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Saturday, 27 July 2013

A-10/OA-10 Thunderbolt II

A-10/OA-10 Thunderbolt II

Mission

The A-10 and OA-10 Thunderbolt IIs are the first Air Force aircraft specially designed for close air support of ground forces. They are simple, effective and survivable twin-engine jet aircraft that can be used against all ground targets, including tanks and other armored vehicles.

Features

The A-10/OA-10 have excellent maneuverability at low air speeds and altitude, and are highly accurate weapons-delivery platforms. They can loiter near battle areas for extended periods of time and operate under 1,000-foot ceilings (303.3 meters) with 1.5-mile (2.4 kilometers) visibility. Their wide combat radius and short takeoff and landing capability permit operations in and out of locations near front lines. Using night vision goggles, A-10/ OA-10 pilots can conduct their missions during darkness.
Thunderbolt IIs have Night Vision Imaging Systems (NVIS), compatible single-seat cockpits forward of their wings and a large bubble canopy which provides pilots all-around vision. The pilots are encircled by titanium armor that also protects parts of the flight-control system. The redundant primary structural sections allow the aircraft to enjoy better survivability during close air support than did previous aircraft. The aircraft can survive direct hits from armor-piercing and high-explosive projectiles up to 23mm. Their self-sealing fuel cells are protected by internal and external foam. Their redundant hydraulic flight-control systems are backed up by manual systems. This permits pilots to fly and land when hydraulic power is lost.
The Thunderbolt II can be serviced and operated from bases with limited facilities near battle areas. Many of the aircraft's parts are interchangeable left and right, including the engines, main landing gear and vertical stabilizers.
Avionics equipment includes communications, inertial navigation systems, fire control and weapons delivery systems, target penetration aids and night vision goggles. Their weapons delivery systems include head-up displays that indicate airspeed, altitude and dive angle on the windscreen, a low altitude safety and targeting enhancement system (LASTE) which provides constantly computing impact point freefall ordnance delivery; and Pave Penny laser-tracking pods under the fuselage. The aircraft also have armament control panels, and infrared and electronic countermeasures to handle surface-to-air-missile threats.
The Thunderbolt II's 30mm GAU-8/A Gatling gun can fire 3,900 rounds a minute and can defeat an array of ground targets to include tanks. Some of their other equipment includes an inertial navigation system, electronic countermeasures, target penetration aids, self-protection systems, and AGM-65 Maverick and AIM-9 Sidewinder missiles.

Background

The first production A-10A was delivered to Davis-Monthan Air Force Base, Ariz., in October 1975. It was designed specially for the close air support mission and had the ability to combine large military loads, long loiter and wide combat radius, which proved to be vital assets to America and its allies during Operation Desert Storm. In the Gulf War, A-10s, with a mission capable rate of 95.7 percent, flew 8,100 sorties and launched 90 percent of the AGM-65 Maverick missiles.

General Characteristics

Primary Function: A-10 -- close air support, OA-10 - airborne forward air control
Contractor: Fairchild Republic Co.
Power Plant: Two General Electric TF34-GE-100 turbofans
Thrust: 9,065 pounds each engine
Length: 53 feet, 4 inches (16.16 meters)
Height: 14 feet, 8 inches (4.42 meters)
Wingspan: 57 feet, 6 inches (17.42 meters)
Speed: 420 miles per hour (Mach 0.56)
Ceiling: 45,000 feet (13,636 meters)
Maximum Takeoff Weight: 51,000 pounds (22,950 kilograms)
Range: 800 miles (695 nautical miles)
Armament: One 30 mm GAU-8/A seven-barrel Gatling gun; up to 16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wing and three under-fuselage pylon stations, including 500 pounds (225 kilograms) of retarded bombs, 2,000 pounds (900 kilograms) of general-purpose bombs, incendiary and Rockeye II cluster bombs, combined effects munitions, Maverick missiles and laser-guided/electro-optically guided bombs; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; 2.75-inch (6.99 centimeters) rockets; illumination flares and AIM-9 Sidewinder missiles.
Crew: One
Date Deployed: March 1976
Unit Cost: $8.8 million
Inventory: Active force, A-10, 72 and OA-10, 72; Reserve, A-10, 24 and OA-10, 12; ANG, A-10, 64 and OA-10, 30

