Sunday, March 23, 2008

United States Department of Defense - T-6 Texan II


The T-6A Texan II is a single-engined turboprop aircraft built by the Raytheon Aircraft Company (now Hawker Beechcraft). It is used by the United States Air Force for basic pilot training and by the United States Navy for Primary and Intermediate Joint Naval Flight Officer (NFO) and Air Force Navigator / Weapon Systems Officer (WSO) training. It is replacing the Air Force's T-37B Tweet and the Navy's T-34C Turbo Mentor. The T-6A is also used as a basic trainer by the Canadian Forces (CT-156 Harvard II) and the Greek Air Force.

The T-6 is a version of the Pilatus PC-9, modified significantly by Beechcraft in order to enter the Joint Primary Aircraft Training System (JPATS) competition in the 1990s. The aircraft was designated under the 1962 United States Tri-Service aircraft designation system named for the decades-earlier T-6 Texan. A similar arrangement between Pilatus and British Aerospace had also been in place for an RAF competition in the 1980s, although this competition selected the Shorts Tucano. The Beechcraft brand has since been purchased from Raytheon by Onex Corporation as Hawker Beechcraft.

The Texan II is built by Hawker Beechcraft in Wichita, Kansas. Although the design is heavily based on the Pilatus PC-9, the T-6 is a complete redesign from the ground up, and is considerably more sophisticated and powerful.

United States Department of Defense - RQ-4 Global Hawk


The Northrop Grumman (formerly Ryan Aeronautical) RQ-4 Global Hawk (known as Tier II+ during development) is an unmanned aerial vehicle (UAV) used by the US Air Force as a surveillance aircraft.

n role and design, it is somewhat similar to the Lockheed U-2, the venerable 1950s spy plane. It is a theater commander's asset to both provide a broad overview and systematically target surveillance shortfalls. The Global Hawk air vehicle is able to provide high resolution Synthetic Aperture Radar (SAR)—that can penetrate cloud-cover and sandstorms—and Electro-Optical/Infrared (EO/IR) imagery at long range with long loiter times over target areas. It can survey as much as 100,000 square kilometers (40,000 square miles) of terrain a day. If a Global Hawk were flown out from San Francisco, it would be able to operate in Maine for 24 hours, observe a 370 x 370 kilometer (230 x 230 mile) grid, and then fly back home.

Potential missions for the Global Hawk cover the spectrum of intelligence collection capability to support forces in worldwide peace, crisis, and wartime operations. According to the Air Force, the capabilities of the aircraft will allow more precise targeting of weapons and better protection of forces through superior surveillance capabilities.

The "R" is the Department of Defense designation for reconnaissance; "Q" means unmanned aircraft system. The "4" refers to it being the fourth of a series of purpose-built unmanned aircraft systems. "A" or "B" refers to these being the first and second versions, respectively.

The Global Hawk is the first UAV to be certified by the FAA to file its own flight plans and use civilian air corridors in the United States with no advance notice. This potentially paves the way for a revolution in unmanned flight, including that of automatically piloted passenger airliners.

The RQ-4 is powered by an Allison Rolls-Royce AE3007H turbofan engine with 31.4 kN (3,200 kgf / 7,050 lbf) thrust, and carries a payload of 900 kilograms (2,000 pounds). The fuselage is mostly of conventional aluminum airframe construction, while the wings are made of carbon composite.

The Global Hawk costs about $35 million USD each (actual per-aircraft costs; with development costs also included, the per-aircraft cost rises to $123.2 million USD each).

United States Department of Defense - MQ-1 Predator


The MQ-1 Predator is an unmanned aerial vehicle (UAV) which the U.S. Air Force describes as a MALE (medium-altitude, long-endurance) UAV system. It can serve in a reconnaissance role, and it can also carry and use two AGM-114 Hellfire missiles. The aircraft has been in use since 1995, and been in combat over Afghanistan, Bosnia, Serbia, Iraq, and Yemen. It is remote-controlled by humans, not an autonomous aircraft.

The MQ-1 Predator is a system, not just an aircraft. The fully operational system consists of four air vehicles (with sensors), a ground control station (GCS), a Predator primary satellite link communication suite and 55 people. In the over-all U.S. Air Force integrated UAV system, the Predator is considered a "Tier II" vehicle.

The Predator system was initially designated the RQ-1 Predator, with the "R" is the Department of Defense designation for reconnaissance, "Q" means unmanned aircraft system. The "1" describes it as being the first of a series of purpose-built unmanned reconnaissance aircraft systems. Pre-production systems were designated as RQ-1A, while the RQ-1B (not to be confused with the RQ-1 Predator B, which became the MQ-9 Reaper) denotes the baseline production configuration. It should be emphasized that these are designations of the system as a unit. The actual aircraft themselves were designated RQ-1K for pre-production models, and RQ-1L for production models. In 2002, the Air Force officially changed the designation to MQ-1 (the "M" designates multi-role) to reflect its growing use as an armed aircraft.

United States Department of Defense - CH-53 Sea Stallion


The CH-53 Sea Stallion is the most common name for the Sikorsky S-65 family of heavy-lift transport helicopters. Originally developed for use by the United States Marine Corps, it is also in service with Germany, Mexico, Iran, Israel, and as the MH-53 Pave Low with the United States Air Force. The USAF also operated the HH-53 "Super Jolly Green Giant" during the late- and post-Viet Nam War era.

The dimensionally-similar CH-53E Super Stallion is a heavier-lifting, improved version designated S-80E by Sikorsky. Its third engine makes it more powerful than the Sea Stallion, which it has replaced in the heavy-lift mission.

The Sea Stallion has a fuselage design similar to the Sikorsky S-61R/Jolly Green Giant series. It has a passenger door on the right side of the fuselage behind the cockpit and a power-operated rear loading ramp. The fuselage was watertight, though not intended for amphibious use, and only landed on water in emergencies. The Stallion has mechanical flight controls which are backed by two independent hydraulic systems. Armor protects crew and vital systems.

The CH-53A carries a crew of four; pilot, copilot, crew chief, and "aerial observer", a load of 38 troops, 24 litters with medical attendants, an internal cargo load of 8,000 pounds (3,630 kg) or an external load of 13,000 lb (5,900 kg) on the single-point sling hook. The CH-53A is equipped with a pair of M60 0.308 in (7.62 mm) machine guns that point out to each side of the fuselage.

The CH-53A features the six-bladed main rotor and four-bladed tail rotor proven on the S-64. To save space on board naval vessels, the tail boom and the rotors folded. The rotor system was initially driven by twin GE T64-GE-6 turboshafts providing 2,850 shp (2,125 kW) each, with an engine on each side of the forward fuselage. It was later produced with the T64-GE-1 with 3,080 shp (2,300 kW) and then the T64-GE-16 with 3,485 shp (2,600 kW).The HH-53B featured T64-GE-3 engines producing 3,080 shp (2,297 kW).

The CH-53D features uprated engines, initially T64-GE-412 with 3,695 shp (2,755 kW) then the T64-GE-413 with 3,925 shp (2,930 kW) with an uprated transmission. Its interior added seats to allow for 55 troops. CH-53Ds are generally armed with twin 0.50 in (12.7 mm) M2/XM218 machine guns. In later years, CH-53Ds have been fitted with defensive countermeasures including an AN/ALE-39 chaff dispenser and an AN/ALQ-157 infrared set.

Later production CH-53Ds featured a Blade Inspection Method (BIM) scheme to detect cracks in its metal rotors. BIM involved pressurizing the interior of the rotor blades. If a crack is present pressure is lost and a red indicator on the rotor blade tip was tripped. Later, the BIM system was connected to a cockpit display. BIM reduced the need to swap out rotor blades on a routine basis.

United States Department of Defense - Mil Mi-8


The Mil Mi-8 (NATO reporting name "Hip") is a medium twin-turbine transport helicopter that can also act as a gunship. The first single-engine (AI-24W) prototype, W-8, flew in 9 July 1961. A second one with two AI-24W engines made its first flight on 17 September 1962. After few changes it was introduced into the Soviet Air Force by 1967 as Mi-8.

The Mi-8 is the world's most-produced helicopter, and is used by over 50 countries. There are numerous variants, including the Mi-8T which is armed with rockets and anti-tank guided missiles, in addition to carrying twenty four soldiers. The Mil Mi-17 export version is employed by around 20 countries; its equivalent in Russian service in the Mi-8M series. The naval Mil Mi-14 and attack Mil Mi-24 are also derived from the Mi-8.

