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Minggu, 22 Januari 2012

PP-19 Bizon (Gun)



PP-19 Bizon
PP-19 Bizon right view.jpg
Type Submachine gun
Place of origin  Russia
Service history
In service 1996–present
Used by FSB, Ministry of Justice
Wars Dagestan conflict, Second Chechen War, 2008 South Ossetia war
Production history
Designer Viktor Kalashnikov, Alexi Dragunov
Designed 1993–1995
Manufacturer Izhmash
Variants See Variants
Specifications
Weight 2.1 kg (4.63 lb)
Length 660 mm (26.0 in) stock extended / 425 mm (16.7 in) stock folded (Bizon)
690 mm (27.2 in) stock extended / 460 mm (18.1 in) stock folded (Bizon-2)
Barrel length 195 mm (7.7 in) (Bizon)
230 mm (9.1 in) (Bizon-2 9x18mm Makarov)
225 mm (8.9 in) (Bizon-2-01 9x19mm Parabellum)

Cartridge 9x18mm Makarov
9x19mm Parabellum
.380 ACP (9x17mm Short)
7.62x25mm Tokarev
Action Blowback, closed bolt
Rate of fire 650–700 rounds/min
Muzzle velocity 320 m/s (1,050 ft/s) (9x18mm Makarov)
380 m/s (1,246.7 ft/s) (9x19mm Parabellum)
Effective range 100 m (9x18mm Makarov)
200 m (9x19mm Parabellum)
Feed system 64-round helical magazine (9x18mm Makarov)
53-round helical magazine (9x19mm Parabellum) (Bizon-2-01)
Sights Hooded front post, rear flip-up notc
The PP-19 Bizon ("Bison") is a 9mm submachine gun developed in the early 1990s at Izhmash by a team of engineers headed by Victor Kalashnikov (son of famed AK-47 designer Mikhail Kalashnikov).[1][2] Alexi Dragunov, youngest son of Evgeny Dragunov (responsible for the SVD sniper rifle), was also a member of the design team.[2][3]
The Bizon was developed at the request of the Ministry of Internal Affairs (MVD)[3] and is primarily intended for counter-terrorist and law enforcement units that usually need fast and accurate fire at close ranges. Prototypes were trialled by the Special Equipment Research Institute in 1995 where they outperformed several competitors, and the weapon was accepted into service on December 28, 1996. The Bizon is issued to armed response units of the Federal Security Service (FSB) and Ministry of Justice. It was used in combat operations against separatists in the volatile North Caucasus region, namely Chechnya and Dagestan.

Design details

The Bizon is a lightweight selective fire weapon that fires from a closed bolt, a trait that enhances the gun's accuracy.[2] It is based on the AKS-74 and features a 60% part commonality with the assault rifle.[1][2][3][4] Chambered for the standard Russian 9x18mm Makarov pistol cartridge, the gun will also fire a new high-impulse armor-piercing 57-N-181SM round.

Operating mechanism

The Bizon uses a simple straight blowback method of operation, an unlocked breech system reduces cost and build complexity.[2] The Bizon's operating cycle is characterized by a very short recoil stroke, standard 9x18mm ammunition will only drive the bolt partially to the rear of the receiver and produces a cyclic rate of 700 rounds/min.[5] High-impulse ammunition forces the bolt to travel all the way to the end of the receiver, barely striking the receiver wall. A rate of fire of 650–680 rounds/min is the result. This has the effect of reducing perceived recoil and increasing controllability and hit probability.[5]

Features

The Bizon has no gas system and the internal components have been modified accordingly. The bolt carrier with integral charging handle was recycled from the AK, however the piston rod and rotary bolt were removed and the piston extension was plugged with a steel insert.[5] The return spring and guide rod are identical to those of the AK.
The Bizon has a four-groove barrel with a 240 mm (1:9 in) right-hand rifling pitch.[5] The gun's muzzle device has a large rectangular port on each side of dead center that serves to reduce muzzle jump, however the main purpose of this device is to protect the muzzle and magazine from damage.[5]
The pinned and riveted sheet metal receiver of the Bizon is derived from the AKS-74 and has been modified at the front end, since the gas system was omitted.[6] The handguard is a sheet metal stamping with three rectangular ventilation slots on each side. The magazine serves as the lower handguard and the current models of the magazine are ribbed to enhance grip. The Bizon also shares the same trigger and safety mechanisms of the AK-74 rifle.[3][6] The selector lever is placed on the right side of the receiver, above the trigger, and has three settings: the uppermost "safe" setting disables the trigger and in this position the lever physically blocks the bolt's integral retracting handle; the middle position (marked "АВ") enables fully automatic fire and the lowest position ("ОД") will activate the semi-automatic function of the trigger.[6] An original five-piece anti-bounce device is built into the trigger unit and this functions as a rate reducer, delaying firing until the bolt has settled entirely into battery.[5]
The Bizon also utilizes the AKS-74 shoulder stock.[5] It folds to the left side of the receiver but unlike the AKS-74 and AKS-74U, it is not held closed by a spring-loaded capture in the forward end of the receiver. Instead, it is held closed by the forward trunnion pin which is longer on the Bizon than on its AKS-74 predecessors. The extended length of the pin allows it to catch the folding skeleton stock. The pistol grip is identical to the grip on the AK-100 series and is made of a black fiberglass-reinforced polyamide.[5]

Feeding

9mm submachine gun PP-19 Bizon with detached magazine
One of the Bizon's more unusual features is the magazine, which is often confused for a grenade launcher.[2] The cylinder below the barrel is in fact a 64-round helical-feed magazine, similar to the type used in the American Calico M960 submachine gun.[2] The magazine is made from a durable glass-reinforced polyamide and mounts under the handguard in line with the barrel. This layout makes the weapon more compact and concealable. All cartridges are aligned nose forward in the Bizon magazine and cannot be loaded incorrectly.[2][3] Early magazines were fabricated from aluminium tubing and had a capacity of 67 rounds.[2] The production magazine capacity of 64 was selected as 64 is a multiple of 16, and 9x18mm Makarov rounds are packaged in boxes of 16.[2] The magazine has hooks on top of the front end that engage a pair of pins under the front sight, and the rear end of the magazine interfaces with a Kalashnikov pattern spring-loaded paddle type magazine catch/release located in front of the trigger guard.[7] Some magazines were produced with indicator holes allowing the user to verify the amount of ammunition loaded; these are spaced at 4, 24, 44 and 64-round increments.[3]

Sights

Front view of 9mm submachine gun PP-19 Bizon
The sighting arrangement resembles that used on the AKS-74U and consists of a rear flip-up sight permanently attached to the receiver top cover with two open square notches with 50 and 100 m elevation settings and a round post front sight taken from the AK series of rifles, common to many Russian small arms. The front sight is contained in a protective hood with a hole in the top to insert an elevation adjustment tool, while the rear sight is shielded by two metal ears.[5]

Accessories

The gun is issued with one magazine, a sling, cleaning kit, oil can and magazine pouch.

