![]() ![]() Subsequent development of the PCR (C1, 1984) has an extended range. Beginning in 1982, a modification of the missile (B1) with a lower trajectory altitude was introduced into service. Navy, funded work to reduce the altitude of the marching flight and change the software aimed at abandoning the slide before attacking the target. For three years, the British Navy, together with the U.S. RGMs of subsequent modifications do not perform such a maneuver, as it is not included in the flight program, and attack the target, dropping to ultra-shallow altitudes (2-5 m).īack in the late 70's to replace the basic model of the RGM-84A1 missiles began to arrive, characterized by a more advanced CNS with enhanced noise immunity. The missiles of the first modifications (RGM-84A and others) when approaching the target made a slide, captured the target and dive at an angle of about 30°. The homing system has a moving target indicator, which makes it unlikely that a cloud of passive interference will be detected.Īfter the start slide, the missile drops to an altitude of 15 m above sea level and then performs a march flight. When a group target is being attacked, it can simultaneously engage the homing heads of different rockets, which allows it to bypass some ships and attack others. When firing on the bearing, the CLO will engage at a set distance so as not to hit any other ship. ![]() The CLO has no selective properties, so the PCR hits the first target that it has captured. If no target is detected, a larger scan sector is used, so that the homing head works until the target is detected and captured. Several scanning modes, starting with the small sector, can be used to improve target acquisition efficiency. When shooting at maximum range, a large scan sector is used. In the first case, the missile's COS is triggered at the moment designated by the operator prior to launch, in the immediate vicinity of the target, which reduces the probability of detection of the ICR and the time for possible interference, in this case, to search for a target can be used small, medium or large sector scanning radar COS, the first is used when shooting at a group of targets at short range, but in this case, with increasing distance, the effectiveness of the COS decreases. The Harpoon PKR can be launched by the operator by bearing and range or only by bearing on the target (if the range is unknown). The trapezoidal wing has a large sweep at the front edge and its folding arms are attached to the fuel tank body. The Harpoon rocket is built according to the normal aerodynamic scheme, has a modular design and a unified hull, folding cross-shaped wing and four steering wheels. Air Force, two squadrons of B-52S bombers have been converted to anti-ship missile carriers. Navy was equipped with more than 210 Harpoon surface ships of the main classes (battleships, cruisers, destroyers, frigates), about 65% of nuclear submarines, more than 800 aircraft (R-ZS Orion, A-6 Intruder, A-7 Corsair, F/A-18 Hornet, S-3 Viking). A "M-84 aircraft were the first to receive Orion R-ZS patrol aircraft in 1978. The first Harpoon RGM-84 missiles were delivered to surface ships in 1976. For example, the following variants can be equally applied: RGM-84C1 or RGM-84 block 1C, RGM-84C block 1 and RGM 84C mod.1. Different foreign editions are characterized by their own ways of designating models and modifications of Harpoon missiles. The RGM-84A model is considered a basic model. The Harpoon anti-ship missile is produced in four main versions:Įach of them has several models and modifications. Design and flight testing of the new system continued until the summer of 1978. The development of the Harpoon anti-ship missile has been conducted by McDonald Douglas since the early 1970s. ![]()
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