United States Department of Defense - HH-60 Pave Hawk


The Sikorsky HH-60 Pave Hawk is a combat search and rescue (CSAR) helicopter derivative of the Sikorsky S-70 family. The HH-60's primary function is to conduct day or night combat search and rescue operations into hostile environments to recover downed aircrew or other isolated personnel during war. Because of its versatility, the HH-60G may also perform peace-time operations. Such tasks include civil search and rescue, emergency aeromedical evacuation (MEDEVAC), disaster relief, international aid, counter-drug activities and NASA space shuttle support.

The Pave Hawk is a highly-modified version of the Sikorsky UH-60 Black Hawk helicopter, manufactured by United Technologies's Sikorsky Aircraft Corporation and first deployed in 1982. It features an upgraded communications and navigation suite that includes an integrated inertial navigation/global positioning/Doppler navigation systems, satellite communications, secure voice, and Have Quick communications.

All HH-60Gs have an automatic flight control system, night vision goggles lighting and forward looking infrared system that greatly enhances night low-level operations. Additionally, some Pave Hawks have color weather radar and an engine/rotor blade anti-ice system that gives the HH-60G an all-weather capability.

Pave Hawk mission equipment includes a retractable in-flight refueling probe, internal auxiliary fuel tanks, two crew-served (or pilot-controlled) 7.62 mm miniguns or .50 caliber machine guns and an 8,000 pound (3,600 kg) capacity cargo hook. To improve air transportability and shipboard operations, all HH-60Gs have folding rotor blades.

Pave Hawk combat enhancements include a radar warning receiver, infrared jammer and a flare/chaff countermeasure dispensing system.

HH-60G rescue equipment includes a hoist capable of lifting a 600 pound (270 kg) load from a hover height of 200 feet (60 m), and a personnel locating system that is compatible with the PRC-112 survival radio and provides range and bearing information to a survivor's location.

A limited number of Pave Hawks are equipped with an over-the-horizon tactical data receiver that is capable of receiving near real-time mission update information.

Variants

* HH-60A: Prototype for the HH-60D rescue helicopter.
* HH-60D: Prototype of early search and rescue variant for the US Air Force.
* HH-60E: Proposed search and rescue variant for the US Air Force
* HH-60G Pave Hawk: Search and rescue helicopter for the US Air Force.
* MH-60G Pave Hawk: Special Operations, search and rescue model for the U.S. Air Force.
* Maplehawk: Proposed search and rescue version for Canada.

United States Department of Defense - MH-53 Pave Low


The Sikorsky HH-53 "Super Jolly Green Giant" is a USAF version of the CH-53 Sea Stallion helicopter for long-range combat search and rescue (CSAR) helicopters. It was developed to replace the HH-3 "Jolly Green Giant"". The HH-53s were later upgraded as MH-53 Pave Low series.

The USAF MH-53J/M fleet is scheduled for retirement, effective 1 October 2008.

The US Air Force ordered HH-53B and HH-53C variants for Search and Rescue units, and developed the MH-53J Pave Low version for Special Operations missions.

The Pave Low's mission is low-level, long-range, undetected penetration into denied areas, day or night, in adverse weather, for infiltration, exfiltration and resupply of special operations forces. Pave Low's often work in conjunction with MC-130H Combat Talon for navigation, communications and combat support,and with MC-130P Combat Shadow for inflight refueling.

Although officially known as the Stallion, the large green airframe of the HH-53B earned it the nickname "Super Jolly Green Giant." This name is a reference to the smaller HH-3E "Jolly Green Giant", a stretched variant of the H-3 Sea King, used in the Vietnam War for combat search-and-rescue (CSAR) operations.

United States Department of Defense - F-117 Nighthawk


The Lockheed F-117 Night Hawk is a stealth ground attack aircraft operated solely by the United States Air Force. The F-117A's first flight was in 1981, and it achieved Initial Operational Capability status in October 1983. The F-117A came out of secrecy and was revealed to the world in November 1988.

As a product of the Skunk Works and a development of the Have Blue prototype, it became the first operational aircraft initially designed around stealth technology. The F-117A was widely publicized during the Gulf War.

The Air Force will retire the F-117 on 21 April 2008, primarily due to the purchasing and eventual deployment of the more effective F-22 Raptor and F-35 Lightning II.

About the size of an F-15C Eagle, the single-seat F-117A is powered by two non-afterburning General Electric F404 turbofan engines, and has quadruple-redundant fly-by-wire flight controls. It is air refuelable. In order to lower development costs, the avionics, fly-by-wire systems, and other parts are derived from the F-16 Fighting Falcon, F/A-18 Hornet and F-15E Strike Eagle. The parts were originally described as spares on budgets for these aircraft, to keep the F-117 project secret.

Among the penalties for stealth are lower engine power thrust, due to losses in the inlet and outlet, a very low wing aspect ratio, and a high sweep angle (50°) needed to deflect incoming radar waves to the sides.

The F-117A is equipped with sophisticated navigation and attack systems integrated into a digital avionics suite. It carries no radar, which lowers emissions and cross-section. It navigates primarily by GPS and high-accuracy inertial navigation. Missions are coordinated by an automated planning system that can automatically perform all aspects of a strike mission, including weapons release. Targets are acquired by a thermal imaging infrared system, slaved to a laser that finds the range and designates targets for laser-guided bombs.

The F-117A's split internal bay can carry 5,000 lb (2,300 kg) of ordnance. Typical weapons are a pair of GBU-10, GBU-12, or GBU-27 laser-guided bombs, two BLU-109 penetration bombs, or two Joint Direct Attack Munitions (JDAMs), a GPS/INS guided stand-off bomb.

United States Department of Defense - F-22 Raptor


The Lockheed Martin/Boeing F-22 Raptor is an American fighter aircraft that uses stealth technology. It is primarily an air superiority fighter, but has multiple capabilities that include ground attack, electronic warfare, and signals intelligence roles. The United States Air Force considers the F-22 a critical component of the U.S. strike force.

Faced with a protracted development period, the aircraft was variously designated F-22 and F/A-22 during the three years before formally entering US Air Force service in December 2005, as the F-22A. Lockheed Martin Aeronautics is the prime contractor and is responsible for the majority of the airframe, weapon systems and final assembly of the F-22. Program partner Boeing Integrated Defense Systems provides the wings, aft fuselage, avionics integration, and all of the pilot and maintenance training systems.

The F-22 is claimed by several sources to be the world’s most effective air superiority fighter. The US Air Force claims that the F-22 cannot be matched by any known or projected fighter aircraft. Chief of the Australian Defence Force, then-Air Marshal Angus Houston, said in 2004 that the "F-22 will be the most outstanding fighter plane ever built."

The F-22 is a fifth-generation fighter that is considered a fourth-generation stealth aircraft by the USAF.Its dual afterburning Pratt & Whitney F119-PW-100 turbofans incorporate thrust vectoring, but in the pitch axis only, with a range of ±20 degrees. The maximum thrust is classified, though most sources place it at about 35,000 lbf (156 kN) per engine. Maximum speed, without external weapons, is estimated to be Mach 1.72 in supercruise mode; as demonstrated by General John P. Jumper, former US Air Force Chief of Staff, when his Raptor exceeded Mach 1.7 without afterburners on 13 January 2005.With afterburners, it is "greater than Mach 2.0" (1,317 mph, 2,120 km/h), according to Lockheed Martin; however, the Raptor can easily exceed its design speed limits, particularly at low altitudes, with max-speed alerts to help prevent the pilot from exceeding them. Former Lockheed Raptor chief test pilot Paul Metz stated that the Raptor has a fixed inlet; but while the absence of variable intake ramps may theoretically make speeds greater than Mach 2.0 unreachable, there is no evidence to prove this. Such ramps would be used to prevent engine surge, but the intake itself may be designed to prevent this. Metz has also stated that the F-22 has a top speed greater than 1,600 mph (Mach 2.42) and its climb rate is faster than the F-15 Eagle due to advances in engine technology, despite the F-15's thrust-to-weight ratio of about 1.2:1, with the F-22 having a ratio closer to 1:1. The US Air Force claims that the F-22A cannot be matched by any known or projected fighter.

The true top-speed of the F-22 is largely unknown to the general public, as engine power is only one factor. The ability of the airframe to withstand the stress and heat from friction is a further, key factor, especially in an aircraft using as many polymers as the F-22. However, while some aircraft are faster on paper, the internal carriage of its standard combat load allows the aircraft to reach comparatively higher performance with a heavy load over other modern aircraft due to its lack of drag from external stores. It is one of only a handful of aircraft that can sustain supersonic flight without the use of afterburner augmented thrust (and its associated high fuel usage). This ability is called supercruise.

