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The AGM-158B JASSM-ER was estimated to have a maximum range of 500 nmi (930 km). [3] [17] However, LRASM's range is shorter than the JASSM-ER it is based upon, due to the extra space for the navigation/sensor/passive radar needs. Lockheed Martin has claimed the missile's range is greater than 200 nmi (370 km). [18]
The original version of the missile, called Block 0, is based on the AIM-9 Sidewinder air-to-air missile, whose rocket motor, fuze, and warhead are used. Block 0 missiles were designed to initially home in on radiation emitted from a target (such as the active radar of an incoming anti-ship missile ), switching to an infrared seeker derived ...
The AIM-174B is a long-range air-to-air missile (AAM) developed by U.S. defense contractor Raytheon and used by the United States Navy (USN). The AIM-174B is a derivative of the RIM-174B Standard Extended Range Active Missile (ERAM, Standard Missile-6, or SM-6) surface-to-air missile, a member of the extended Standard Missile family, with the USN describing the AIM-174B as the "Air-Launched ...
After having spent €5 billion ($6.7 billion) developing the missile, the French government placed a €3 billion ($3.9 billion) order with EADS SPACE Transportation for the M51 in December 2004. The contract covered serial production of the M51 for 10 years, with the company to be responsible for sustained readiness support throughout the ...
The blunt nose contains the active sonar seeker with the 75-pound (34 kg) high-explosive warhead immediately behind it. The second section contains the guidance and gyroscopes. The third contains the 24 kilowatt seawater battery which uses silver chloride and magnesium electrodes with seawater acting as the electrolyte.
The GBU-44/B Viper Strike glide bomb was a GPS-aided laser-guided variant of the Northrop Grumman Brilliant Anti-Tank (BAT) munition which originally had a combination acoustic and infrared homing seeker.
It then used the first stage of this system to develop the 700 km range single-stage Agni-1, which was first tested in January 2002 Weighing 12 tonne with a length of 15 metres, Agni-1 has a range of 700–900 km [7] and is capable of carrying a conventional payload of 1,000 kg (2,200 lb) or a nuclear warhead [1] at a speed of 2.5 km/s. [3]
The tandem warhead is fitted with two shaped charges: a precursor warhead to detonate any explosive reactive armor and a primary warhead to penetrate base armor. In what is known as a " soft launch arrangement," the missile is ejected from the launcher to a safe distance from the operator before the main rocket motors ignite. [ 17 ]
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