Sunday, 21 July 2013

Weapons

Weapons
Boasting a lethal number of mini-guns, cannons and howitzers, the AC-130 Gunship has earned a reputation as one of the deadliest combat weapons on the planet.
A Transport Plane with Firepower The AC-130 Gunship -- Fire In The Sky
The AC-130 is a modified version of Lockheed Martin Corp.’s C-130 transport plane. The aircraft gets its intimidating array of weapons from The Boeing Company, which is responsible for converting the transport plane into a gunship. The AC-130 is used in combat missions to provide support to other aircraft and soldiers fighting on the ground.
The U.S. Air Force is the only user of the AC-130 Gunship. The aircraft comes in two variants known as "Sceptre" and "Spooky." With a flight crew of 13 Air Force personnel and weapons ranging from 25 millimeter Gatling guns to 105 millimeter howitzers, the AC-130 has a reputation for delivering punishing assaults in combat zones.
In addition to its firepower, the AC-130 gunship has proved popular with the U.S. Air Force because of its ability to operate in adverse weather conditions and for long periods at night. Equipped with high-tech sensors, scanners and radar, the aircraft is able to distinguish between allied forces and enemy troops from great distances. This makes the AC-130’s accuracy one of the best among conventional military aircraft.
A Legacy that Began in Vietnam
The current model of the AC-130 Gunship has been used to fight enemy combatants in Iraq, Afghanistan and Somalia. However, the aircraft got its start in the Vietnam War. The U.S. Air Force first developed the gunship to provide support to fighter jets and ground soldiers conducting missions in Laos and South Vietnam.
From its inception in 1967, the AC-130 Gunship proved extremely capable and popular – destroying, by some estimates, more than 10,000 enemy ground vehicles and thousands of enemy aircraft. Within a year of coming into service, there were enough AC-130 Gunships in Vietnam to form a squadron. The first AC-130 squadron was called the 16th Special Operations Squadron and went by the acronym "S.O.S."
More recently, the AC-130 Gunship has been used to provide firepower and support during the invasion of Panama in 1989, the first Gulf War in 1991, and present day operations in Iraq, Afghanistan and parts of Africa. The AC-130 Gunship has been used recently to remove al-Qaeda militants from difficult mountain terrain.
Upgrading to More Firepower
The AC-130 Gunship has been criticized for being too heavily armed and providing an overwhelming display of force. However, the Air Force Special Operations Command has moved in recent years to add more firepower to the aircraft.
In 2007, the U.S. Air Force announced that it wants to upgrade and add to the armaments on the AC-130 Gunship. There are plans to possibly replace the aircraft’s howitzers with 120 millimeter mortars and Hellfire missiles. There have also been discussions about adding Viper Strike Glide Bombs and an Advanced Precision Kill Weapon System to the aircraft. Taken together, these additions would make the AC-130 Gunship an even more formidable piece of weaponry.

The U.S. Air Force has stated that it will begin a process in 2011 to purchase 16 new gunships. The new gunships will be Lockheed Martin C-130J transport planes modified to include what the military has called a "precision strike package." The U.S. Air Force has said that it will spend $1.6 billion to acquire the additional gunships between 2011 and 2015. With the new additions, the U.S. Air Forces’ fleet of gunships is expected to number 33 aircraft.
F-22
F-22
Nicknamed the Raptor, the F-22 is the most advanced and expensive fighter fielded by any air force in the world.
It is also the U.S. Air Force’s newest fighter aircraft. It entered service in December 2005 after 15 years of testing and development. During this process, the airframe was significantly redesigned and production numbers cut, as prototypes of the Raptor failed to meet Air Force expectations.
The jet performs both air-to-air and air-to-ground missions.
The Raptor is state-of-the-art. It boasts the most capable radar fitted in an aircraft of its size: 62 feet long, with a wingspan of 44.5 feet. It can fly up to 1,600 miles per hour (Mach 2.42).
It’s also difficult to detect, with greater stealth capabilities than other aircraft. Technologies that make a plane “low-observable,” in the vocabulary of the Air Force, muffle noise and radio transmissions and lower the heat of its infrared picture. The angles of the wings and the tail of the Raptor are aligned in way that makes it harder to spot; the slope of the main body and the fact that its weapons can be carried inside also help make it less visible.
The F-22 also has more thrust and a sleeker design than other fighters, so it can hit the speed of sound without using afterburner, which slows and limits the range of aircraft that need to use it.
The jet can outmaneuver other aircraft because of its “sophisticated aerodesign, advanced flight controls, thrust vectoring, and high thrust-to-weight ratio,” according to the Air Force.
The maiden flight of the original test model was made in September 1990, and the Air Force has since ordered around 400 of the fighter jets.

F-15

The Eagle

Nicknamed the Eagle, the F-15 has a Doppler radar system that can track targets both above and below and a windscreen that doubles as a display panel so a pilot needn’t look down to receive critical tracking and targeting information.
The Eagle is a two-seat tactical fighter, powered by two turbofan engines. It is supersonic, flying at a rate of 1,875 miles per hour (Mach 2.5) at an altitude of 65,000 feet. It is more than 63 feet long with a wingspan of nearly 43 feet.
Two design factors enable the F-15 to accelerate more rapidly and nimbly than other aircraft. In addition to a high thrust-to-weight ratio, it has low wing loading, which enables it to make tight turns without slowing down. The F-15 can be armed with a variety of air-to-air weapons, and it can be refueled mid-flight.
The Air Force fact sheet on the F-15 says its avionics system “includes a head-up display, advanced radar, inertial navigation system, flight instruments, ultra-high frequency communications, tactical navigation system and instrument landing system. It also has an internally mounted, tactical electronic-warfare system, ‘identification friend or foe’ system, electronic countermeasures set and a central digital computer.” The Air Force has more than 500 of the combat aircraft.
The first F-15 flight, involving the original model single-seater, took place in July 1972.
The most recent model, the F-15E, is called the Strike Eagle and sometimes the Beagle. It can perform air-to-air and air-to-ground missions. It can fly low, which enables the weapons officer to address ground targets while also identifying and striking at air threats.
The F-15E made its combat debut over Iraq in Operation Desert Storm in 1991, tracking down SCUD missile launchers and artillery sites in nighttime sweeps. The aircraft also have been deployed to monitor the no-fly zone in southern Iraq and have been used in Bosnia, Afghanistan and the current conflict in Iraq.