The F-22 is highly maneuverable, at both supersonic and subsonic speeds. The F-22's thrust vectoring nozzles allow the aircraft to turn tightly, and perform extremely high alpha (angle of attack) maneuvers such as the Herbst maneuver (or J-turn), Pugachev's Cobra, and the Kulbit, though the J-Turn is more useful in combat.The F-22 is also capable of maintaining a constant angle of attack of over 60°, yet still having some control of roll. During June 2006 exercises in Alaska, F-22 pilots demonstrated that cruise altitude has a significant effect on combat performance, and routinely attributed their altitude advantage as a major factor in achieving an unblemished kill ratio.

United States Department of Defense - F-16 Fighting Falcon


The Lockheed Martin F-16 Fighting Falcon is an American multirole jet fighter aircraft originally developed by General Dynamics for the United States Air Force. Designed as a lightweight fighter, it evolved into a successful multirole aircraft. The Falcon's versatility is a paramount reason it was a success on the export market, serving 24 countries.The F-16 is the largest Western fighter program with over 4,000 aircraft built since production started in 1976. Though no longer produced for the US Air Force, it is still produced for export. In 1993, General Dynamics sold its aircraft manufacturing business to the Lockheed Corporation,which in turn became part of Lockheed Martin after a 1995 merger with Martin Marietta.

The Fighting Falcon is a dogfighter with innovations including a frameless, bubble canopy for better visibility, side-mounted control stick to ease control while under high g-forces, and reclined seat to reduce the effect of g-forces on the pilot. It was also the first fighter aircraft to be deliberately built to sustain 9-g turns. It has a thrust-to-weight ratio greater than one, providing enough power to climb and accelerate vertically - if necessary. Although the F-16's official name is "Fighting Falcon", it is known to its pilots as the "Viper", after the Battlestar Galactica starfighter.

During the 1960s, the U.S. Air Force and Navy both concluded that the future of air combat would be determined by increasingly sophisticated missiles. Future "fighters" would be designed primarily for long range, high speed, and equipped with extremely large radar systems in order to detect opposing fighters at beyond visual range (BVR). This made them much more like interceptors than classic fighter designs. In the early 1960s, both the Air Force and Navy expected to use the F-111 (then still in development as the TFX) and F-4 Phantoms for their long and medium range needs complemented by several single-engine designs including upgraded F-100 Super Sabres, F-104 Starfighters, and F-8 Crusaders. Future twin-engine fighter programs were getting underway and the Air Force began a replacement for its single-engine fighter designs to maintain its high-low mix of air superiority aircraft.

Real-world experience in the Vietnam War showed the continued need for the 'high-low' fighter matrix system. Soviet-bloc fighters over Vietnam were proving to be more of a problem than expected for US designs. Even though the US had very large kills to losses ratio in its favor, combat revealed some shortcomings. Missiles of this era still had notable reliability issues, and restrictions on how they were functionally used. Combat invariably closed to short ranges where air-combat maneuverability and short range air-air weapons became critical. Dedicated interceptors like the F-102 Delta Dagger had also been tested in combat which revealed certain shortcomings. Although US training, doctrine and air control more than made up for these disadvantages, it was nevertheless clear to some in the Air Force that the all-missile doctrine was seriously flawed. Both aircraft of the future high-low mix for the USAF would have guns (F-15 and F-16).

In particular, Colonel John Boyd developed the theory of energy maintenance in fighter combat, which relied on larger wings in order to preserve maneuverability. Larger wings would mean more drag in flight, usually resulting in lower range and slower top speed (although larger wings can also result in greater range due to increased payload and fuel). He felt this was a fair trade-off for a "real" fighter design. At about this time the navalized F-111 was running into serious problems, and was eventually abandoned in favor of a new design, the F-14 Tomcat. A combination of Boyd's tireless advocacy of maneuverability, and what is often viewed as a failure of the F-111 to develop into a suitable fighter, and notably the rather over-inflated performance estimates of the MiG-25 led the USAF to also start development of their own fighter design, the F-15 Eagle.

It was not long before the F-15 started growing into a very large design that appeared to be turning into an "F-111 mark II". Boyd was frustrated by this development, and convinced a number of others that the F-15 would need to be complemented by larger numbers of smaller fighters like previous twin-engine fighters. A group of interested parties formed the self-named "fighter mafia" and agitated for the development of the Light Weight Fighter. They eventually won a small amount of money, only $149,000 (~$715,000 year 2000 dollars) to conduct studies into such a design. Northrop had always been a proponent of light-weight designs and had continually developed plans for an advanced F-5 Freedom Fighter, and received $100,000. General Dynamics, looking to redeem themselves from the controversial F-111, received the remainder.

In May 1971, the US Congress released a report that was highly critical of both the F-14 and F-15 programs. They proposed funding the LWF with $50 million and an additional $12 million the next year. Several companies submitted proposals, but General Dynamics and Northrop had such a head start that they were both asked to produce prototypes for head-to-head testing. These were ready in 1974, and in extensive testing General Dynamics' YF-16 proved somewhat better overall, winning the LWF contest.

By this time a number of countries were looking for a multi-role replacement for their existing F-104Gs and other older designs. Up to this point, the LWF was merely an evaluation program with no plans to purchase models, but the possibility of a European order led the Pentagon to reconsider. The Air Force was now seeking a multi-role fighter to replace the F-105, so the program was renamed the Air Combat Fighter (ACF). In September 1974, the Air Force announced plans to purchase 650 ACF's. On 13 January 1975, Secretary of the Air Force John McLucas announced the selection of the YF-16, beating out Northrop's YF-17.

The F-16 is planned to remain in service with the U.S. Air Force until 2025. The planned replacement is the F-35 Lightning II, which is scheduled to enter service in 2011 and will gradually begin replacing a number of multirole aircraft among the air forces of the program's member nations.

United States Department of Defense - F-15E Strike Eagle


The F-15E Strike Eagle is a modern American all-weather strike fighter, designed for long-range interdiction of enemy ground targets deep behind enemy lines. A derivative of the F-15 Eagle air superiority fighter, the Strike Eagle proved its worth in Desert Storm, carrying out deep strikes against high-value targets, performing "Wild Weasel" (SEAD) patrols and providing close air support for coalition troops. The F-15E Strike Eagle can be distinguished from other U.S. Eagle variants by its darker camouflage and the conformal fuel tanks mounted along the engine intakes.

In March 1981, the USAF announced the Enhanced Tactical Fighter program to procure a replacement for the F-111 'Aardvark'. The concept envisioned an aircraft capable of launching deep interdiction missions without requiring additional support by fighter escort or jamming. General Dynamics submitted the F-16XL, while McDonnell Douglas submitted a variant of the F-15 Eagle. On February 24, 1984, the USAF awarded the ETF to McDonnell Douglas's F-15E Strike Eagle.he F-15E's first flight was on December 11, 1986.The first production model of the F-15E was delivered to the 405th Tactical Training Wing, Luke Air Force Base, Ariz., in April 1988. The "Strike Eagle", as it was dubbed, received initial operational capability on September 30, 1989 at Seymour Johnson AFB in North Carolina with the 4th Tactical Fighter Wing, 336th Tactical Fighter Squadron.

Variants of the F-15E have been developed for Israel (F-15I), Korea (F-15K), Saudi Arabia (F-15S), and Singapore (F-15SG).

The F-15E will be upgraded with the Raytheon APG-63(V)4 Active Electronically Scanned Array (AESA) radar after 2007. It combines the processor of the APG-79 used on the F/A-18E/F with the antenna of the APG-63(V)3 AESA being fitted on the F-15C.The radar upgrade is expected to begin in 2008.

While most of the F-15C/Ds are being replaced by the F-22 Raptor there is no slated replacement for the F-15E. The Strike Eagle is a more recent variant of the F-15, and has a sturdier airframe rated for twice the lifetime of earlier variants. The F-15Es are expected to remain in service past 2025. The Air Force is currently pursuing the 2018 Bomber, a medium bomber concept which could also take over the Strike Eagle's "deep strike" profile. The "A" variant of the F-35 Lightning II, which is projected to eventually replace many other attack aircraft such as the F-16 and A-10, could also take over much of the F-15E's role.

United States Department of Defense - F-15A Eagle


The McDonnell Douglas (now Boeing) F-15 Eagle is an all-weather tactical fighter designed to gain and maintain air superiority in aerial combat. It was developed for the U.S. Air Force, and first flew in July 1972. The F-15E Strike Eagle derivative is an all-weather strike fighter that entered service in 1989. The U.S. Air Force plans to keep the F-15 in service until 2025.

Origins

During the mid-1960s U.S. Air Force intelligence was surprised to find that the Soviet Union was building a large fighter aircraft, known as the MiG-25 "Foxbat". It was not known in the West at the time that the MiG-25 was designed as a high-speed interceptor, not an air superiority fighter;as such, its primary asset was speed, not maneuverability. The MiG-25's huge tailplanes and vertical stabilizers (tail fins) hinted at a very maneuverable aircraft, which worried the Air Force that its performance might be higher than its American counterparts. In reality, the MiG's large fins and stabilators were necessary to prevent the aircraft from encountering inertia coupling in high-speed, high-altitude flight.