Variants

The original Bizon was retroactively designated Bizon-1 after the design was improved with the introduction of the Bizon-2.[3]

Bizon-2

9mm submachine gun PP-19 Bizon left side view with folded buttstock
The Bizon has been continuously modified over its production life and the current model is the Bizon-2, which has AK-style iron sights (an open U-notch rear sight on a tangent with three settings: 50, 100 and 150 m and a semi-shrouded front post), a receiver-mounted side rail adapter for optics and a new slotted flash hider designed to accept a quick-detachable sound suppressor. The Bizon-2 is made in several variants to increase the product's commercial appeal and demonstrate its versatility; it is offered in 8 different configurations:
  • Bizon-2-01: Chambered for the NATO-standard 9x19mm Parabellum cartridge using a modified magazine with a 53-round capacity.
  • Bizon-2-02: Chambered in the .380 ACP (9x17mm Short) pistol round (64-round magazine capacity).
  • Bizon-2-03: 9x18mm Makarov variant with an integral sound suppressor.
  • Bizon-2-04: 9x18mm Makarov semi-automatic carbine model.
  • Bizon-2-05: 9x19mm Parabellum semi-automatic only model.
  • Bizon-2-06: Semi-automatic only carbine version in .380 ACP (9x17mm Short).
  • Bizon-2-07: Select-fire model chambered in 7.62x25mm Tokarev. This model dispenses with the Bizon's helical magazine and uses a conventional staggered-column 35-round steel magazine.

Bizon-3

A variant known as the Bizon-3 was also developed, and features a flip-up rear peep sight moved further to the rear on the receiver cover and a stock that folds up and over the receiver to lock into a spring-loaded latch on the receiver top cover. The weapon's barrel has an adapter for several types of muzzle devices. These are selected by the operator depending on the weapon's tactical employment and include sound suppressors, muzzle brakes, compensators and flash hiders.

Tupolev Tu-160 (Bomber)


The Tupolev Tu-160 (Russian: Туполев Ту-160, NATO reporting name: Blackjack) is a supersonic, variable-sweep wing heavy strategic bomber designed by the Tupolev Design Bureau in the Soviet Union. Although several civil and military transport aircraft are larger in overall dimensions, the Tu-160 is currently the world's largest combat aircraft, largest supersonic aircraft, and largest variable-sweep aircraft built. In addition, the Tu-160 has the heaviest takeoff weight of any combat aircraft.
Entering service in 1987, the Tu-160 was the last strategic bomber designed for the Soviet Union. The aircraft remains in limited production, with at least 16 aircraft currently in service with the Russian Air Force.  

Tu-160
Tupolev Tu-160
Role Supersonic strategic bomber and missile carrier
National origin Soviet Union, now Russia
Design group Tupolev
Built by Kazan Aircraft Production Association
First flight 18 December 1981
Introduction 1987 low rate initial production (LRIP); 2005 official
Status In production
Primary user Russian Air Force
Number built 35


Development
The first competition for a supersonic strategic heavy bomber was launched in the Soviet Union in 1967. The new bomber was to have a cruise speed of over Mach 3, in response to the American B-70 Valkyrie. It soon became apparent that such an aircraft would be too expensive and difficult to produce, so it was decided to reduce demands (in the US, the B-70 bomber project had already been cancelled).[citation needed]
In 1972, the Soviet Union launched a new multi-mission bomber competition to create a new supersonic, variable-geometry ("swing-wing") heavy bomber with a maximum speed of Mach 2.3, in direct response to the US Air Force B-1 bomber project. The Tupolev design, dubbed Aircraft 160M, with a lengthened flying wing layout and incorporating some elements of the Tu-144, competed against the Myasishchev M-18 and the Sukhoi T-4 designs.[1] Myasishchev's version, a variable-geometry aircraft, was considered to be the most successful. However, the Tupolev organization was regarded as having the greatest potential for completing this complex project and was assigned in 1973 the development of a new aircraft based on the Myasishchev design.

Tu-160 in flight.
Work on the new Soviet bomber continued despite an end to the B-1A, and in the same year, the design was accepted by the government committee. The prototype was photographed by an airline passenger at a Zhukovsky Airfield in November 1981, about a month before the aircraft's first flight on 18 December 1981. Production was authorized in 1984, beginning at Kazan Aircraft Production Association. Production of the aircraft, designated Tu-160 (factory designation "aircraft K" or "product 70"), was originally intended to total 100 aircraft, although only 35 have been produced, including three prototypes. The second prototype was lost in flight testing in 1987, the crew ejecting successfully.

Modernisation

In 2006, the Russian Air Force was expected to receive five modernised and one new-built Tu-160.[2] The Russian Air Force will receive a further five modernized Tu-160s each year, which means that modernization of the fleet could be achieved within three years if the schedule is kept up.[3]
Changes announced include completely digital, multireserved, neutron and other nuclear emissions resistant avionics; full support of cruising and steering through GLONASS global satellite positioning system; and updated version of NK-32 engines with increased reliability.[3] Weapon upgrades will allow the use of new nuclear/non-nuclear GLONASS-navigated cruise missiles (Kh-55),[4] and drop laser-guided bombs.[5] Planned upgrades are also to add the ability to handle missiles that launch military or civil satellites;[6] and addition of advanced radar emissions absorbing coatings.[7]

Design


Soviet officers in front of a Tu-160 in September 1989.