Joint STARS Mission

High over Iraq, an E-8C Joint STARS aircraft surveys hundreds of miles of the country at a time, looking for insurgent activity, controlling those situations and taking action if needed.
The aircraft's crew ultimately keeps ground troops safer by communicating with convoys and directing air power to quell the enemy.
The Joint Surveillance and Target Attack Radar System mission has two parts. The first is to radio relay with convoys throughout Iraq. Through radio and a text-messaging system, convoys can contact Joint STARS for help.
Air National Guard Maj. Thomas Grabowski, senior director on the aircraft, deployed from Robins Air Force Base, Ga. He said the Joint STARS is the 911 call for convoys on the ground.
“So if one of these convoys gets in trouble -- they break down, they have troops in contact, small-arms fire or any type of a problem -- they call us,” Major Grabowski said. “We’re like the ‘On-Star’ for the ground commander.”
The second part of the mission is to deter insurgent activity on Iraq’s borders. Junior enlisted Airmen are in charge of the multimillion dollar radar attached to the bottom of the aircraft that zeros in on the enemy 100 to 200 miles away. Major Grabowski said the advanced system allows them to see the enemy without the enemy seeing them.
“Think about where you live at home and then think of a place 125 miles from that location. If you were to move out of your driveway and we were orbiting 125 miles away, we would see you move. So it’s that advanced,” the major said.
Joint STARS is truly a joint mission aircraft with Army, Air Force and Marine aircrew members. Air National Guard Airmen add total force flavor as well. Army Maj. Clifton Hughes, deputy mission crew commander, is also deployed from Robins. He said he works closely with Major Grabowski and the other Air Force folks on every Joint STARS mission.
“While the Army and Marines are keeping in close contact with convoy commanders, I can then coordinate with the Joint STARS Air Force assets on the aircraft to direct air support either as a show of force or to take out the enemy,” he said.
A typical mission can last from 10 to 20 hours in flight after refueling in the air. The aircraft brings such a capability to the fight that many convoys won’t go out on the road unless Joint STARS is airborne.
A total of $300 million worth of technology goes into this aircraft. What comes out is full-spectrum dominance and reconnaissance capability that ensures peace of mind to U.S. forces on the ground that someone is always watching their backs.

Robots of the Air Force

EGLIN AIR FORCE BASE, FL -- Pentagon officials and guests were treated to a demonstration of the remote detection challenge and response, or REDCAR, initiative June 23.
REDCAR uses unmanned robotic platforms to provide perimeter defense of Air Force bases and forward-deployed units.
“With REDCAR we can integrate a family of robots to secure an airfield and take the warfighter out of the initial line of attack,” said Capt. Adolfo Meana, chief of the Force Protection Battlelab’s concepts division at Lackland Air Force Base, Texas. “The forces are kept in reserve to tactically move against the enemy. We put the robots in danger first and save troops’ lives.”
Operators control the robots from a safe location, such as an armored vehicle, using a laptop computer. They are able to manage many robots at the same time and can even pass control between operators.
Battlelab and Air Force Research Laboratory workers developed the REDCAR family of robotic vehicles.
The proof of concept demonstration included three robotic vehicles. The first was Scout, a rough-terrain vehicle that travels at up to 20 mph using preprogrammed navigation and obstacle avoidance. The Scout controller can issue voice commands to people it encounters through its Phraselator.
“Scout has up to 57 pre-programmed languages and can issue such police phrases as ‘halt, drop your weapon,’ etcetera” Captain Meana said. “However, we hope controllers will be able to speak directly through the Phraselator in the future.”
The Mobile Detection and Response System is another robot. It provides area surveillance and detects threats, with Scout acting as an interceptor.
The third robotic vehicle, called Matilda, is a small-scale, tracked vehicle that can be carried on MDARS. Matilda provides reconnaissance in limited-access areas, including under vehicles, aircraft, and inside buildings.
“The challenge is getting all the robots to work together,” said Walt Waltz, the laboratory’s chief of robotics research at Tyndall AFB, Fla. “Communication between the robots is key.”
During the demonstrations here, all three robots demonstrated scenarios. In one scenario, Scout detected and confronted an intruder trying to gain unauthorized access to the flightline. After the intruder refused to obey commands issued by the controller, he was disabled with a pepper spray system mounted on Scout. Another scenario featured Scout and MDARS detecting and defending against a guerrilla force trying to attack the base. During the attack, Scout used a precision-targeted M-16A2 rifle controlled from a remote location. Toward the end of the attack, Matilda was released from MDARS to search for attackers hiding in culverts.
Staff Sgt. Miguel Jimenez, assigned to the 325th Security Forces Squadron at nearby Hurlburt Field, is excited about the new technology.
“It will help out a lot having the robotic platforms alerting us to possible hostilities. It will provide an immediate visual assessment before we get there and we can use the weapon if necessary,” Sergeant Jimenez said.