The F-4 Phantom II of the USAF and U.S. Navy was the only fighter with enough power, range and maneuverability to be given the primary task of dealing with the threat of Soviet fighters while flying with visual engagement rules. As a matter of policy, the Phantoms could not engage targets without positive visual identification, so they could not engage targets at long ranges, as designed. Medium-range AIM-7 Sparrow missiles, and to a lesser degree even the AIM-9 Sidewinder, were often unreliable and ineffective at close ranges where it was found that guns were often the only effective weapon.

The Phantom did not originally have a gun, as it was intended that only missiles would be used to engage slowly moving and maneuvering Warsaw Pact bombers and fighters at longer ranges. Experience in Vietnam showed this not to be the case and led to the addition of a gun. At first an external gun pod was tried but that proved inaccurate and increased drag. Later, the 20 mm M61 Vulcan was integrated internally on the F-4E.

United States Department of Defense - E-3 Sentry


The Boeing E-3 Sentry is an American military airborne warning and control system (AWACS) aircraft that provides all-weather surveillance, command, control and communications, to the United States, United Kingdom, France, Saudi Arabia, and NATO air defense forces. Production ended in 1992 after 68 had been built.

The E-3 Sentry is a modified Boeing 707-320B Advanced commercial airframe. Modifications included a rotating radar dome, single-point ground, and air refueling points. The dome is 30 feet (9.1 m) in diameter, six feet (1.8 m) thick at the center, and is held 14 feet (4.2 m) above the fuselage by two struts. It contains a hydraulically rotated antenna system that permits the AN/APY-1/2 passive electronically scanned array radar system to provide surveillance from the Earth's surface up into the stratosphere, over land or water. Generators on each of the four engines provide the 1 megawatt of power required by the radar. The Pulse Doppler radar has a range of more than 250 miles (375 km) for low-flying targets at its operating altitude (essentially to the radar horizon), and the Pulse(BTH) beyond the horizon radar has a range of approximately 400 miles for aerospace vehicles flying at medium to high altitudes (essentially above the radar horizon). The radar combined with an SSR subsystem can look down to detect, identify and track enemy and friendly low-flying aircraft by eliminating ground clutter returns.

Variants

EC-137D
Two prototype AWACS aircraft with JT3D engines, one fitted with a Westinghouse radar and the other with a Hughes radar. Both converted to E-3A standard with TF33 engines.

E-3A
Production aircraft with TF33 engines and AN/APY-1 radar, 25 built for USAF later converted to E-3B standard. 18 built for NATO with TF33 engines and five for Saudi Arabia with CFM56 engines.

KE-3A
These are not AWACS aircraft but CFM56 powered tankers for Saudia Arabia, 8 built.

E-3B
E-3As converted with AN/APY-2 radar and other improvements, 24 conversions.

E-3C
Production aircraft with system improvements, nine built. NATO E-3A aircraft although not re-designated have been modified to the same equipment standard.

JE-3C
One E-3A aircraft used by Boeing for trials later redesignated E-3C.

E-3D
Production aircraft for the Royal Air Force to E-3C standard with CFM56 engines and British modifications designated Sentry AEW1, seven built.

E-3F
Production aircraft for the French Air Force to E-3C standard with CFM56 engines and French modifications, four built.

Sentry AEW1
British designation for the E-3D.

Saturday, March 22, 2008

United States Department of Defense - Lockheed MC-130


The Lockheed MC-130 is the basic designation for a family of special-missions aircraft operated by the United States Air Force. Based on the C-130 Hercules transport, they are designed to provide infiltration, exfiltration, and resupply of special operations forces, as well as psychological operations support and helicopter air refueling. Variants include the MC-130E Combat Talon I, MC-130H Combat Talon II, MC-130P Combat Shadow, and MC-130W Combat Spear.

United States Department of Defense - Lockheed AC-130


The AC-130 gunship is a heavily-armed ground attack airplane. The basic airframe is manufactured by Lockheed, and Boeing is responsible for the conversion into a gunship and for aircraft support. It is a variant of the C-130 Hercules transport plane. The AC-130 Gunship II superseded the AC-47 Gunship I in Vietnam.

The gunship's sole user is the United States Air Force, which uses AC-130H Spectre and AC-130U Spooky variants. The AC-130 is powered by four turboprops and has an armament ranging from 20 mm Gatling guns to 105 mm howitzers. It has a standard crew of twelve to thirteen Airmen, including five officers (two pilots, a navigator, an electronic warfare officer and a fire control officer) and enlisted personnel (flight engineer, electronics operators and aerial gunners).

The US Air Force uses the AC-130 gunships for close air support, air interdiction, and force protection. Close air support roles include supporting ground troops, escorting convoys, and flying urban operations. Air interdiction missions are conducted against planned targets and targets of opportunity. Force protection missions include defending air bases and other military facilities. The gunship squadrons are part of the Air Force Special Operations Command and are all assigned to AFSOC at Hurlburt Field in Northwest Florida.

The C-130 Hercules was selected to replace the AC-47 Gunship I (known as Spooky or Puff the Magic Dragon) during the Vietnam War, due to its ability to carry more and heavier weapons, and better endurance.

In 1967, JC-130A USAF 54-1626 was selected for conversion into the prototype AC-130A gunship. The modifications were done that year at Wright-Patterson Air Force Base, by the Aeronautical Systems Division. A direct view night vision telescope was installed in the forward door, an early forward looking infrared (FLIR) in the forward part of the left wheel well, and Gatling guns fixed mounted facing down and aft along the left side. The analog fire control computer prototype was handcrafted by RAF Wing Commander Tom Pinkerton at the USAF Avionics Laboratory. Then flight testing of the prototype was performed primarily at Eglin Air Force Base, followed by further testing and modifications. By September 1967, the aircraft was certified ready for combat testing and was flown to Nha Trang Air Base, South Vietnam for a 90 day test program. Following these successes, a few more AC-130As were constructed using similar equipment and manufactured versions of the analog computer. The original 54-1626 Gunship is displayed at the USAF Museum.

The AC-130 was supplemented by the AC-119 Shadow Gunship III during this time, which would prove underpowered with warload. In 1970, an additional dozen AC-130As were acquired under the "Pave Pronto" project. Regardless of their project names, the aircraft were more commonly referred to by the Squadron's call sign of Spectre.

United States Department of Defense - C-130 Hercules


The Lockheed C-130 Hercules is an American four-engine turboprop military transport aircraft and the main tactical airlifter for many military forces worldwide. Over 40 models and variants of the Hercules serve with more than 50 nations. In December 2006, the C-130 became the fourth aircraft – after the English Electric Canberra in May 2001, the B-52 Stratofortress in January 2005 and the Tupolev Tu-95 in January 2006 – to mark 50 years of continuous use with its original primary customer, in this case the United States Air Force. The C-130 remains in production as the updated C-130J Super Hercules.

Capable of short takeoffs and landings from unprepared runways, the C-130 was originally designed as a troop, medical evacuation and cargo transport aircraft. The versatile airframe has found uses in a variety of other roles, including as a gunship, and for airborne assault, search and rescue, scientific research support, weather reconnaissance, aerial refuelling and aerial firefighting. The Hercules family has the longest continuous production run of any military aircraft in history. During more than 50 years of service the family has participated in military, civilian and humanitarian aid operations.

The Korean War, which began in June, 1950, showed that World War II-era transports—C-119 Flying Boxcars, C-47 Skytrains and C-46 Commandos—were inadequate for modern warfare. Thus, on February 2, 1951, the United States Air Force issued a General Operating Requirement (GOR) for a new transport to Boeing, Douglas, Fairchild, Lockheed, Martin, Chase Aircraft, North American Northrop, and Airlifts Inc. The new transport would have a capacity for 92 passengers, 72 combat troops or 64 paratroopers, a range of 1,100 nautical miles (2,000 km), takeoff capability from short and unprepared strips, and the ability to fly with one engine shut down.

Fairchild, North American, Martin and Northrop declined to participate. The remaining five companies tendered a total of ten designs: Lockheed two, Boeing one, Chase three, Douglas three, Airlifts Inc one. The contest was a close affair between the lighter of the two Lockheed (preliminary project designation L-206) proposals and a four-turboprop Douglas design. The Lockheed design team was led by Willis Hawkins starting with a 130 page proposal for the Lockheed L-206 and another two-turboprop and heavier one.Hall Hibbard, Lockheed vice president and chief engineer, saw the proposal and directed it to Kelly Johnson, who remarked when he saw the proposal, "If you sign that letter, you will destroy the Lockheed Company." Both Hibbard and Johnson signed the proposal and the company won the contract for the now-designated Model 82 on July 2, 1951.

