When was the tomahawk cruise missile invented




















Navy ships and submarines in subsequent days of the conflict. The new weapon proved instrumental in bringing a swift end to the war. Production of the missile ramped up after that, and hundreds of Tomahawks were used throughout the s.

On December 16, , missiles were fired at Iraqi targets during Operation Desert Fox, after Saddam Hussein refused to abide by United Nations-mandated inspections. More than Tomahawks were launched during the invasion of Iraq, and other successful deployments include Afghanistan, Somalia and Libya. Use of the missile has not been without controversy. On December 17, , 41 civilians—mostly women and children—were killed by missiles targeting an alleged Al-Qaeda training camp in Yemen.

Although U. But if you see something that doesn't look right, click here to contact us! Twice a week we compile our most fascinating features and deliver them straight to you. The weight of the missile is 1,kg. It has a life span of 30 years.

The missile can be reprogrammed in-flight to a new target. The two-way satellite communications are used to perform post-launch mission changes throughout the flight. The on-board camera provides imagery of the target to the commanders before the strike. The system enables the planning of new missions on board the launch vessel. TTWCS is also used to communicate with multiple missiles for reassigning the targets and redirecting the missiles in flight.

Its joint multi-effects warhead enables the commander to control the blast. All cruisers, destroyers, guided missile and attack submarines in the US Navy are equipped with a Tomahawk weapons system. US Navy launch platforms were modified to accommodate upgraded Tomahawk missile variants. Four Ohio class nuclear ballistic missile submarines were converted into cruise missile submarines for firing Tomahawk missiles. The Virginia class submarines and the Royal Navy Astute class submarines were also fitted with new vertical launch modules for Tomahawk missile.

The first batch of missiles was delivered in The "bulge" at the top front surface of the fuselage houses the 48 inch Ku-band wideband satellite communications antenna.

Data is transferred by Ku-band satellite communications, X-band line-of-sight links and both Satcom and line of sight links at UHF-band. The mission control ground station includes a shelter measuring 8 x 8 x 24 feet, housing the communications, command and control, mission planning and image processing computers with four workstations for the mission control team.

The control station has data up- and down-links to the Global Hawk vehicle directly and via the Ku satellite and the UHF satellite systems. The launch and recovery ground station is housed in an 8 x 8 x 10 foot shelter equipped with two workstations and the launch and recovery mission computers, along with it's own data up- and down-links.

The solar-powered Helios Prototype, ultra light flying wing. The solar-powered Helios Prototype is a slow-flying ultralight flying wing designed for long-duration, high-altitude Earth science or telecommunications relay missions in the stratosphere.

The craft has a wingspan of feet, longer than the wingspan of the Boeing jetliner, yet weighs in at only 1, pounds empty. The cruising speed of Helios ranges from 19 to 27 mph, with takeoff and landing equating to the average speed of a bicycle. It's constructed mostly of composite materials such as carbon fiber, graphite epoxy, Kevlar, styrofoam, and a thin, transparent plastic skin.

The all-wing aircraft is assembled in six sections, each about 41 feet long. An underwing pod is attached at each panel joint to carry the landing gear, the battery power system, flight control computers, and data instrumentation.

The five aerodynamically shaped pods are made mostly of the same materials as the wing itself, with the exception of the transparent wing covering.

Two wheels on each pod make up the fixed landing gear-rugged mountain bike wheels on the rear and smaller scooter wheels on the front.

The Helios Prototype is powered by 14 brushless direct-current electric motors mounted across the wing's entire span. The motors are rated at 2 hp. The propellers are made from advanced composite materials and a laminar-flow design for efficiency at high altitudes. An array of more than 65, bi-facial silicon solar cells mounted on the upper surface of Helios' wing is capable of producing a maximum output of about 35 kilowatts power at high noon on a summer day.

The cells convert about 19 percent of the solar energy they receive into electrical current. For long duration missions, the solar cells will be assisted by an on-board fuel-cell based energy storage system now in development.

Excess electrical energy generated by the solar arrays during the daytime will be diverted to the hydrogen-oxygen fuel cell energy storage system, which will release the electricity to power the Helios after dark. The only flight control surfaces used on the Helios Prototype are 72 trailing-edge elevators that provide pitch control. Spanning the entire wing, they are operated by tiny servomotors linked to the aircraft's fight control computer.

To turn the aircraft in flight, yaw control is applied by applying differential power on the motors--speeding up the motors on one outer wing panel while slowing down motors on the other outer panel.

The Helios Prototype is controlled remotely by a pilot on the ground, either from a mobile control van or a fixed ground station that is equipped with a full flight control station and consoles for systems monitoring. The craft has a differential Global Positioning Satellite GPS system to improve navigation, an extensive turbulence monitoring system payload to record structural loads on the aircraft both in the air and on the ground, and radiator plates to assist in cooling the avionics at high altitudes where there is little air to dissipate heat.

A flight termination system, required on remotely piloted aircraft flown in military restricted airspace, includes a parachute system deployed on command, plus a homing beacon to aid in the aircraft's location.

In case of loss of control or other contingency, the system is designed to bring the aircraft down within the restricted airspace area to avoid any potential damage or injuries to fixed assets or personnel on the ground. Production versions of the Helios are expected to fly missions lasting months at a time, becoming true "atmospheric satellites.

This propeller-driven radio controlled boat, built by Nikola Tesla in , is the original prototype of all modern-day uninhabited aerial vehicles and precision guided weapons — in fact, all remotely operated vehicles — air, land or sea.

Powered by lead-acid batteries and an electric drive motor, the vessel was designed to be maneuvered alongside a target using instructions received from a wireless remote-control transmitter. Once in position, a command would be sent to detonate an explosive charge contained within the boat's forward compartment. The weapon's guidance system incorporated a secure communications link between the pilot's controller and the surface-running torpedo in an effort to assure that control could be maintained even in the presence of electronic countermeasures.

Article List. A Brief History of Precision Guided Weapons "During wartime there was much research under way toward reducing the Tesla concept of the guided weapon in various laboratories.

The arrival on Mars of the Pathfinder robotic planetary exploration vehicle with it's diminutive rover Sojourner on July 4, was a landmark event in the history of wireless remote control. After nearly years of development, a technology with roots in an instrument of war had begun to fulfill what may be its greatest potential — helping mankind to establish a virtual presence on other worlds.



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