Tuesday, 25 June 2013

F-15 Eagle

F-15 Eagle



Design

The McDonnell Douglas F-15 Eagle emerged from the complex and extensive set of requirements established by the USAF. Configuration of the twin-engine aircraft is characterized by a high-mounted wing, twin vertical tails mounted at the rear of the short fuselage, and large, horizontal-ramp variable- geometry external-compression inlets located on the sides of the fuselage ahead of the wing. The horizontal-tall surfaces are mounted in the low position on fuselage extensions on either side of the exhaust nozzles.
Propulsion of the F-15 is supplied by two Pratt & Whitney F100-PW-100 afterburning turbofan engines of 23,904/14,780 pounds thrust each. Developed especially for the F-15, these high-pressure-ratio engines are reported to have much improved efficiency over earlier engines for fighter aircraft.
The wing planform of the F-15 suggests a modified cropped delta shape with a leading-edge sweepback angle of 45°. Ailerons and a simple high-lift flap are located on the trailing edge. No leading-edge maneuvering flaps are utilized, although such flaps were extensively analyzed in the design of the wing. This complication was avoided, however, by the combination of low wing loading and fixed leading-edge camber that varies with spanwise position along the wing. Airfoil thickness ratios vary from 6 percent at the root to 3 percent at the tip.
To succeed in the air-to-air role, a plane needs the right airframe in combination with strong powerplant and avionics. The plane's designers understood this and stretched technology to the limits. It was determined that a very low wing loading combined with heavy thrust from the engines would be required. US fighter aircraft of the period were going faster (Mach 2 plus), but were heavy and lacked maneuverability compared to their Soviet counterparts. When combined with a capable airframe, better maneuverability can be achieved by maximizing thrust, thereby maximizing energy. The Pratt & Whitney F100 Turbofan engine provides the needed thrust. Each engine is capable of producing 15,000 pounds of thrust at maximum power, and 25,000 pounds of thrust in afterburner. This gives the Eagle a total of 50,000 pounds of thrust. In other words, a nominally loaded F-15 Eagle of 48,000 pounds has a thrust-to-weight ratio of 1.04 pounds of thrust to each pound of aircraft weight. Thrust of this caliber allows an F-15 to accelerate while going straight up! A specially modified F-15A Eagle known as the "Streak Eagle" was able to outclimb a Saturn V Moon Rocket to almost 60,000 feet. This same aircraft flew to 98,430 feet (30,000 meters) in 207.80 seconds (less than 3 minutes and 30 seconds).
The wing loading of the F-15 is significantly lower and the thrust loading much greater than corresponding values for earlier fighter aircraft. At the lower weights to be expected during combat, wing loadings as low as 55 pounds per square foot and static thrust-to-weight-ratios of as much as 1.35 might be expected. (As the Mach number increases at a given altitude, the thrust of the afterburning turbofan also increases. For example, the thrust of the F-15 engine at sea level and Mach 0.9 is nearly twice the sea-level static value.) The values of these parameters represent a significant departure from previous fighter design philosophy and resulted from the energy-maneuverability concepts employed in specifying the aircraft.
To understand the design of the F-15 and its unique capabilities, some insight into the meaning of maneuverability and its relation to several aircraft design parameters is necessary. The maneuvering capability of an aircraft has many facets, but one of the most important of these is its turning capability. In a combat situation between two opposing fighters flying at the same speed, the aircraft capable of turning with the shortest radius of turn without losing altitude usually has the advantage. This assumes equality of many other factors such as aircraft stability and control characteristics, armament, and, of course, pilot skill.
In steady, turning flight the lift developed by the wing must balance not only the weight of the aircraft but the centrifugal force generated by the turn. (The term "balance" is used here in a vector sense; that is, the lift vector must equal the sum of the weight and centrifugal force vectors.) The load factor is defined as the ratio of the lift in the turn to the weight of the aircraft and is usually expressed in g units, where g is the acceleration due to gravity. Thus, a 2-g turn is one in which the wing must develop a lift force twice the weight of the aircraft. The value of the load factor is uniquely defined by the aircraft angle of bank. For example, 2-g and 5-g turns require bank angles of 60 and 78.5 respectively. Finally, for a given bank angle and thus load factor, the turning radius varies as the square of the speed; for example, doubling the speed of the aircraft increases the turning radius by a factor of 4. It would then appear that two different aircraft flying at the same speed would have the same turning radius; however, this conclusion is not necessarily correct. The maximum load factor and associated turning radius may be limited by wing stalling. For a given speed and altitude, stalling occurs as a function of the wing maximum lift coefficient and the wing loading in straight and level flight. Clearly then, the turning capability of different aircraft types may vary widely.
Two other important aircraft physical parameters may also limit turning performance. First, at a given speed and altitude, the aircraft drag increases rapidly with lift coefficient; as a consequence, the available thrust may not be sufficient to balance the drag at some load factors that the wing can sustain. In this case the aircraft loses altitude in the turn, an undesirable situation in combat. As for maximum lift coefficient, the drag rise with increasing lift depends upon the wing design and Mach number, as well as upon the added drag required to trim the aircraft at high lift coefficients. Finally, the turning performance may be limited by the control power available in the horizontal tail for trimming the aircraft at the high maneuvering lift coefficients.