United States Department of Defense - Boeing VC-25 "Air Force One"

Air Force One

The Boeing VC-25 is the designation of a United States Air Force passenger transportation aircraft, a military version of the Boeing 747.

The VC-25 is most famous for its role as Air Force One, the callsign of any U.S. Air Force aircraft carrying the President of the United States. The two aircraft currently in U.S. service are highly modified versions of Boeing's 747-200B, with tail numbers 28000 and 29000. Although the Air Force One designation technically applies to the planes only while the President is aboard, the term is commonly applied to the VC-25As more generally. They often operate in conjunction with Marine One, the helicopter which ferries the President to airports in circumstances where a vehicle motorcade would be inappropriate.

United States Department of Defense - C-17 Globemaster III


The Boeing (formerly McDonnell Douglas) C-17 Globemaster III is an American strategic airlifter manufactured by Boeing Integrated Defense Systems, and operated by the United States Air Force, British Royal Air Force, the Royal Australian Air Force, and the Canadian Forces Air Command. NATO also has plans to acquire the airlifter.

The C-17 Globemaster III is capable of rapid strategic delivery of troops and all types of cargo to main operating bases or directly to forward bases in the deployment area. It is also capable of performing tactical airlift, medical evacuation and airdrop missions. The C-17 takes its name from two previous United States cargo aircraft, the C-74 Globemaster and the C-124 Globemaster II.

In the 1970s, the US Air Force began looking for a replacement for the C-130 Hercules tactical airlifter. The Advanced Medium STOL Transport (AMST) competition was held, with Boeing proposing the YC-14, and McDonnell Douglas proposing the YC-15. Despite both entrants exceeding specified requirements, the AMST competition was canceled before a winner had been selected.

By the early 1980s, the USAF found itself with a large fleet of aging C-141 Starlifter cargo aircraft. Some of the C-141s had major structural problems due to heavy use. Compounding matters, USAF historically never possessed sufficient strategic airlift capabilities to fulfill its airlift requirements. In response, McDonnell Douglas elected to develop a new aircraft using the YC-15 as the basis. McDonnell Douglas was awarded a contract to build its proposed aircraft, by then designated the C-17A Globemaster III, on August 28, 1981. The new aircraft differed in having swept wings, increased size, and more powerful engines. This would allow it to perform all work performed by the C-141, but to also fulfill some of the duties of the C-5 Galaxy, freeing the C-5 fleet for larger outsize cargo.

Development continued until December 1985 when a full-scale production contract was signed for 210 aircraft. Development problems and limited funding caused delays in the late 1980s. Questions were also raised about more cost-effective alternatives during this time. In April 1990, Defense Secretary Richard Cheney reduced the order from 210 to 120 aircraft. The C-17's maiden flight was on September 15, 1991 from the McDonnell Douglas west coast plant in Long Beach, California, about a year behind schedule. This aircraft (T-1) and five more production models (P1-P5) participated in extensive flight testing and evaluation at Edwards AFB. In late 1993, the DoD gave the contractor two years to solve production and cost overrun problems or face termination of the contract after the delivery of the fortieth aircraft. By accepting the 1993 terms, McDonnell Douglas incurred a loss of nearly US$1.5 billion on the development phase of the program.

In April 1994, the C-17 program was still experiencing cost overruns, and did not meet weight, fuel burn, payload and range specifications. Airflow issues caused problems with parachutes and there were various other technical problems with mission software, landing gear, etc.A July 1994 GAO document revealed that to justify investing in the C-17 rather than in the C-5, Air Force and DoD studies from 1986 and 1991 had claimed that the C-17 could use 6,400 more runways (outside the US) than the C-5. It was later discovered that this study had only considered the runway dimensions, but not their strength or Load Classification Numbers (LCN). The C-5 has a lower LCN than the C-17, although the US Air Force places both in the same broad Load Classification Group (LCG). When considering runway dimensions and their load ratings, the C-17's worldwide runway advantage over the C-5 shrank from 6,400 to 911 airfields.However, the C-17's ability to use lower quality, austere airfields was not considered.

A January 1995 GAO report revealed that while the original C-17 budget was US$41.8 billion for 210 aircraft, the 120 aircraft already ordered at that point had already cost US$39.5 billion. In March 1994, the U.S. Army had decided it no longer needed the 60,000 lb (27,000 kg) Low Altitude Parachute Extraction System (LAPES) delivery that the C-17 was supposed to provide, feeling that the 42,000 lb (19,000 kg) capability of the C-130 Hercules was sufficient. It was decided not to conduct C-17 LAPES training beyond the testing of a 42,000 lb (19,000 kg) LAPES delivery. There were still airflow problems making it impossible for the C-17 to meet its original airdrop requirements. A February 1997 GAO Report revealed that a C-17 with a full payload could not land on 3,000 feet (900 m) wet runways, for simulations suggested 5,000 ft (1,500 m) was required.

By the mid-1990s, most of the problems had been resolved. The first C-17 squadron was declared operational by the U.S. Air Force in January 1995. In 1996, DoD ordered another 80 aircraft for a total of 120. In 1997 McDonnell Douglas merged with its former competitor, Boeing. In 1998, the order was increased to 134 units and in August 2002 to 180.

In July 2006, C-17A production was planned to end in 2009 unless Boeing received a follow-on order in sufficient time to allow the production pipeline to remain in operation. If such an order is placed, Boeing would begin C-17B production in 2010. The proposed C-17B would be capable of landing on sandy beaches and other areas off-limits to the C-17A.

On August 18, 2006 Boeing announced it was telling suppliers to stop work on parts for uncommitted C-17s. This move is the first step in shutting down production if no new plane orders were received from the US Government. However, just one month later on September 21, a House and Senate conference committee approved a US$447 billion defense bill for 2007, that includes US$2.1 billion for 10 additional C-17s – which is seven more planes than either chamber originally approved in separate versions of their funding language. The additional purchase follows intense lobbying by Boeing, as well as by California state leaders (where the plane is manufactured), and Missouri leaders, where Boeing's defense business is based. However, this extends the life of the program for only one additional year, to 2010.

On March 2, 2007, Boeing announced the C-17 production line may end in mid-2009 due to the lack of additional US government and international orders.
A total of 190 C-17s are contracted for delivery to the USAF as of October 24, 2007. Efforts are underway to add a further 10 C-17s to a funding/supplemental bill so that production may be extended to 2010 and to allow for further potential FMS purchases to take effect.

United States Department of Defense - C-5 Galaxy


The Lockheed C-5 Galaxy is an American military transport aircraft built by Lockheed. It was designed to provide strategic heavy airlift over intercontinental distances and to carry outsize and oversize cargo. The C-5 Galaxy has been operated by the United States Air Force since 1969 and is one of the largest military aircraft in the world.
In 1961, several aircraft companies began studying heavy jet transport designs that would replace the C-133 transport and complement C-141 Starlifters. In addition to higher overall performance, the US Army wanted a transport with a larger cargo bay than the C-141, whose interior was too small to carry a variety of their outsized equipment. These studies led to the "CX-4" design concept, but in 1962 the proposed six-engine design was rejected, because it was not viewed as a significant advance over the C-141.

By late 1963, the next conceptual design was named CX-X. It was equipped with four engines, instead of six engines in the earlier CX-4 concept. The CX-X had a gross weight of 550,000 pounds (249,000 kg), a maximum payload of 180,000 pounds (81,600 kg) and a speed of Mach 0.75 (500 mph/805 km/h). The cargo compartment was 17.2 feet (5.24 m) wide by 13.5 feet (4.11 m) high and 100 feet (30.5 m) long with front and rear access doors. In order to provide the required power and range with only four engines, a new engine with dramatically improved fuel economy would be needed.

The criteria were finalized and an official Request for Proposal was sent out in April 1964 for the "Heavy Logistics System" (CX-HLS) (previously CX-X). In May 1964, proposals for aircraft were received from Boeing, Douglas, General Dynamics, Lockheed, and Martin Marietta. Proposals for engines were received from General Electric, Curtiss-Wright Corporation, and Pratt & Whitney. After a downselect, Boeing, Douglas and Lockheed were given additional study contracts for the airframe, along with General Electric and Pratt and Whitney for the engines.

All three of the designs shared a number of features. In particular, all three placed the cockpit well above the cargo area so that in a crash the cargo would not crush the crew as it moved forward. The Boeing and Douglas designs used a "pod" on the top of the fuselage containing the the cockpit, while the Lockheed design extended the cockpit line the length of the fuselage, giving it an egg-shaped cross section. All of the designs featured swept wings, T-tails, and front and rear cargo doors allowing simultaneous loading and unloading.

