Aviation and War Machine

Exocet missiles started in development in 1967, originally as the ship-launched variant MM 38 which entered service in 1975. The air-launched version, AM 39, was developed later starting in 1974 and entering service with the French Navy in 1979. The missile is designed to attack large warships. A block 2 upgrade programme was carried out from the late 1980s until 1993, and introduced an improved digital active radar seeker and upgraded inertial navigation and control electronics.

The Exocet has four clipped delta wings at mid-body and four raked clipped-tip moving delta control fins at the rear. The missile is 4.7 m long, has a body diameter of 350 mm and a wingspan of 1.1 m. The missile weighs 670 kg and has a 165 kg HE shaped charge fragmentation warhead. Guidance in the mid-course phase is inertial, followed by an active radar terminal phase. There is also a radar altimeter to control the sea-skimming trajectory, at around 10.0 m until the terminal phase when, in calm sea conditions, the missile can descend to 3.0 m or so. The solid propellant motor gives Exocet a range of about 50 km, but when released from 10,000 m (32,800 ft) the range achieved was reported to be 70 km.

The F-35 is the result of the Defense Department’s Joint Strike Fighter (JSF) program, which sought to build a multirole fighter optimized for the air-to-ground role with secondary air-to-air capability. The JSF requirement was to meet the needs of the Air Force, Navy, Marine Corps and allies, with improved survivability, precision engagement capability, and reduced life cycle costs. By using many of the same technologies developed for the F-22, the F-35 has the opportunity to capitalize on commonality and modularity to maximize affordability.

The Lockheed Martin X-35 was chosen over the competing Boeing X-32 primarily because of Lockheed’s lift-fan STOVL design, which proved superior to the Boeing vectored-thrust approach. The lift fan, which is powered by the aircraft engine via a clutched driveshaft, was technically challenging but DoD concluded that Lockheed has the technology in hand. The lift fan has significant excess power which could be critical given the weight gain that all fighter aircraft experience.
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The F-2 is a close support fighter completed with Japan-U.S. cooperation and superior technology, as the model succeeding the F-1. MHI is the primary contractor. As for the wings, with the introduction of an integral structure, using composite material and maximizing the wingspan, there is better maneuvering capability. Also, with the use of various high tech materials and structural technology, we have succeeded in making the wings lighter.
In avionics, the newest technological domestic oriented equipment has been installed, such as integrated electronic warfare system, and an on-board computer.
Also, the Control Configured Vehicle (CCV) and Stealth characteristics are improved, using radio wave absorption materials, and equipping the engine with more thrust to increase capability in take-offs and landings.

October 1995 : The first flight of F-2 prototype aircraft.
March 1996 : The delivery of the first prototype aircraft.
MHI has manufactured 61 aircraft including prototype aircraft by March 2005.

The B-52H BUFF [Big Ugly Fat Fellow] is the primary nuclear roled bomber in the USAF inventory. It provides the only Air Launch Cruise Missile carriage in the USAF. The B-52H also provides theater CINCs with a long range strike capability. The bomber is capable of flying at high subsonic speeds at altitudes up to 50,000 feet (15,166.6 meters). It can carry nuclear or conventional ordnance with worldwide precision navigation capability.

The aircraft’s flexibility was evident during the Vietnam War and, again, in Operation Desert Storm. B-52s struck wide-area troop concentrations, fixed installations and bunkers, and decimated the morale of Iraq’s Republican Guard. The Gulf War involved the longest strike mission in the history of aerial warfare when B-52s took off from Barksdale Air Force Base, La., launched conventional air launched cruise missiles and returned to Barksdale — a 35-hour, non-stop combat mission.
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The Boeing (McDonnell Douglas) (formerly Hughes) AH-64A Apache is the Army’s primary attack helicopter. It is a quick-reacting, airborne weapon system that can fight close and deep to destroy, disrupt, or delay enemy forces. The Apache is designed to fight and survive during the day, night, and in adverse weather throughout the world. The principal mission of the Apache is the destruction of high-value targets with the HELLFIRE missile. It is also capable of employing a 30MM M230 chain gun and Hydra 70 (2.75 inch) rockets that are lethal against a wide variety of targets. The Apache has a full range of aircraft survivability equipment and has the ability to withstand hits from rounds up to 23MM in critical areas.