These ideas are embodied in a technique for describing and specifying fighter aircraft maneuverability. Known by the term "energy maneuverability," the technique involves the specification of desired aircraft climb and/or acceleration capability for various combinations of speed, altitude, and turning load factor. The quantity specified for each of these combinations is labeled "specific excess power" Ps and is simply the excess power available per unit aircraft weight as compared with the power required to maintain constant altitude in the turn.
The lightly loaded airframe is combined with an equally impressive flight control system. A hydraulically actuated, mechanically controlled flight control system is augmented by an electronic system known as the Control Augmentation System (CAS). This system takes the stick inputs from the pilot and deflects the flight controls in the proper direction at the proper rate for optimal aircraft handling. This system allows the pilot to fly the aircraft to the limits of its capabilities without losing control of the aircraft. The CAS can also actuate the flight controls via pilot input if the hydro-mechanical system is damaged.
In order to win air-to-air battles, the pilot must be able to see, shoot, evade, and destroy the adversary first. The Eagle has an impressive array of weapons and avionics which allow it to get the advantage. The APG-63 and 70 radars allow crews to see targets that are as far away as 100 miles. These "Eyes" are able to ferret out the targets even if the targets are flying at high speeds at low altitudes. A Tactical Electronic Warfare System (TEWS) lets the aircrew know if any threat is present. The Heads-up-Display (HUD), and the Hands on Throttle and Stick (HOTAS), allow the Pilot to select, track and shoot the adversary without having to look back into the cockpit.
The F-15's versatile pulse-Doppler radar system can look up at high-flying targets and down at low-flying targets without being confused by ground clutter. It can detect and track aircraft and small high-speed targets at distances beyond visual range down to close range, and at altitudes down to tree-top level. The radar feeds target information into the central computer for effective weapons delivery. For close-in dog fights, the radar automatically acquires enemy aircraft, and this information is projected on the head-up display.
In addition to the F-15C AESA, Raytheon is developing AESAs for the F/A-18E/F Super Hornet. The Boeing Phantom Works unit led a team that received a $250 million contract to install the AESA radar, upgrade the aircraft's environmental control systems and install an advanced identification friend or foe system. Honeywell Aerospace and BAE Systems, respectively, provided the latter systems. The Air Force F-15 System Program Office's Projects Team at Wright-Patterson Air Force Base, Ohio, managed the program for the U.S. government.
An inertial navigation system enables the Eagle to navigate anywhere in the world. It gives aircraft position at all times as well as pitch, roll, heading, acceleration and speed information.
The F-15's electronic warfare system provides both threat warning and automatic countermeasures against selected threats. The "identification friend or foe" system informs the pilot if an aircraft seen visually or on radar is friendly. It also informs U.S. or allied ground stations and other suitably equipped aircraft that the F-15 is a friendly aircraft.
The Fiber Optic Towed Decoy (FOTD) provides aircraft protection against modern radar-guided missiles to supplement traditional radar jamming equipment. The device is towed at varying distances behind the aircraft while transmitting a signal like that of a threat radar. The missile will detect and lock onto the decoy rather than on the aircraft. This is achieved by making the decoy's radiated signal stronger than that of the aircraft.
A variety of air-to-air weaponry can be carried by the F-15. An automated weapon system enables the pilot to perform aerial combat safely and effectively, using the head-up display and the avionics and weapons controls located on the engine throttles or control stick. When the pilot changes from one weapon system to another, visual guidance for the required weapon automatically appears on the head-up display.
The Eagle can be armed with combinations of four different air-to-air weapons: AIM-7F/M Sparrow missiles or AIM-120 Advanced Medium Range Air-to-Air Missiles on its lower fuselage corners, AIM-9L/M Sidewinder or AIM-120 missiles on two pylons under the wings, and an internal 20mm Gatling gun (with 940 rounds of ammunition) in the right wing root.
The current AIM-9 missile does not have the capabilities demonstrated by foreign technologies, giving the F-15 a distinct disadvantage during IR dogfight scenarios. AIM-9X integration will once again put the F-15 in the air superiority position in all arenas. The F-15/AIM-9X weapon system is to consist of F-15 carriage of the AIM-9X missile on a LAU-128 Air-to-Air (A/A) launcher from existing AIM-9 certified stations. The AIM-9X will be an upgrade to the AIM-9L/M, incorporating increased missile maneuverability and allowing a high off-boresight targeting capability.
Low-drag, conformal fuel tanks were especially developed for the F-15C and D models. Conformal fuel tanks can be attached to the sides of the engine air intake trunks under each wing and are designed to the same load factors and airspeed limits as the basic aircraft. Each conformal fuel tank contains about 114 cubic feet of usable space. These tanks reduce the need for in-flight refueling on global missions and increase time in the combat area. All external stations for munitions remain available with the tanks in use. AIM-7F/M Sparrow and AIM-120 missiles, moreover, can be attached to the corners of the conformal fuel tanks.
Conformal Fuel Tanks [CFT] are carried in pairs and fit closely to the side of the aircraft, with one CFT underneath each wing. By designing the CFT to minimize the effect on aircraft aerodynamics, much lower drag results than if a similar amount of fuel is carried in conventional external fuel tanks. This lower drag translate directly into longer aircraft ranges, a particularly desirable characteristic of a deep strike fighter like the F-15E.

