in range, the F-16 pilot maneuvered the missile into the target using man-in-the-loop controls with the missile's terminal guidance TV seeker. As planned, the missile struck the target with an inert warhead. |
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In May 1997 Israel and Turkey agreed to jointly produce the Popeye 2 air-to-ground missile in a deal initially worth about $100 million dollars. The new deal involved a consortium to be established between two Turkish firms and Rafael to jointly produce the Popeye 2, a smaller missile with more advanced technology. The Popeye 2, also known as the Have Lite, is designed for deployment on fighter aircraft and has a range of 150 kilometers. The Popeye 2 missiles were expected to be delivered beginning in 2000. The overall Popeye 1 and Popeye 2 missiles program with Turkey was valued at some $500 million.
In December 1999 press reports suggested the possibility of the sale of Popeye 2 missiles to India. US officials told Israel that they were concerned about sales of arms to India because of tensions in the region. |
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Specifications |
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Missile
Guidance
Midcourse
Terminal
Propulsion
Length
Diameter
Horizontal Span (max)
Vertical Span
Overall Weight
Warhead Section
(Penetrator or Blast Fragmentation) |
GPS ai ded inertial
IIR or TV with man-in-the-loop
Solid Fuel
424 cm (167 in)
53cm (21 in)
152 cm (60 in)
107 cm (41 in)
1125 kg (2500 lb)
454 kg (1000 lb)
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Data Link Pod
Weight
Length
Diameter
Pointing Antenna |
393 kg (865 lb)
353 cm (139 in)
53 cm (21 in)
Narrow Beam
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Characteristic |
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Characteristics
Weight
Propulsion
Seeker
Weapon Control
Warhead
Aircraft Compatibility |
1125 kg
Solid Fuel Rocket
IIR, TV
Video and command data link
341 kg general purpose or 364 kg penetrator (approximate equivalent penetration capability to BLU-109/B)
B-52, F-111, F-15, F-4,
F-16, Mirage 2000, Kfir and A-4. |
Capability
Standoff Range
Accuracy
Aimpoint Selection
Day/Night Operation
Trajectory Control
Battle Damage Information
Target kill hard/soft |
Greater than 50 nautical miles
Precision less than 3 meters
Yes
Yes, IIR day or night, TV day
Yes – programmable vertical or horizontal flight profiles and impact angles
Yes – real-time in-flight playback impact up to impact
Yes – against horizontal and vertical targets at weapons max standoff range
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Employment
Delivery Tactics
Aircraft Exposure
Degraded weather conditions |
Flexible – several vertical and horizontal trajectory options
Has the longest standoff PGW system currently operational, minimizing aircraft attrition
Yes –demonstrated capability
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Logistics and Training |
Exists world-wide |
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