Vladimir Putin inside the cabin of a Tupolev Tu-160 in August 2005.
The Tu-160 is a variable-geometry wing aircraft, with sweep selectable from 20° to 65°. The aircraft employs a fly-by-wire control system with a blended wing profile and full-span slats are used on the leading edges, with double-slotted flaps on the trailing edges. The variable geometry gives conventional takeoff, and efficient subsonic cruise, while also permitting Mach 2 flight.
The Tu-160 is powered by four Kuznetsov NK-321 afterburning turbofan engines, the most powerful ever fitted to a combat aircraft. Unlike the American B-1B Lancer, which reduced the original Mach 2+ requirement for the B-1A to achieve a smaller radar profile, the Tu-160 retains variable intakes, and is capable of reaching Mach 2 speed at altitude. The NK-321 turbofans are efficient for subsonic cruise, but suboptimal for supersonic flight due to inlet drag.
The Tu-160 is equipped with a probe-and-drogue in-flight refueling system for extended-range missions, although it is rarely used. The Tu-160's internal fuel capacity of 130 tons gives the aircraft a roughly 15-hour flight endurance at a cruise speed of around 850 km/h (Mach 0.77, 530 mph) at 9,145 m (30,003 ft).[8] In February 2008, Tu-160 bombers and Il-78 refueling tankers practiced air refueling during air combat exercise, as well as Mig-31, A50 and other Russian combat aircrafts.[9]
Although the Tu-160 was designed for reduced detectability to both radar and infrared, it is not a stealth aircraft. Nevertheless, on 25 April 2006 Lt. Gen. Igor Khvorov claimed that Tu-160s managed to penetrate the US sector of the Arctic undetected, leading to a USAF investigation according to a Russian source.[10]
The Tu-160 has an Obzor-K attack radar in a slightly upturned dielectric radome, and a separate "Sopka" terrain-following radar, which provides fully automatic terrain-following flight at low altitude. The Tu-160 has an electro-optical bombsight. Its electronic warfare suite includes comprehensive active and passive ECM systems.
The Tu-160 has a crew of four (pilot, co-pilot, weapons systems officer and defensive systems operator) in K-36DM ejection seats. The pilot has a fighter-style control stick, but the flight instruments are traditional "steam gauge" dials. A crew rest area, a toilet, and a galley are provided for long flights. There is no HUD, nor are CRT multi-function displays provided in the original aircraft; however, plans for modernization of all Tu-160s were announced in 2003. They include a new digital flight control system, and the ability to carry new weapon types, such as new non-nuclear long-range cruise missiles.
Weapons are carried in two internal bays, each capable of holding 20,000 kg (44,400 lb) of free-fall weapons or a rotary launcher for nuclear missiles; additional missiles may also be carried externally. The aircraft's total weapons load capacity is 40,000 kg (88,185 lb).[11] However, no defensive weapons are provided; the Tu-160 is the first unarmed post-World War II Soviet bomber.
A demilitarized, commercial version of the Tu-160, named Tu-160SK, was displayed at Asian Aerospace in Singapore in 1994 with a model of a small space vehicle named Burlak attached underneath the fuselage. In 1995 Tupolev announced a partnership with the German firm OHB-System to produce the aircraft as a carrier for the launch vehicle; the German government subsequently withdrew funding in 1998.
While similar in appearance to the American B-1 Lancer, the Tu-160 is an entirely different class of combat aircraft, its primary role being a standoff missile platform (strategic missile carrier). The Tu-160 is also larger and faster than the B-1B and has a slightly greater combat range, though the B-1B has a larger combined payload and more modern avionics.[12] Another significant difference is that the colour scheme on the B-1B Lancer is usually radar-absorbant Black, the Tu-160 is painted with anti-flash white, giving it the nick-name among Russian Airforce soldiers "White Swan".

Operational history

The Tu-160 began service with the 184 Guards Bomber Regiment, based at Priluki, Soviet Union, in 1987.

Deployment

Squadron deployments to Long Range Aviation began in April 1987 before the Tu-160 was first presented to the public in a parade in 1989. In 1989 and 1990 it set 44 world speed flight records in its weight class. Until 1991, 19 aircraft served in the 184th Guards Heavy Bomber Regiment in Pryluky in the Ukrainian Soviet Socialist Republic, replacing Tu-16 and Tu-22M3 aircraft. In January 1992, Boris Yeltsin decided to discontinue production of the Tu-160. By this time, 35 aircraft had been built. In the same year, Russia unilaterally suspended its flights of strategic aviation in remote regions. After the fall of the Soviet Union, 19 of 35 aircraft became property of the newly-independent Ukraine, although in 1999 a deal between Russia and the Ukraine led to eight of those aircraft being turned over to Russia in exchange for a reduction in Ukraine's energy debts. Ukraine, which gave up nuclear weapons under the Nunn–Lugar Cooperative Threat Reduction Agreement, destroyed its other Blackjacks, except for one airframe retained for static display.
Russia's second Tu-160 unit, the 121st Guards Heavy Bomber Regiment based in Engels, was organised in 1992, but by 1994 it had received only six aircraft. Between 1999 and 2000 the eight former Ukrainian aircraft were assigned to the regiment, and another newly-built aircraft was assigned in 2000. By early 2001, in accordance with the START-2 Treaty, Russia has had 15 new-built Tu-160s, of which six were formerly missile-armed strategic bombers. One aircraft was lost during a test flight after engine repairs, on 18 September 2003.
There were 14 Tu-160s in service as of November 2005. Another two new-built aircraft are nearing completion at the Kazan Aircraft Plant, one of which was due to enter service in March 2006, with the other following later in the year. As of 2001, six additional Tu-160 have served as experimental aircraft at Zhukovski, four remaining airworthy.
On 30 December 2005, under an order signed by Russian President Vladimir Putin, the Tu-160 officially entered service in the Russian Air Force.
On 17 August 2007 Putin announced that Russia was resuming the strategic aviation flights stopped in 1991, sending its bomber aircraft on long-range patrols.[13] On 14 September 2007, British and Norwegian fighters intercepted two Tu-160s which breached NATO airspace near the UK and Finland.[14] On 25 December 2007, two Blackjacks came close to Danish airspace, and two Danish Air Force F-16 Fighting Falcons scrambled to intercept and identify them.[15]
According to Russian government sources, on 11 September 2007, a Tu-160 was used to drop the massive fuel-air explosive device, the Father of all bombs, for its first ever field test.[16] However, some military analysts expressed skepticism that the weapon was actually delivered by a Blackjack.[17]
On 28 December 2007, the first flight of a new Tu-160 was reported to have taken place following completion of the aircraft at the Kazan Aviation Plant.[18] After flight testing, the bomber joined the Russian Air Force on 29 April 2008, bringing the total number of aircraft in service to 16. One new Tu-160 is expected to be built every one to two years until the active inventory reaches 30 or more aircraft by 2025–30.[19][20]