In 1965 Lockheed's aircraft design and General Electric's engine design were selected for the new transport.

United States Department of Defense - B-52 Stratofortress


The Boeing B-52 Stratofortress is a long-range, subsonic, jet-powered, strategic bomber flown by the United States Air Force (USAF) since 1955.

Beginning with the successful contract bid on 5 June 1946, the B-52 went through several designs, from a straight wing aircraft powered by six turboprop engines, to the final prototype, YB-52 (with 8 engines), which first flew on 15 April 1952 by "Tex" Johnston.

Built to carry nuclear weapons for Cold War-era deterrence missions, the B-52 Stratofortress replaced the Convair B-36. Although a veteran of a number of wars, the Stratofortress has dropped only conventional munitions in actual combat. With the longest unrefuelled range of any contemporary bomber, the B-52 carries up to 70,000 pounds of weapons.

The USAF has had B-52s in active service since 1955 with Strategic Air Command and were later absorbed into Air Combat Command in 1992. Superior performance at high subsonic speeds and relatively low operating costs have kept the B-52 in service despite proposals to replace it with the Mach 3 XB-70 Valkyrie, supersonic B-1B Lancer and stealthy B-2 Spirit. In January 2005, the B-52 became the second aircraft, after the English Electric Canberra, to mark 50 years of continuous service with its original primary operator.

On 23 November 1945, Air Materiel Command (AMC) issued desired performance characteristics for a new strategic bomber "capable of carrying out the strategic mission without dependence upon advanced and intermediate bases controlled by other countries".The aircraft was to have a crew of five plus turret gunners, and a six-man relief crew. It had to cruise at 300 Miles per hour (240 kn, 480 km/h) at 34,000 feet (10,400 m) with a combat radius of 5,000 statute miles (4,300 nmi, 8,000 km). The armament was to consist of an unspecified number of 20 mm cannon and 10,000 pounds (4,500 kg) of bombs. On 13 February 1946, the Air Force issued bid invitations for these specifications, with Boeing, Consolidated Aircraft, and Glenn L. Martin Company submitting proposals.


On 5 June 1946, Boeing's Model 462, a straight-wing aircraft powered by six Wright T-35 turboprops with a gross weight of 360,000 pounds (160,000 kg) and combat radius of 3,110 statute miles (2,700 nmi, 5,010 km), was declared the winner.On 28 June 1946, Boeing was issued a letter of contract for US$1.7 million (1946 dollars) to build a full-scale mock-up of the new XB-52 and do preliminary engineering and testing. However, by October 1946, the Air Force began to express concern about the sheer size of the new aircraft and its inability to meet the specified design requirements. In response, Boeing produced Model 464, a smaller four-engine version with a 230,000 pound (105,000 kg) gross weight, which was briefly deemed acceptable.

Then, in November 1946, the Deputy Chief of Air Staff for Research and Development Curtis LeMay expressed the desire for a cruise speed of 400 miles per hour (345 kn, 645 km/h), to which Boeing responded with a 300,000 pound (140,000 kg) aircraft. In December 1946, Boeing was asked to change their design to a four-engine bomber with a top speed of 400 miles per hour, range of 12,000 statute miles (10,000 nmi, 19,000 km), and the ability to carry a nuclear weapon. The aircraft could weigh up to 480,000 pounds (220,000 kg). Boeing responded with two models powered by the T-35 turboprops. The Model 464-16 was a "nuclear-only" bomber with a 10,000 pound payload, while the Model 464-17 was a general purpose bomber with a 90,000 pound (40,000 kg) payload. Due to the cost associated with purchasing two specialized aircraft, the Air Force selected Model 464-17 with the understanding that it could be adapted for nuclear strikes.

In June 1947 the military requirements were updated and the Model 464-17 met all of them except for the range. It was becoming obvious to the Air Force that, even with the updated performance, the XB-52 would be obsolete by the time it entered production and would offer little improvement over the Convair B-36. As the result, the entire project was put on hold for six months. During this time, Boeing continued to perfect the design which resulted in the Model 464-29 with a top speed of 455 miles per hour (395 kn, 730 km/h) and a 5,000-mile range. In September 1947, the Heavy Bombardment Committee was convened to ascertain performance requirements for a nuclear bomber. Formalized on 8 December 1947, these called for a top speed of 500 miles per hour (440 kn, 800 km/h) and an 8,000 statute mile (7,000 nmi, 13,000 km) range, far beyond the capabilities of 464-29.

The outright cancellation of the Boeing contract on 11 December 1947 was staved off by a plea from its president William McPherson Allen, and in January 1948 Boeing was instructed to thoroughly explore recent technological innovations, including aerial refueling and the flying wing. Noting stability and control problems Northrop was experiencing with their YB-35 and YB-49 flying wing bombers, Boeing insisted on a conventional aircraft, and in April 1948 presented a US$30 million (1948 dollars) proposal for design, construction, and testing of two Model 464-35 prototypes. Further revisions of specifications during 1948 resulted in an aircraft with a top speed of 513 miles per hour (445 kn, 825 km/h) at 35,000 feet (10,700 m), a range of 6,909 statute miles (6,005 nmi, 11,125 km), and a 280,000 pounds (125,000 kg) gross weight which included 10,000 pounds of bombs and 19,875 US gallons (75,225 L) of fuel.

United States Department of Defense - B-2 Spirit


The Northrop Grumman B-2 Spirit is a multi-role stealth heavy bomber, capable of deploying both conventional and nuclear weapons. It is operated exclusively by the United States Air Force. Its development was a milestone in the modernization program of the U.S. Department of Defense. The B-2's stealth technology is intended to aid the aircraft's penetration role in order to survive extremely dense anti-aircraft defenses otherwise considered impenetrable by combat aircraft.

The B-2 started life as a black project known as the High Altitude Penetrating Bomber (HAPB), then became the Advanced Technology Bomber (ATB), which became the B-2 Spirit. The bomber's design was changed in the mid-1980s when its mission profile was changed from high-altitude to low-altitude, terrain following. The redesign delayed the B-2's first flight by two years and added about $1 billion to the program's cost.[4] An estimated US$23 billion was secretly spent for research and development on the B-2 in the 1980s.[citation needed]

The first B-2 was publicly displayed on 22 November 1988, when it was rolled out of its hangar at Air Force Plant 42, Palmdale, California, where it was built. Its first public flight was on 17 July 1989. The B-2 Combined Test Force, Air Force Flight Test Center, Edwards Air Force Base, California, is responsible for flight testing the engineering, manufacturing and development aircraft.


The original procurement of 132 aircraft was later reduced to 75 in the late 1980s. In his 1992 State of the Union Address, President George H.W. Bush announced total B-2 production would be limited to 20 aircraft, with a total inventory of 21 by upgrading the first test aircraft to B-2A Block 30 standard.This reduction was largely a result of the disintegration of the Soviet Union, which effectively rendered void the Spirit's primary mission.

The cost of the B-2 program in 1994 dollars was reported at $737 million per plane; however, the total cost of the program with development, spares, and facilities averaged over $2.1 billion per plane as of 1997 according to the B-2 program office.

Northrop made a proposal to the USAF in the late 1990s to build additional aircraft for ~$550M each. This more accurately reflects the per aircraft cost if the full order had been manufactured. The high development costs included: another stealth prototype (now at the USAF museum), security costs which included inefficiencies of separating design teams, the development of a computer aided design system which requires no paper (it was the first aircraft so designed), a totally computerized manufacturing control system (the first of its kind), and a computerized maintenance system to help crew chiefs with the most complex aircraft yet made.

Armament

* 2 internal bays for 50,000 lb (22,700 kg) of ordnance.[25]
o 80× 500 lb class bombs (Mk-82) mounted on Bomb Rack Assembly (BRA)
o 36× 750 lb CBU class bombs on BRA
o 16× 2000 lb class weapons (Mk-84, JDAM-84, JDAM-102) mounted on Rotary Launcher Assembly (RLA)
o 16× B61 or B83 nuclear weapons on RLA

United States Department of Defense - B-1 Lancer


The B-1 Lancer is an American supersonic strategic bomber with variable-sweep wings. Its origins began in the 1960s as a supersonic bomber with sufficient range and payload to replace the B-52 Stratofortress. The B-1B production version has been in service with the United States Air Force (USAF) since 1986. The Lancer serves as the supersonic-capable component of the USAF's long-range bomber force, with the subsonic B-52 and B-2 Spirit. As with several official popular names, the Lancer is commonly called the "Bone" (originally from "B-One") within the USAF. With the retirement of the EF-111 Raven in 1998 and the F-14 Tomcat in 2006, the B-1B is the last variable-sweep wing aircraft remaining in U.S. military inventory.