The AH-64 Apache is a twin-engine, four bladed, multi-mission attack helicopter designed as a highly stable aerial weapons-delivery platform. It is designed to fight and survive during the day, night, and in adverse weather throughout the world. With a tandem-seated crew consisting of the pilot, located in the rear cockpit position and the co-pilot gunner (CPG), located in the front position, the Apache is self-deployable, highly survivable and delivers a lethal array of battlefield armaments. The Apache features a Target Acquisition Designation Sight (TADS) and a Pilot Night Vision Sensor (PNVS) which enables the crew to navigate and conduct precision attacks in day, night and adverse weather conditions.
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The MK 15 Phalanx Close-In Weapons System (CIWS - pronounced “sea-whiz”) is a fast-reaction, rapid-fire 20-millimeter gun system that provides US Navy ships with a terminal defense against anti-ship missiles that have penetrated other fleet defenses. Designed to engage anti-ship cruise missiles and fixed-wing aircraft at short range, Phalanx automatically engages functions usually performed by separate, independent systems such as search, detection, threat evaluation, acquisition, track, firing, target destruction, kill assessment and cease fire. Phalanx underwent operational tests and evaluation onboard USS Bigelow in 1977, and exceeded maintenance and reliability specifications. Phalanx production started in 1978 with orders for 23 USN and 14 Foreign Military Sales (FMS) systems.

Phalanx is a point-defense, total-weapon system consisting of two 20mm gun mounts that provide a terminal defense against incoming air targets. CIWS, without assistance from other shipboard systems, will automatically engage incoming anti-ship missiles and high-speed, low-level aircraft that have penetrated the ship primary defense envelope. As a unitized system, CIWS automatically performs search, detecting, tracking, threat evaluation, firing, and kill assessments of targets while providing for manual override. Each gun mount houses a fire control assembly and a gun subsystem. The fire control assembly is composed of a search radar for surveillance and detection of hostile targets and a track radar for aiming the gun while tracking a target. The unique closed-loop fire control system that tracks both the incoming target and the stream of outgoing projectiles (by monitoring their incoming noise signature) gives CIWS the capability to correct its aim to hit fast-moving targets, including ASMs.
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USS Kitty Hawk is a conventionally powered aircraft carrier. Combined with the aircraft of Carrier Air Wing FIVE, it carries F-14, F/A-18, EA-6B, S-3 A/B, E-2CA aircraft and SH-60 helicopters, which give a multi-dimensional response to air, surface, and subsurface threats. KITTY HAWK underwent two overhauls in the Bremerton, Wash., Naval Shipyard in 1977 and 1982. The ship’s most significant maintenance period, however, was a Service Life Extension Program (SLEP) in the Philadelphia Naval Shipyard beginning from 1987 through 1991. That rigorous four-year overhaul added an estimated 20 years to the planned 30-year life of the ship.

Over a three month period in early 1998, nearly 4,000 shipyard workers, Sailors and contractors completed $65 million in repairs (over 500 major jobs) in the Complex Overhaul of the dry-docked Kitty Hawk. All four of the Hawk’s screws were repaired (number three was replaced), and all the line shaft bearings were replaced. Containments were built around the shafts to maintain temperature and humidity levels while complex fiberglass work was completed. For the rudders, large holes were cut through the decks, and the rudders and all associated systems were removed. Refurbished rudders were then removed from the decommissioned carrier USS Ranger while that ship was in the water, to be re-machined and installed on the Hawk.
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