TU-160, No. 02 "Vasily Reshetnikov" at the Engels airbase.
On 10 September 2008 two Russian Tu-160 landed in Venezuela as part of military maneuvers, announcing an unprecedented deployment to Russia's ally at a time of increasingly tense relations between Russia and the United States. The Russian Ministry of Defence said the two Tu-160 bombers were on a training mission. It said in a statement carried by Russian news agencies that the aircraft would conduct training flights over neutral waters before returning to Russia. Its spokesman added that the aircraft were escorted by NATO fighters as they flew across the Atlantic Ocean.[21]
On 12 October 2008 a number of Tu-160 bombers were involved in the largest Russian strategic bomber exercise since 1984. A total of 12 bombers including Tu-160 Blackjack and Tu-95 Bear conducted a series of launches of their cruise missiles. Some bombers launched a full complement of their missiles. It was the first time that a Tu-160 had ever fired a full complement of missiles.[22]
Pilots of the Tu-160 call it the “White Swan”, due to its maneuverability and anti-flash white finish.[23]
On 10 June 2010, two Tu-160 bombers carried out a record-breaking 23-hour patrol with a planned flight range of 18,000 kilometers. The bombers flew along the Russian borders and over neutral waters in the Arctic and Pacific Oceans.[24]

Trainer aircraft

No dedicated Tu-160 trainer version has yet appeared. Initially, pilot training was conducted using Tu-22M Backfire bombers, but these were soon replaced with a highly modified variant of the Tupolev Tu-134 airliner. Designated the Tu-134UBL, this unusual aircraft has had the nose and cockpit section of a Tu-160 grafted onto the aircraft's nose, giving students an unobstructed view from the simulated Tu-160 cockpit. In this arrangement the Tu-134UBL is reported to have flying characteristics similar to the Tu-160.[citation needed]

Variants

  • Tu-160: Production version.
Several variants have been proposed, but not built, including:
  • Tu-160S: designation used for serial Tu-160s when needed to separate them from all the pre-production and experimental aircraft.[25]
  • Tu-160V: liquid hydrogen fueled version (see also Tu-155).[25]
  • Tu-160 NK-74: upgraded (extended range) version with NK-74 engines.[25]
  • Tu-160M: a stretched bomber carrying two long-range, hypersonic Kh-90 (3M25 Meteorit-A) missiles.
  • Tu-160P (Tu-161): a very long-range escort fighter/interceptor.
  • Tu-160PP: an electronic warfare aircraft carrying stand-off jamming and ECM gear (Russian: ПП - постановщик помех).
  • Tu-160R: a strategic reconnaissance platform.
  • Tu-160SK: commercial version, designed to launch satellites within the "Burlak" (Russian: Бурлак, "hauler") system.[25]
  • Tu-170: a conventional bomber (conceived in order to avoid SALT-2 limits).

Operators

Current

 Russia
  • Russian Air Force: As of April 2008, 16 were in service, with the 121st Guards Heavy Bomber Regiment at Engels/Saratov.[26]

[edit] Former

 Ukraine
  • Ukrainian Air Force inherited 19 Tu-160s from the former Soviet Union, but subsequently handed over eight Tu-160s to Russia as exchange for debt relief in 1999; the remainder have been withdrawn from service.
 Soviet Union
184th Guards Heavy Bomber Regiment (TBAP), Priluki, Ukrainian SSR

Specifications (Tu-160)

Orthographic projection of the Tupolev Tu-160.
Data from Jane's All The World's Aircraft 2003–2004,[11]
General characteristics
  • Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
  • Length: 54.10 m (177 ft 6 in)
  • Wingspan:
    • Spread (20° sweep): 55.70 m (189 ft 9 in)
    • Swept (65° sweep): 35.60 m (116 ft 9¾ in)
  • Height: 13.10 m (43 ft 0 in)
  • Wing area:
    • Spread: 400 m² (4,306 ft²)
    • Swept: 360 m² (3,875 ft²)
  • Empty weight: 110,000 kg (242,505 lb)
  • Loaded weight: 267,600 kg (589,950 lb)
  • Max takeoff weight: 275,000 kg (606,260 lb)
  • Powerplant: 4 × Samara NK-321 turbofans
    • Dry thrust: 137.3 kN (30,865 lbf) each
    • Thrust with afterburner: 245 kN (55,115 lbf) each
Performance
  • Maximum speed: Mach 2.05 (2,220 km/h, 1,200 knots, 1,380 mph) at 12,200 m (40,000 ft)
  • Cruise speed: Mach 0.9 (960 km/h, 518 knots, 596 mph)
  • Range: 12,300 km (7,643 mi) practical range without in-flight refuelling, Mach 0.77 and carrying 6 × Kh-55SM dropped at mid range and 5% fuel reserves[27]
  • Combat radius: 7,300 km[28] (3,994 nmi, 4,536 mi) , 2,000 km (1,080 nmi, 1,240 mi) at Mach 1.5[11]
  • Service ceiling: 15,000 m (49,200 ft)
  • Rate of climb: 70 m/s (13,860 ft/min)
  • Wing loading: 742 kg/m² with wings fully swept (152 lb/ft²)
  • lift-to-drag: 18.5-19, while supersonic it is above 6.