As with any system, the use of CFTs on F-15s involves some compromise. The weight and drag of the CFTs (even when empty) degrades aircraft performance when compared to external fuel tanks, which can be jettisoned when needed (CFTs are not jettisonable and can only be downloaded by maintenance crews). As a result, CFTs are typically used in situations where increased range offsets any performance drawbacks; for example, F-15s flying alert missions out of Keflavik, Iceland often encounter unforseen weather changes forcing them to fly more than 500 miles to an alternate landing field in Scotland or Norway. In the case of the F-15E, CFTs allow air-to-ground munitions to be loaded on stations which would otherwise carry external fuel tanks. In general, CFT usage is the norm for F15Es and the exception for F-15C/D's.
Specifications
VariantC/D modelsE/F models
Primary FunctionTactical fighter.Tactical Bomber
ContractorBoeing (McDonnell Aircraft and Missiles Systems)Boeing (McDonnell Aircraft and Missiles Systems)
Power PlantTwo Pratt & Whitney F100-PW-100 turbofan engines with afterburners, each rated at 25,000 pounds engine ( 11,250 kilograms)two Pratt and Whitney FIOO-P-220 turbofans each rated at 14,670 lb st (65.26 kN) dry and 23,830 lb st (106.0 kN) with afterburning or,
after August 1991, two FlOO-PW-229 each rated at 17,800 lb st (79.18 kN) dry and 29,100 lb st (129.45 kN) with afterburning;
Length63 feet, 9 inches (19.43 meters).63 ft 9 in (19.43 m)
Height18 feet, 8 inches (5.69 meters).18 ft 5.5 in (5.63 m)
Wingspan42 feet, 10 inches (13.06 meters)42ft 9.75 in (13.05 m)
Wing aspect ratio3.01
Wing area608.00 sq ft (56.48 m2)
Speed1,875 mph (Mach 2.5-plus).1,433 kt (1,650 mph; 2655 km/h) maximum level speed 'clean' at high altitude
495 kt (570 mph; 917 km/h) cruising speed at optimum altitude
Ceiling65,000 feet (19,697 meters).60,000 ft (18290 m);
Operating Empty Weight31,700 lb (14379 kg)
Maximum Takeoff Weight68,000 pounds (30,600 kilograms).81,000 lb (36741 kg)
fuel13,123 lb (5952 kg) internal
21,645 lb (9818 kg) in two CFTs
up to three 610-US gal (2309-liter~ drop tanks;
Range3,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks.3,100 nm (3,570 miles; 5745 km) ferry range with CFTs and drop tanks
2,400 nm (2,765 miles; 4445 km) with drop tanks
1,000 nm (1,150 mi; 1,853 km) Max Combat Radius
685 nm (790 miles; 1270 km) combat radius
Systems
  • AN/APG-63 X-band pulsed-Doppler radar [Hughes]
  • AN/APG-63 V2 AESA X-band pulsed-Doppler radar [Raytheon] [ on F-15C/D]
  • AN/APG-63 V3 AESA X-band pulsed-Doppler radar [Raytheon] [ on F-15C/D, F-15SG]
  • AN/APG-70 X-band pulsed-Doppler radar [Hughes]
    [ on F-15E, F-15C/D, F-15A/B MSIP]
  • AN/APX-76 IFF interrogator [Hazeltine]
  • AN/ALQ-135(V) internal countermeasures system
  • AN/ALQ-128 radar warning[Magnavox] suite
  • AN/ALR-56 radar warning receiver (RWR) [Loral]
  • AN/ALE-45 chaff/flare dispensers[Tracor]