Variants

B-1A/B

The B-1A was original B-1 design with variable engine intakes and Mach 2.2 top speed. Four prototypes were built.

The B-1B is the improved B-1 design with reduced radar signature and a top speed of Mach 1.25. A total of 100 B-1B were produced.

B-1R

The B-1R is a proposed replacement for the B-1B fleet. Boeing's director of global strike integration, Rich Parke, was first quoted about the "B-1R" bomber in Air Force Magazine. Parke said the B-1R (R stands for "regional") would be a Lancer with advanced radars, air-to-air missiles, and Pratt & Whitney F119 engines (originally developed for the F-22 Raptor). Its new top speed of Mach 2.2 would be purchased at the price of a 20% reduction of the B-1B's combat range. This proposal would involve modifying existing aircraft. The FB-22 and YF-23-based design are alternative proposals.


Boeing's proposal appears to modify the B-1B into a design able to serve these two purposes. For the bomb-truck role Boeing proposes the modification of existing external hardpoints to allow them to carry multiple conventional warheads, dramatically improving overall warload. For the air-to-air role, both defensive and offensive, they propose to add active electronically-scanned array radar and allow some of the hardpoints to carry AA missiles. Even with its somewhat reduced range as compared to the original B-1B, its fuel capacity remains quite large. This would allow it to escape from unfavorable air-to-air encounters by simply running away; there are few enough aircraft capable of Mach 2.2 performance in general, and those that are deployed can maintain these speeds for only very short periods of time.

In general terms the B-1R most closely resembles the original F-111 concept, as opposed to a pure bomber role. However it would be able to carry out these missions at ranges even greater than the F-111.

United States Department of Defense - Antonov An-26


The Antonov An-26 (NATO reporting name: "Curl") is a twin-engined light turboprop transport aircraft and is a development of the Antonov An-24, with particular attention made to the potential military use. First seen in 1969, it has a modified rear fuselage with a large cargo ramp. The An-26 is also manufactured without a licence in China by Xian Aircraft Factory as the Y-14, though the designation later changed back to the Y-7 series.

Design and development

* An-26 "Curl-A" : Twin-engined tactical transport aircraft.
* In 1981, An-26B was introduced. The main character of it is that it is equipped with roller gangs which can be swung up against the cabin walls when not in use. It was also equipped with two ZMDB Progress(Ivchyenko)Al-24VT turboprop engines for more power.
* An-26BRL : Ice research aircraft.
* An-26L : Airfield calibration version.
* An-26M : Air ambulance version.
* An-26P : Fire fighting version.
* An-26RTR "Curl-B" : Elint, sigint, electronic warfare aircraft.
* An-26ST : Special duties aircraft for the East German Air Force.
* Y-7H : Military transport version. Chinese production version.
* Y-7-500 : Civilian cargo version. Chinese production version.

United States Department of Defense - A-10 Thunderbolt II


The A-10 Thunderbolt II is an American single-seat, twin-engine jet aircraft developed by Fairchild-Republic for the United States Air Force to provide close air support (CAS) of ground forces by attacking tanks, armored vehicles, and other ground targets, also providing a limited air interdiction role. It is the first U.S. Air Force aircraft designed exclusively for close air support.

The A-10's official name comes from the Republic P-47 Thunderbolt of World War II, a fighter that was particularly effective at the CAS mission. However, the A-10 is more commonly known by its nickname "Warthog" or simply "Hog". As a secondary mission, it provides airborne forward air control, guiding other aircraft against ground targets. In the USAF inventory, the airframe is designated OA-10 when used primarily in a forward air control role.

There had been, over the years, some criticism of the U.S. Air Force not taking the role of close air support seriously enough which prompted a few members of the USAF hierarchy to desire a specialized close air support attack aircraft. In the Vietnam War large numbers of ground-attack aircraft were shot down by small arms fire, surface-to-air missiles, and low level anti-aircraft gunfire indicating that modern combat aircraft were still vulnerable to such defensive measures and prompted the development of an aircraft better able to survive such an environment. In addition, the UH-1 Huey and AH-1 Cobra helicopters of the day, which USAF commanders had said should handle the close air support role, were ill-suited for use against armor, carrying only anti-personnel machine guns and unguided rockets meant for soft targets. The F-4 Phantom was pressed into use as a CAS aircraft, but usually on an emergency basis, as its high cruising speed and fuel consumption rate hindered its ability to loiter, and the lack of an onboard gun on most F-4 variants coupled with the relative ineffectiveness of the standard 20mm Vulcan round against hard targets made strafing runs either ineffective or impossible.

On 6 March 1967, the U.S. Air Force released a request for information to 21 companies. Their objective was to create a design study for a low cost attack aircraft designated A-X, or "Attack Experimental". The officer in charge of the project was Col. Avery Kay. In 1969, the Secretary of the Air Force asked Pierre Sprey to write the detailed specifications for the proposed A-X project. However, his initial involvement was kept secret due to Sprey's earlier controversial involvement in the F-X project. Sprey's discussions with A-1 Skyraider pilots operating in Vietnam and analysis of the effectiveness of current aircraft used in the role indicated the ideal aircraft should have long loiter time, low-speed maneuverability, massive cannon firepower, and extreme survivability. Based upon this information Sprey felt the need to build an aircraft incorporating the best elements of the Ilyushin Il-2, Henschel Hs 129 and A-1 Skyraider. The specifications also demanded that the cost of the aircraft be less than 3 million dollars. In May 1970, the USAF issued a modified, and much more detailed request for proposals (RFP), as the threat of Soviet armored forces and all weather attack operations became more serious. Six companies submitted proposals to the USAF, with Northrop and Fairchild Republic selected to build prototypes: the YA-9A and YA-10A, respectively.

The YA-10A first flew on 10 May 1972. After trials and a fly-off against the YA-9A, the Air Force selected Fairchild-Republic's YA-10A on 10 January 1973 for production. (There was an additional fly-off against the A-7D Corsair II, the Air Force attack aircraft at the time, to prove the need to purchase a new aircraft) The first production A-10 flew in October 1975, and deliveries to the Air Force commenced in March 1976, to units at Davis-Monthan Air Force Base, Arizona. The first squadron to use the A-10 went operational in October 1977. In total, 715 airplanes were produced, the last in 1984.

One experimental two-seat A-10 Night Adverse Weather (N/AW) version was built by converting an A-10A. The Night Adverse Weather (N/AW) aircraft was developed by Fairchild from the first Demonstration Testing and Evaluation (DT&E) A-10 for consideration by the USAF. It included a second seat for a weapons officer responsible for ECM, navigation, and target acquisition. The variant was canceled and the only two-seat A-10 built now sits at Edwards Air Force Base awaiting a spot in the Flight Test Historical Foundation museum. The proposed two-seat A-10 trainer aircraft did not go into production, as it was felt that the A-10 was simple enough to fly that a trainer version would not be required.

The decision to make the 30 mm GAU-8 gun the main anti-tank weapon of the A-10 was influenced by Vietnam A-1 pilots and by Hans-Ulrich Rudel and his book, "Stuka Pilot". In World War II, Rudel flew the Ju 87G Stuka and destroyed many tanks using its two underwing 37 mm guns. His book was required reading for members on the A-X project. The JU-87G was an outmoded airframe with ersatz anti-tank weapons attached, yet still inflicted impressive casualties on Soviet tank forces.

A-10s were initially an unwelcome addition to the arsenal in the eyes of Air Force brass. The Air Force prized the high-flying, high-performance F-15 Eagle and F-16 Fighting Falcon air-superiority jets, and were determined to leave the dirty work of close air support to Army helicopters (the development of the AGM-114 Hellfire anti-armor missile and AH-64 Apache attack helicopter having since provided the Army with a viable anti-tank aircraft). Attempts to transfer the A-10 to the Army and the Marines were at first prevented by the 1948 Key West Agreement, and then by the A-10's impressive combat record during the Gulf War in 1991. Shortly after the war, the Air Force gave up on the idea of replacing the A-10 with a close air support version of the F-16.

Weapons Systems

Although the A-10 can carry a considerable weight of disposable stores, its primary built-in weapon is the 30 mm GAU-8/A Avenger Gatling gun. One of the most powerful aircraft cannons ever flown, it fires large depleted uranium armor-piercing shells. In the original design, the rate of fire was selectable, 2,100 rounds per minute in the low setting, or 4,200 in the high setting. Later this was changed to a fixed rate of 3,900 rounds per minute. The cannon takes about half a second to come up to speed, so 50 rounds are fired during the first second, 70 or 65 rounds per second thereafter. The gun is accurate as well, being capable of placing 80% of its shots within a 40-foot- (12.4 meter-) wide circle from a distance of 4,000 feet (1,800 meters) while the aircraft is in flight.[17] A two-second burst, therefore, will on average result in about 100 hits on a tank-sized target. The GAU-8 is optimized for slant range of 4,000 feet (1,800 m) with the A-10 in a 30 degree dive.