Grumman B-2 Spirit (Bomber)

Northrop Grumman B-2 Spirit

B-2 Spirit
A USAF B-2 Spirit in flight
Role Stealth bomber
National origin United States
Manufacturer Northrop Corporation
Northrop Grumman
First flight 17 July 1989
Introduction April 1997
Status Active service: 20 aircraft
Primary user United States Air Force
Number built 21[1][2]
Program cost US$44.75 billion (through 2004)[3]
Unit cost $737 million (1997 cost for each aircraft, $1.01 billion today)[3][4]
The Northrop Grumman B-2 Spirit (also known as the Stealth Bomber) is an American heavy bomber with low observable stealth technology designed to penetrate dense anti-aircraft defenses and deploy both conventional and nuclear weapons. The bomber has a crew of two and can drop up to 80 500 lb (230 kg)-class JDAM GPS-guided bombs, or 16 2,400 lb (1,100 kg) B83 nuclear bombs. The B-2 is the only aircraft that can carry large air to surface standoff weapons in a stealth configuration.
Development originally started under the "Advanced Technology Bomber" (ATB) project during the Carter administration, and its performance was one of the reasons for his cancellation of the B-1 Lancer. ATB continued during the Reagan administration, but worries about delays in its introduction led to the reinstatement of the B-1 program as well. Program costs rose throughout development. Designed and manufactured by Northrop Grumman with assistance from Boeing, the cost of each aircraft averaged US$737 million in 1997 dollars).[3] Total procurement costs averaged $929 million per aircraft, which includes spare parts, equipment, retrofitting, and software support.[3] The total program cost, which includes development, engineering and testing, averaged $2.1 billion per aircraft in 1997.[3]
Because of its considerable capital and operational costs, the project was controversial in the U.S. Congress and among the Joint Chiefs of Staff. The winding-down of the Cold War in the later portion of the 1980s dramatically reduced the need for the aircraft, which was designed with the intention of penetrating Soviet airspace and attacking high-value targets. During the late 1980s and early 1990s, the Congress slashed initial plans to purchase 132 bombers to 21. In 2008 one bomber crashed just after takeoff and was destroyed as the crew ejected safely.[5] A total of 20 B-2s remain in service with the United States Air Force.
Though originally designed primarily as a nuclear bomber, the B-2 was first used in combat to drop conventional bombs on Serbia during the Kosovo War in 1999, and saw continued use during the wars in Iraq and Afghanistan.[6] B-2s were also used during the 2011 Libyan uprising.


Development

Origins

In the mid-1970s the search for a new US strategic bomber to replace the Boeing B-52 Stratofortress was underway, with nothing to show for it. First the North American XB-70 Valkyrie and then the Rockwell B-1 Lancer both became obsolete before entering service, and were canceled after only small numbers had been built. The B-70 was intended to fly above and beyond defensive interceptor aircraft, only to find these same attributes made it especially vulnerable to surface-to-air missiles (SAMs). The B-1 attempted to avoid SAMs by flying close to the ground to mask their radars behind terrain, only to face a new generation of interceptors with look-down/shoot-down capabilities that could attack them from above.
However, technology continued to progress throughout. By the mid-1970s it was becoming clear that there was an entirely different way to avoid missiles and intercepts. Known today as "stealth", the idea was to build an aircraft with an airframe that deflected or absorbed radar signals so that too little was reflected back to the radar unit. An aircraft that was stealthy enough would be able to fly wherever it pleased, and could be attacked only by weapons and systems that did not rely on radar. Although such possibilities exist, notably human observers, ranges were so short that most aircraft could fly right by the defence with impunity, especially at night.[8]
In 1974 DARPA requested information from US aviation firms about the largest radar cross section of an aircraft where it would remain effectively invisible to radars.[9] Initially, Northrop and McDonnell Douglas were selected for further work. Lockheed had experience in this field due to their work on the Lockheed SR-71, which included a number of stealthy features, notably its canted vertical stabilizers, the use of composite materials in key locations, and the overall finish in radar absorbing paint. A key improvement was the introduction of computer models that could be used to predict the reflections from flat surfaces and could be used to design a "faceted" aircraft. Work on the first such designs had started in 1975 with "the hopeless diamond", a model built at Lockheed to test the concepts.[10] Improvements quickly followed that allowed designs with more traditional layouts and construction techniques.
These plans were well advanced by the summer of 1975, when DARPA started the Experimental Survivability Testbed (XST) project. Northrop and Lockheed won the first round of testing, and Lockheed was the sole winner of the second round in April 1976. This led to the Have Blue program.[11]

ATB program

By 1976 these programs had advanced to the point where the concept of a long-range strategic stealth bomber appeared to be a safe bet. Whereas the B-1 relied on flying around known defense sites and could only change its mission within a limited selection of pre-selected routes, a stealth bomber would be able to overfly the Soviet Union with impunity, allowing it to loiter and hunt for targets instead of simply running in and out as fast as possible. In a nuclear exchange, this would allow it to wait out the initial attacks and find targets that escape destruction, eliminating the "overkill" that was built into existing war planning. Better yet, as the need for high speed was reduced or eliminated, and all of the extremely expensive electronic warfare equipment removed, the aircraft would be much simpler and less expensive.
Carter was aware of these developments during 1977, and it appears to have been one of the major reasons the B-1 was canceled.[12] Further studies were ordered in early 1978, by which point the Have Blue platform had flown and proven the concepts. During the 1980 presidential election in 1979, Ronald Reagan repeatedly complained that Carter was weak on defence, and used the B-1 as a prime example. In return, on 22 August 1980, the Carter administration publicly disclosed that the United States Department of Defense (DoD) was working to develop stealth aircraft, including a bomber.[13]
The Advanced Technology Bomber (ATB) began in 1979.[14] Full development of the black project followed. The black program was funded under the code name "Aurora".[15] After the evaluations of the companies' proposals, the ATB competition was reduced to the Northrop/Boeing and Lockheed/Rockwell teams with each receiving a study contract for further work.[14] Both teams used flying wing designs.[15] Northrop had previous experience from the development of the YB-35 and YB-49 flying wing aircraft.[16] The Northrop design was larger while the Lockheed design included a small tail.[15]
Front view of tailless aircraft parked in front of building. On the building face is a blue and red rectangular flag. In the foreground is a star shape on the ground
The B-2's first public display in 1988
The Northrop/Boeing team's ATB design was selected over the Lockheed/Rockwell design on 20 October 1981.[14][17] The Northrop design received the designation B-2 and the name "Spirit". The bomber's design was changed in the mid-1980s when the 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 US$1 billion to the program's cost.[13] An estimated US$23 billion was secretly spent for research and development on the B-2 by 1989.[18]
The B-2 was first publicly displayed on 22 November 1988, at Air Force Plant 42, Palmdale, California, where it was assembled. This initial viewing was heavily guarded and guests were not allowed to see the rear of the B-2. However, Aviation Week editors found that there was no ban on overflying the airfield apron/presentation area and, to the chagrin of the USAF, took pictures from above of the aircraft's then-secret planform and suppressed engine exhausts. The B-2's first public flight was on 17 July 1989 from Palmdale.[19] At the program's peak, approximately 13,000 people were employed at a dedicated plant in Pico Rivera, California for the aircraft's engineering and portions of its manufacturing.[20]
Top view of triangular aircraft, with sawtooth trailing edge, in flight over desert
The B-2's first public flight in 1989