  • AN/APG-70 X-band pulsed-Doppler radar [Hughes]
    [ on F-15E, F-15C/D, F-15A/B MSIP]
  • AN/APG-63 V3 AESA X-band pulsed-Doppler radar [Raytheon] [ on F-15C/D, F-15SG]
  • AN/APG-82 AESA X-band pulsed-Doppler radar [Raytheon]
    [ on F-15E]
  • AN/AVQ-26 Pave Tack
  • AN/AXQ-14 Data Link System
  • LANTIRN
  • AN/APX-76 IFF interrogator [Hazeltine]
  • AN/ALQ-135(V) internal countermeasures system
  • AN/ALQ-128 radar warning [Magnavox] suite
  • AN/ALR-56 radar warning receiver (RWR) [Loral]
  • AN/ALE-45 chaff/flare dispensers[Tracor]
  • CrewF-15A/C: one. F-15B/D: two.two
    Unit cost $FY98
    [Total Program]
    $43 million.probably around $55 million for USAF
    close to $100 million (including spares and support) for export customers.
    Date DeployedJuly 1972April 1988
    Fuselage Lifetime8,000 hours16,000 hours
    Key Maintenance IndicatorsUnited States Air Forces standard
  • 81 % - Mission Capapble - Percentage of aircraft readily available to do the mission.
  • 15 % - Not Mission Capable for Maintenance - Percentage not mission capable for maintenance reasons.
  • 9 % - Not Mission Capable for Supply - Percentage not mission capable for supply reasons.
  • 6 % - Abort Rate - Rate of aircraft that cannot fly sorties due to ground or air abort.
  • 19 % - Break Rate - Number of Code 3s divided by total number of sorties flown. Different aircraft codes indicate mission capability upon completion of a sortie: Code One is mission capable. Code 2 is an aircraft with a problem but is still mission capable. Code 3 is an aircraft not mission capable until problem is fixed.
  • 75 % - Fix Rate - Percentage of Code 3 aircraft fixed in eight-hour period.
  • 18 % - Cannibilization Rate - Percentage of cannibalizations (parts taken from one aircraft to fix another) divided by number of sorties.
  • 9 % - Repeat/Recur Rate - Percentage of repeats or recurs divided by total of pilot-reported discrepancies.
  • 95 % - Maintenance Scheduling Effectiveness Rate - Percentage of maintenance scheduling actions done on time.
  • 88 % - Flying Scheduling Effectiveness Rate - Ability to fly selected aircraft without deviation
  • Armament

    F-15C Weapon Loads

    1 - M-61A1 20mm multibarrel internal gun, 940 rounds of ammunition
    4 - AIM-9L/M Sidewinder and
    4 - AIM-7F/M Sparrow missiles, or
    combination of AIM-9L/M, AIM-7-F/M and AIM-120 missiles.
    AIMAIMAIMAGM20
    7912088MM
    44900
    422900
    224900
    444900
    444900
    8900

    F-15E Weapon Loads

    1 - M-61A1 20mm multibarrel internal gun, 512 rounds of ammunition
    4 - AIM-9L/M Sidewinder on the underwing stations and
    4 - AIM-7F/M Sparrow missiles conformal fuel tank
    up to eight AIM-120 AMRAAM missiles
    12 CBU-52 (6 with wing tanks)
    12 CBU-59 (6 with wing tanks)
    12 CBU-71 (6 with wing tanks)
    12 CBU-87 (6 with wing tanks)
    12 CBU-89 (6 with wing tanks)
    20 MK-20 (6 with wing tanks)

    Lockheed SR-71 Blackbird

    Lockheed SR-71 Blackbird


    Stealth and threat avoidance    

    Water vapor is condensed by the low-pressure vortices generated by the chines outboard of each engine inlet.
    The first operational aircraft designed around a stealthy shape and materials, the SR-71 had several features designed to reduce its radar signature. The SR-71 had a radar cross section (RCS) of around 10 square meters, much greater than the later Lockheed F-117 Nighthawk, which had an RCS equivalent in size to a ball bearing.Drawing on the first studies in radar stealth technology, which indicated that a shape with flattened, tapering sides would reflect most radar energy away from the radar beams' place of origin, engineers added chines and canted the vertical control surfaces inward. Special radar-absorbing materials were incorporated into sawtooth-shaped sections of the aircraft's skin. Cesium-based substances were added to the fuel to somewhat reduce the visibility of the exhaust plumes to radar, although the large and hot exhaust stream produced at speed remained quite apparent. For all this effort, Kelly Johnson later conceded that Soviet radar technology advanced faster than the stealth technology employed against it.
    The SR-71 carried electronic countermeasures, but its greatest protection was its high speed and cruising altitude that made it almost invulnerable to the weapons of its day. Merely accelerating would typically be enough to evade a surface-to-air missile, and the plane was faster than the Soviet Union's principal interceptor, the MiG-25. In its service life, no SR-71 was shot down, despite many attempts to do so.
    Few weapon systems have ever entered the military arena with such blinding superiority as did the Lockheed SR-71 Blackbird. No weapon system has ever maintained that same degree of superiority over a period of four decades. Today, the Blackbird is still the fastest, highest-flying, most-effective reconnaissance aircraft in history, even though budgetary considerations have caused it to be withdrawn from active service.
    Like the U-2, a product of the U.S. government's super-secret Skunk Works research & development center, the Lockheed SR-71 Blackbird is a perfect expression of Kelly Johnson's genius and his leadership of a brilliant team of fewer than 200 engineers.
    The USAF's SR-71 was a two-seat development of the earlier A-12 aircraft used by the Central Intelligence Agency. The Lockheed SR-71 Blackbird first flew on December 22, 1964, and by December 1967, all 31 of the Blackbirds had been delivered to the USAF.
    The Blackbird was both a miracle of design and of production, for its performance (speed of Mach 3.2, more than 90,000 feet of altitude, a 4,000-mile range) had to overcome not only the sound barrier, but also the heat barrier. Skin temperatures of the craft exceeded 1,050 degrees Fahrenheit. Special fuels, hydraulic fluids, electronics, and glass had to be developed to match the strength of the aircraft's titanium structure.
    A Lockheed SR-71 Blackbird, flown invariably by a highly skilled crew, became an invulnerable, invaluable reconnaissance aircraft. Unlike satellites in fixed orbits, the SR-71 could be deployed within hours to anywhere in the world.
    The usefulness of the Lockheed SR-71 Blackbird went beyond military applications to diplomatic roles. During the 1973 Middle East Yom Kippur War, reconnaissance photos taken by the SR-71 determined the positions of the advancing Israeli forces, and were used during subsequent peace negotiations. And as a research instrument, the SR-71 has few peers; although officially retired, Blackbirds are rumored to be occasionally flown -- "unofficially" -- in NASA research.
    Blackbirds set many records for speed and altitude, the last one a transcontinental speed record of less than 68 minutes -- on the delivery flight of a retired SR-71 to the National Air and Space Museum in Washington, D.C.