The fuselage of the aircraft is actually built around the gun. For example, the nosewheel is offset to the right so that the gun's firing barrel at the 9 o'clock position is aligned on the aircraft's centerline. The early A-10s carried 1,350 rounds of 30 mm ammunition. It was replaced by the 1,174 round drum. The helix in the 1,350 round drums were being damaged during loading. The 1,174 round drums were beefed up to accommodate real world conditions. The damage caused by a portion of those rounds firing prematurely due to impact of an explosive shell would be catastrophic. It is for this reason that a great deal of effort has been taken to protect the 5 ft (1.52 m) wide, 9 ft (2.74 m) long drum. There are many plates of differing thicknesses between the skin and the drum. These plates are called trigger plates because when an explosive shell hits a target it first penetrates its armor, then detonates. As the drum has many layers of thin armor, the shell's detonation is triggered before reaching the drum. A final layer of armor around the drum itself protects it from fragmentation damage. The gun is loaded by Syn-Tech's linked tube carrier GFU-7/E 30 mm ammunition loading assembly cart. This vehicle is unique to the A-10 and the GAU-8.

Another commonly used weapon is the AGM-65 Maverick air-to-surface missile, with different variations for either electro-optical (TV-guided) or infra-red targeting. The Maverick allows targets to be engaged at much greater ranges than the cannon, a safer proposition in the face of modern anti-aircraft systems. During Desert Storm, in the absence of dedicated forward-looking infrared cameras, the Maverick's infra-red camera was used for night missions as a "poor man's FLIR". Other weapons include cluster bombs and Hydra rocket pods. Although the A-10 is equipped to deliver laser-guided bombs, their use is relatively uncommon; at the low altitudes and speeds of typical A-10 operations, standard unguided bombs provide adequate accuracy at far lower cost. In any event, the guided weapons would provide little benefit, as there would be nearly no time for the weapons to steer onto a target. A-10s usually fly with an ALQ-131 ECM pod under one wing and two AIM-9 Sidewinder air-to-air missiles under the other for self-defense.

Variants

YA-10A
The first two prototypes.
A-10A
Single-seat close air support, ground-attack version.
OA-10A
Single-seat forward air control version.
YA-10B Night/Adverse Weather A-10
Two-seat experimental prototype, for night and adverse weather work. Later redesignated YA-10B. Only one example was built, which is now on static display.
A-10C
A-10As updated under the incremental Precision Engagement (PE) program featuring a new glass cockpit (including digital moving map displays), advanced datalink, and all-weather multi-mission precision weapons and laser targeting capability.

Friday, March 21, 2008

United States Department of Defense - United States Air Force


The United States Air Force (USAF) is the aerial warfare branch of the United States armed forces and one of the seven uniformed services of the U.S.. Previously part of the United States Army, the USAF was formed as a separate branch of the military on September 18, 1947.

The USAF is the largest and most technologically advanced air force in the world, with about 6013 manned aircraft in service (4,282 USAF; 1,321 Air National Guard; and 410 Air Force Reserve); approximately 160 Unmanned Combat Air Vehicles, 2161 Air-Launched Cruise Missiles, and 580 Intercontinental Ballistic Missiles;and as of September 30, 2006, had 334,200 personnel on active duty, 120,369 in the Selected and Individual Ready Reserves, and 107,000 in the Air National Guard. An additional 10,675 personnel were in the Standby Reserve, and the Air Force employed 168,558 civilian personnel.

The USAF is currently planning a massive Reduction-in-Force (RIF). Because of budget constraints, the USAF will reduce the service's current size by 40,000 full time equivalent positions by 2011, with approximately half to be eliminated in FY 2007. Approximately 35,000 active duty positions (ADPs), or one year's cycle of enlistments and retirements, will be eliminated over 5 years. The current size of the active-duty force is roughly 70% of that of the USAF at the end of the first Gulf War in 1991.

Not all of the United States' military combat aircraft are operated by the USAF. The United States Army operates its own helicopters, mostly for support of ground combatants; it as well maintains a small fleet of fixed wing aircraft (mostly Unmanned Aerial Vehicles). The Navy is responsible for the aircraft operating on its aircraft carriers and Naval air stations, and the Marine Corps operates its own combat and transport aircraft. The Coast Guard also maintains transport and search-and-rescue aircraft (SARA), which may be used in a combat and law enforcement role. All branches of the U.S. military operate helicopters.

The Department of the Air Force is headed by the civilian Secretary of the Air Force who heads administrative affairs. The Department of the Air Force is a division of the United States Department of Defense which is headed by the United States Secretary of Defense. The highest ranking military officer in the department is the Chief of Staff of the Air Force.

United States Department of Defense - Federal Bureau of Investigation (FBI)


The Federal Bureau of Investigation (FBI) is the primary investigative arm of the United States Department of Justice (DOJ), serving as both a federal criminal investigative body and a domestic intelligence agency. At present, the FBI has investigative jurisdiction over violations of more than 200 categories of federal crimes, making the FBI the de-facto lead law enforcement agency of the United States government. The motto of the bureau is "Fidelity, Bravery, Integrity".

In fiscal year 2006, the FBI's total budget was approximately $8.7 billion, including $495 million in program increases to enhance counter-terrorism, counterintelligence, cyber crime, information technology, security, forensics, training, and criminal programs.

It was established in 1908 as the Bureau of Investigation (BOI), and the name was changed to the FBI in 1935.

The FBI headquarters is in Washington, D.C., and there are also has 56 field offices located in major cities throughout the United States as well as over 400 resident agencies in smaller cities and towns across the nation, and more than 50 international offices, called "Legal Attachés", in U.S. embassies worldwide.

Mission and priorities

The mission of the FBI is "To protect and defend the United States against terrorist and foreign intelligence threats, to uphold and enforce the criminal laws of the United States, and to provide leadership and criminal justice services to federal, state, municipal, and international agencies and partners."

Currently, the FBI's top investigative priorities are:

1. Protect the United States from terrorist attack (see counter-terrorism);
2. Protect the United States against foreign intelligence operations and espionage (see counter-intelligence);
3. Protect the United States against cyber-based attacks and high-technology crimes (see cyber-warfare);
4. Combat public corruption at all levels;
5. Protect civil rights;
6. Combat transnational/national criminal organizations and enterprises (see organized crime);
7. Combat major white-collar crime;
8. Combat significant violent crime;
9. Support federal, state, local and international partners; and
10. Upgrade technology for successful performance of the FBI's mission.

In August 2007, the top categories of lead criminal charges resulting from FBI investigations were:

1. Bank robbery and incidental crimes (107 charges)
2. Drugs (104 charges)
3. Attempt and conspiracy (81 charges)
4. Material involving sexual exploitation of minors (53 charges)
5. Mail fraud - frauds and swindles (51 charges)
6. Bank fraud (31 charges)
7. Prohibition of illegal gambling businesses (22 charges)
8. Fraud by wire, radio, or television (20 charges)
9. Hobbs Act (17 charges)
10. RICO - prohibited activities (17 charges)

Legal authority
An FBI Agent tags the cockpit voice recorder from EgyptAir Flight 990 on the deck of the USS Grapple (ARS 53) at the crash site on November 13, 1999.
An FBI Agent tags the cockpit voice recorder from EgyptAir Flight 990 on the deck of the USS Grapple (ARS 53) at the crash site on November 13, 1999.

The FBI's mandate is established in Title 28 of the United States Code (U.S. Code), Section 533, which authorizes the Attorney General to "appoint officials to detect... crimes against the United States." Other federal statutes give the FBI the authority and responsibility to investigate specific crimes.

The USA PATRIOT Act increased the powers allotted to the FBI, especially in wiretapping and monitoring of Internet activity. One of the most controversial provisions of the act is the so-called sneak and peek provision, granting the FBI powers to search a house while the residents are away, and not requiring them to notify the residents for several weeks afterwards. Under the PATRIOT Act's provisions the FBI also resumed inquiring into the library records of those who are suspected of terrorism (something it had supposedly not done since the 1970s).

The FBI's chief tool against organized crime is the Racketeer Influenced and Corrupt Organizations (RICO) Act. The FBI is also charged with the responsibility of enforcing compliance of the United States Civil Rights Act of 1964 and investigating violations of the act in addition to prosecuting such violations with the United States Department of Justice (DOJ). The FBI also shares concurrent jurisdiction with the Drug Enforcement Administration (DEA) in the enforcement of the Controlled Substances Act of 1970.

Information obtained through an FBI investigation is presented to the appropriate US Attorney or Department of Justice (DOJ) official, who decides if prosecution or other action is warranted.