Espionage

In 1984, a Northrop employee, Thomas Cavanaugh, was arrested for attempting to sell classified information to the Soviet Union, which apparently was smuggled out of the Pico Rivera, California factory.[21] Cavanaugh was eventually sentenced to life in prison and released on parole in 2001.
Noshir Gowadia, a design engineer who worked on the B-2's propulsion system, was arrested in October 2005 for selling B-2 related classified information to foreign countries.[22] On 9 August 2010, Gowadia was convicted in the United States District Court for the District of Hawaii on 14 of 17 charges against him.[23] On 24 January 2011, Gowadia was sentenced to 32 years in prison.[24]

Program costs and procurement

A procurement of 132 aircraft was planned in the mid-1980s, but was later reduced to 75.[25] By the early 1990s, the Soviet Union had disintegrated, which effectively eliminated the Spirit's primary Cold War mission. Under budgetary pressures and congressional opposition, in his 1992 State of the Union Address, President George H.W. Bush announced B-2 production would be limited to 20 aircraft.[26] In 1996, however, the Clinton administration, though originally committed to ending production of the bombers at 20 aircraft, authorized the conversion of a 21st bomber, a prototype test model, to Block 30 fully operational status at a cost of nearly $500 million.[27]
In 1995, Northrop made a proposal to the USAF to build 20 additional aircraft with a flyaway cost of $566 million each.[28]
The program was the subject of public controversy for its costs to American taxpayers. In 1996, the General Accounting Office disclosed that the USAF's B-2 bombers "will be, by far, the most costly bombers to operate on a per aircraft basis", costing over three times as much as the B-1B (US$9.6 million annually) and over four times as much as the B-52H ($US6.8 million annually). In September 1997, each hour of B-2 flight necessitated 119 hours of maintenance in turn. Comparable maintenance needs for the B-52 and the B-1B are 53 and 60 hours respectively for each hour of flight. A key reason for this cost is the provision of air-conditioned hangars large enough for the bomber's 172 ft (52.4 m) wingspan, which are needed to maintain the aircraft's stealthy properties, especially its "low-observable" stealthy skins.[29][30] Maintenance costs are about $3.4 million a month for each aircraft.[31]
In a 1994 live fire exercise near Point Mugu, California, a B-2 drops forty-seven 500 lb (230 kg) class Mark 82 bombs, which is more than half of a B-2's total ordnance payload
The total "military construction" cost related to the program was projected to be US$553.6 million in 1997 dollars. The cost to procure each B-2 was US$737 million in 1997 dollars, based only on a fleet cost of US$15.48 billion.[3] The procurement cost per aircraft as detailed in General Accounting Office (GAO) reports, which include spare parts and software support, was $929 million per aircraft in 1997 dollars.[3]
The total program cost projected through 2004 was US$44.75 billion in 1997 dollars. This includes development, procurement, facilities, construction, and spare parts. The total program cost averaged US$2.13 billion per aircraft.[3]

Opposition

In its consideration of the fiscal year 1990 defense budget, the House Armed Services Committee trimmed $800 million from the B-2 research and development budget, while at the same time staving off a motion to kill the bomber. Opposition in committee and in Congress as mostly broad and bipartisan, with Congressmen Ron Dellums (D-CA), John Kasich (R-OH), and John G. Rowland (R-CT) authorizing the motion to kill the bomber and others in the Senate such as Jim Exon (D-NE) and John McCain (R-AZ) also opposing the project.[32]
The growing cost of the B-2 program, and evidence of flaws in the aircraft's ability to elude detection by radar,[32] were among factors that drove opposition. At the peak production period specified in 1989, the schedule called for spending US$7 billion to $8 billion per year in 1989 dollars, something Committee Chair Les Aspin (D-WI) said "won't fly financially."[33]
In 1990, the Department of Defense accused Northrop of using faulty components in the flight control system. Efforts have also been made to reduce the probability of bird ingestion, which could damage engine fan blades.[34]
In time, a number of prominent members of Congress began to oppose the program's expansion, including former Democratic presidential nominee John Kerry, who cast votes against the B-2 in 1989, 1991 and 1992 while a US Senator representing Massachusetts. By 1992, Republican President George H.W. Bush called for the cancellation of the B-2 and promised to cut military spending by 30% in the wake of the collapse of the Soviet Union.[35]
In May 1995, on the basis of its 1995 Heavy Bomber Force Study, the DOD determined that additional B-2 procurements would exacerbate efforts to develop and implement long term recapitalization plans for the U.S. Air Force bomber force.
In October 1995, former Chief of Staff of the United States Air Force, General Mike Ryan, and Former Chairman of the Joint Chiefs of Staff, General John Shalikashvili, strongly recommended against Congressional action to fund the purchase of any additional B-2s, arguing that to do so would require unacceptable cuts in existing conventional and nuclear-capable aircraft to pay for the new bombers,[36] and because the military had much higher priorities on which to spend its limited procurement dollars.[37]
Some B-2 advocates argued that procuring twenty additional aircraft would save money because B-2s would be able to deeply penetrate anti-aircraft defenses and use low-cost, short-range attack weapons rather than expensive standoff weapons. However, in 1995, the Congressional Budget Office (CBO), and its Director of National Security Analysis, found that additional B-2s would reduce the cost of weapons expended by the bomber force by less than US$2 billion in 1995 dollars during the first two weeks of a conflict, which is when the Air Force envisions bombers would make their greatest contribution. This is a small fraction of the US$26.8 billion (in 1995 dollars) life cycle cost that the CBO projected an additional 20 B-2s would cost.[38]
In 1997, as Ranking Member of the House Armed Services Committee and National Security Committee, Congressman Ron Dellums (D-CA), a long-time opponent of the bomber, cited five independent studies and offered an amendment to that year's defense authorization bill to cap production of the bombers to the existing 21 aircraft. The amendment was narrowly defeated.[39] Nonetheless, Congress did not approve funding for the purchase of any additional B-2 bombers.