    LOCKHEED SR-71 BLACKBIRD SPECIFICATIONS

    Wingspan: 55 ft. 7 in.
    Length: 107 ft. 5 in.
    Height: 18 ft. 6 in.
    Empty Weight: 60,000 lbs
    Gross Weight: 170,000 lbs
    Top Speed: Mach 3.2-plus
    Service Ceiling: 90,000 ft.-plus
    Range: 2,600 miles
    Engine/Thrust: Two Pratt & Whitney J58 turbojets/32,500 lbs each
    Crew: 2
    Equipment: Wide range of classified intelligence-gathering equipment

    Alien Spaceship

    Alien Spaceship

    Looking to build the perfect classic alien spaceship, huh? Well you've come to the right place! My design firm has built thousands of these things, so I'll throw some ideas out and you can tell me what you think:
    For the interior, first off, I'm thinking CATWALKS. We should have sterile, metal catwalks spiraling all over the damn place, and every inch of every wall should be covered in tubes. What kind of tubes? Insider Tip: It doesn't matter, they're just there for decoration, but if any of them get pulled out of the wall, they'll start shooting out dry-ice smoke for some reason. Sure, these smoke-shooting purposeless tubes will run you a few extra Rembulaxx (our form of money, as you already know), but it's the direction everyone's going in, and it'll definitely up the resale value.
    For lighting, I'm thinking we go nice and traditional. Three words: Light Blue EVERYTHING. It'll mostly be pitch black, but then bathed in a really futuristic-seeming light blue, because MAN, do we love that color. Also we can coordinate the interior light-blue with the light-blue tractor beam, force field, and the lasers that we shoot. Also it's literally the only color of bulb available at Spaceship Depotblorff, so it's stylish and practical.
    For the Medical Room, I'm thinking we paint everything SUPER white. Like, creepy-ass white, with an impossibly spotless glowing tile floor and one really ominous slab-shaped table in the very center. Then we surround the table with weird automated arms coming out of the ceiling with drills and stuff jutting out of them, which is partly aesthetic, but also useful for doing weird, scary operations. It's sleek, it's elegant, and Hyper-Scareminism is very in right now.
    A couple other random design thoughts:
    - The core should be a big pulsating aqua-colored thing that makes a low bass hum at all times and can easily be set to self-destruct. (It's not technically a Ranch unless you can bump a button and have it self destruct.)
    - There should be one room with a bunch of glass pods containing a weird liquid and gross embryos. Can double-function as a breakfast nook.
    - All the doors are slidey and automatic and make whooshing noises. Also they get dangerously sealed off anytime anything happens.
    - The temperature is constantly super-hot or super-cold. Just something not normal, because we are aliens.
    - Granite countertops and stainless steel appliances. Like, uhhhDUHHHH.
    And finally, here's the kicker: the entire ship will be CIRCULAR. And the whole thing SPINS when it flies. And it emits a shrill, kinda Theremin-sounding "eeehooooeeehoooooeeehooo" noise whenever it's in the air, so it sounds like a loud, broken ray gun, but constantly.
    What's that? You'll "be in touch?" Ok! Do you want to take my card? It's a clear blue microchip that plugs into a holo-puter that's different looking than computers now but will look crappy and dated in eleven years. No, you'll just call me? Oh, alright.
    Well, I will talk to you soon then! And let me know ASAP so I can get started on pricing that purple embryo-preserving juice!