Upgrades

A number of upgrade packages were applied to the B-2 during the 21st century. In 2004, Northrop Grumman tested a new alternate high-frequency material (AHFM) for use as a RAM coating for the B-2.[40] The Air Force Research Laboratory has developed a new material to be used on the part of the wing trailing edge that is subject to engine exhaust to replace the current material that degrades.[41] In 2008, the US Congress funded upgrades to the B-2's weapon control systems for hitting moving targets.[42]
In July 2008, the B-2's computing architecture was redesigned with a new integrated processing unit (IPU) that communicates via a fiber optic network and a smaller, faster single-board processor that runs a new version of the operational flight program (OFP) software converted from JOVIAL to C by automated tools.[43][44]
On 29 December 2008, Air Force officials awarded a production contract to Northrop Grumman to modernize the B-2 fleet's radars. The contract provides advanced radar components, with the aim of sustained operational viability of the B-2 fleet into the future. The contract has a target value of some US$468 million.[45] The award follows successful flight testing with the upgraded equipment. A modification to the radar was needed since the US Department of Commerce required the B-2 to use a different radar frequency.[46] It was reported on 22 July 2009 that the B-2 had passed the second of the two USAF audit milestones associated with this upgraded AESA radar capability.[47]
On 28 April 2009, an Air Force/contractor team verified that the 30,000 lb (14,000 kg) Massive Ordnance Penetrator (MOP) would fit in the B-2's bomb bay.[48]

Future developments

The Pentagon is currently (as of 2011) evaluating a radically different unmanned stealth bomber, characterized as a "mini-B2", to come into operational service by 2020.[49] During a transition period, US political expert Rebecca Grant has posited when the B-2 is no longer able to penetrate enemy defenses, the Lockheed Martin F-35 Lightning II may take on its strike/interdiction role. The F-35 also carries the B61 nuclear bomb as a tactical bomber and is not covered by strategic arms limitation treaties such as New START.[50]

Design

The B-2's engines are buried within its wing to conceal the induction fans and minimize their exhaust signature. The crew of two sit side-by-side in the cockpit.
The B-2's low-observable, or "stealth", characteristics give it the ability to penetrate an enemy's most sophisticated anti-aircraft defenses to attack its most heavily defended targets. The bomber's stealth comes from a combination of reduced acoustic, infrared, visual and radar signatures, making it difficult for opposition defenses to detect, track and engage the aircraft. Many specific aspects of the low-observability process remain classified. The B-2's composite materials, special coatings and flying wing design, which reduces the number of leading edges, contribute to its stealth characteristics.[51] The Spirit has a radar signature of about 0.1 m2.[52] Each B-2 requires a climate-controlled hangar large enough for its 172-foot (52 m) wingspan to protect the operational integrity of its sophisticated radar absorbent material and coatings.[53] The engines are buried within the wing to conceal the induction fans and hide their exhaust.[54]
The blending of low-observable technologies with high aerodynamic efficiency and large payload gives the B-2 significant advantages over previous bombers. The U.S. Air Force reports its range as approximately 6,000 nautical miles (6,900 mi; 11,000 km).[6][55] Also, its low-observation ability provides the B-2 greater freedom of action at high altitudes, thus increasing its range and providing a better field of view for the aircraft's sensors. It combines GPS Aided Targeting System (GATS) with GPS-aided bombs such as Joint Direct Attack Munition (JDAM). This uses its passive electronically scanned array APQ-181 radar to correct GPS errors of targets and gain much better than laser-guided weapon accuracy when "unguided" gravity bombs are equipped with a GPS-aided "smart" guidance tail kit. It can bomb 16 targets in a single pass when equipped with 1,000 or 2,000-pound (450 kg or 900 kg) bombs, or as many as 80 when carrying 500 lb (230 kg) bombs.
Former Vice President Dick Cheney sits inside the cockpit of a B-2 with pilot Capt. Luke Jayne during a visit to Whiteman AFB in 2006.
The B-2 has a crew of two: a pilot in the left seat, and mission commander in the right.[6] The B-2 has provisions for a third crew member if needed.[56] For comparison, the B-1B has a crew of four and the B-52 has a crew of five.[6] B-2 crews have been used to pioneer sleep cycle research to improve crew performance on long sorties. The B-2 is highly automated, and, unlike two-seat fighters, one crew member can sleep, use a toilet or prepare a hot meal while the other monitors the aircraft.[57]
As with the Boeing B-52 Stratofortress and Rockwell B-1 Lancer, the B-2 provides the versatility inherent in manned bombers. Like other bombers, its assigned targets can be canceled or changed while in flight, the particular weapon assigned to a target can be changed, and the timing of attack, or the route to the target can be changed while in flight.
A B-2 during aerial refueling which extends its range past 6,000 miles (9,700 km) to support intercontinental sorties.
The prime contractor, responsible for overall system design, integration and support, is Northrop Grumman. Boeing, Raytheon (formerly Hughes Aircraft), G.E. and Vought Aircraft Industries, are subcontractors.
The original B-2 design had tanks for a contrail-inhibiting chemical, but this was replaced in the final design with a contrail sensor from Ophir that alerts the pilot when he should change altitude.[58] Mission planning also considers altitudes where the probability of contrail formation is minimized.

Operational history

The first operational aircraft, christened Spirit of Missouri, was delivered to Whiteman Air Force Base, Missouri, where the fleet is based, on 17 December 1993.[59] The B-2 reached initial operational capability (IOC) on 1 January 1997.[60] Depot maintenance for the B-2 is accomplished by U.S. Air Force contractor support and managed at Oklahoma City Air Logistics Center at Tinker Air Force Base.[6] Originally designed to deliver nuclear weapons, modern usage has shifted towards a flexible role with conventional and nuclear capability.

Into combat

An Air Force maintenance crew services a B-2 at Andersen AFB, Guam, 2004
The B-2 has seen service in four campaigns. Its combat debut was during the Kosovo War in 1999. It was responsible for destroying 33% of selected Serbian bombing targets in the first eight weeks of U.S. involvement in the War.[6] During this war, B-2s flew non-stop to Kosovo from their home base in Missouri and back.[6] The B-2 was the first aircraft to deploy GPS satellite guided JDAM "smart bombs" in combat use in Kosovo.[61]
B-2 Spirit.ogv
B-2 Spirit U.S. Air Force video
The B-2 has been used to drop bombs on Afghanistan in support of the Operation Enduring Freedom. With the support of aerial refueling, the B-2 flew one of its longest missions to date from Whiteman Air Force Base, Missouri to Afghanistan and back.[6]
The B-2's combat use preceded a U.S. Air Force declaration of "full operational capability" in December 2003.[6] The Pentagon's Operational Test and Evaluation 2003 Annual Report noted that the B-2's serviceability for Fiscal Year 2003 was still inadequate, mainly due to the maintainability of the B-2's low observable coatings. The evaluation also noted that the Defensive Avionics suite also had shortcomings with "pop-up threats".[6]
During the Iraq War (Operation Iraqi Freedom), B-2s operated from Diego Garcia and an undisclosed "forward operating location". Other sorties in Iraq have launched from Whiteman AFB.[6] This resulted in missions lasting over 30 hours and one mission of over 50 hours. "Forward operating locations" have been previously designated as Andersen Air Force Base in Guam and RAF Fairford in the UK, where new climate controlled hangars have been constructed. B-2s have conducted 27 sorties from Whiteman AFB and 22 sorties from a forward operating location, releasing more than 1.5 million pounds of munitions,[6] including 583 JDAM "smart bombs" in 2003.[62]
All B-2s, nuclear-capable B-52s, and nuclear intercontinental ballistic missiles have shifted to the nuclear-focused Air Force Global Strike Command set up on September 2009.[63][64]
In March 2011, B-2s were the first US aircraft into action in Operation Odyssey Dawn, the UN mandated enforcement of the Libyan no-fly zone. Three B-2s dropped 40 bombs on a Libyan airfield in support of the UN no-fly zone.[65]

Operators

The "Spirit of Indiana" sits on the ramp at Andersen AFB in Guam on 23 June 2006
B-2s are operated exclusively by the United States Air Force active units.

Accident

The crashed B-2
On 23 February 2008, the B-2 Spirit of Kansas, 89-0127 crashed on the runway shortly after takeoff from Andersen Air Force Base in Guam.[67] B-2 89-0127 had been operated by the 393rd Bomb Squadron, 509th Bomb Wing, Whiteman Air Force Base, Missouri, and had logged 5,176 flight hours. It was the first crash of a B-2. The two person crew ejected safely from the aircraft and survived the crash. The aircraft was completely destroyed, a hull loss valued at US$1.4 billion.[68][69] After the accident, the Air Force took the B-2 fleet off operational status until clearing the fleet for flight status 53 days later on 15 April 2008.[70] The cause of the crash was later determined to be moisture in the aircraft's Port Transducer Units during air data calibration, which distorted the information being sent to the bomber's air data system. As a result, the flight control computers calculated an inaccurate airspeed, and a negative angle of attack, causing the aircraft to pitch upward 30 degrees during takeoff.[71]

Aircraft on display

Mockup of a B-2 Spirit on display at the National Museum of the United States Air Force
Because of its high cost, strategic bombing role, and the still-classified aspects of its low observable coatings, no production B-2 has been placed on permanent display. However, B-2s have made periodic appearances on ground display at various air shows.
  • B-2 test article (s/n AT-1000), the second of two built without engines or instruments for static testing, was placed on display in 2004 at the National Museum of the United States Air Force near Dayton, Ohio.[72] The test article passed all structural testing requirements before the airframe failed.[73] The Museum's restoration team spent over a year reassembling the fractured airframe. The display airframe is marked to resemble The Spirit of Ohio (S/N 82-1070), the B-2 used to test the design's ability to withstand extreme heat and cold.[72] The exhibit features the actual Spirit of Ohio nose wheel door, with its distinctive Fire and Ice artwork, which was painted and signed by the technicians who performed the temperature testing.[72] The restored test aircraft is on display in the museum's "Cold War Gallery".[74]
  • From 1989 to 2004, the South Dakota Air and Space Museum located on the grounds of Ellsworth Air Force Base displayed the 10-short-ton (9-metric-ton) "Honda- Stealth", a 60% scale mock-up of a stealthy bomber which had been built by North American Honda in 1988 for an advertising campaign.[75] Although not an actual replica of a B-2, the mock-up was close enough to the B-2's design to arouse suspicion that Honda had intercepted classified, top secret information, as the B-2 project was still officially classified in 1988. Honda donated the model to the museum in 1989, on condition that the model be destroyed if it was ever replaced with a different example. In 2005, when the museum received a B-1 Lancer for display (Ellsworth being a B-1 base), the museum destroyed the mock-up.[76][77]

Specifications (B-2A Block 30)

Orthographically projected diagram of the B-2 Spirit
Data from USAF Fact Sheet,[6] Pace,[78] Spick,[55] Globalsecurity[79]
General characteristics
Performance
Armament
  • 2 internal bays for 50,000 lb (23,000 kg) of ordnance.[55]
  • 80× 500 lb class bombs (Mk-82) mounted on Bomb Rack Assembly (BRA)
  • 36× 750 lb CBU class bombs on BRA
  • 16× 2000 lb class weapons (Mk-84, JDAM-84, JDAM-102) mounted on Rotary Launcher Assembly (RLA)
  • 16× B61 or B83 nuclear weapons on RLA
Later avionics and equipment improvements allow B-2A to carry JSOW, GBU-28, and GBU-57A/Bs as well. The Spirit is also designated as a delivery aircraft for the AGM-158 JASSM when the missile enters service.

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