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Mikoyan-Gurevich MiG-15 "Fagot"

The MiG-15 was a jet fighter developed after World War II by the Soviets. It first saw action in the Korean War from 1950-1953, fighting against the F-86 Sabre. One thing peculiar is that both of the jets look very much the same, and the reason might be that the U.S. and Russia were looking at the same blue prints of the German jet designs.

An F-86 Sabre.

A MiG-15 "Fagot".

Design...

The Fagot was one of the first jet planes to have swept wings as German research in World War II proved that piston-engined fighters with ninety-degree wings limited their high-speed performance. There were many claims that Artem Mikoyan and Mikhail Gurevich were heavily influenced by the Folke-Wulf Ta-183, but these claims were discredited as most of the Folke-Wulf engineers were captured by the West and the MiG-15 differ significantly in structure and general design with the Ta-183. Currently, most sources acknowledge that the MiG-15 is an orginal Svoiet design only benefiting from German research.

By 1946, there was increasing problems for the Soviet engineers to perfect the German HeS-011 axial-flow jet engine, making it almost impossible to power the MiG-15. There were also new airframe designs from Mikoyan-Gurevich which threatened to outstrip development of the engines to power them. Soviet aviation ministers approached the Soviet Premier Joseph Stalin with suggestions to buy advanced jet engines from the British. Stalin is said to have replied, "What fool will us his secrets?"

The proposal was, however, approved and engine designers, such as Vladimir Klimov, travelled to the UK to request the engines. To their shock and amazement, the British agreed and they were provided technical information and license to manufacture the Rolls Royce Nene, which was reverse-engineered and produced as the Klimov RD-45, which subsuquently used to power the MiG-15. Rolls Royce, however, was not able to claim £207 million in license fees from the USSR.

Operational History...

The Fagot has seen action throughout the entire Cold War, having confrontations with NATO aircraft and ending up either getting shot down, or shooting down the enemy. And as time went by, MiG-15 aces emerged from the many Soviet pilots, one of them, Yevgeny Pepelyayev having a total of 19 kills.

The MiG-15 first appeared in the Korean War, where it was greatly mistaken as the F-86 Sabre by US Forces due to their remarkable similarity. Many thought they were being attacked by their own people.

MiG-15s also participated in the 1956 Suez Canal Crisis under Egyptian pilots.

Defection...

The first detailed examination of the MiG-15 was capable due to a defection by a North Korean traitor, Lieutenant No Kum-Sok. The U.S., at that time, was offering a US $100 000 (a huge amount back then) reward to any pilot who defected with a MiG-15, and No Kum-Sok recieved every cent of it. However, Lieutenant No Kum-Sok claimed he was not aware of the reward when he decided to defect. The MiG-15 was inspected thoroughly and test flown by several test pilots, as well as Chuck Yeager, the first man to survive breaking the sound barrier. Lieutenant No's aircraft is not in display in the National Museum of United States Air Force.

Specifications...

Generael Characteristics

Crew: MiG-15bis=1, MiG-15UTI=2
Length: 10.11 m (33 ft 2 in)
Wingspan: 10.08 m (33 ft 1 in)
Height: 3.70 m (12 ft 2 in)
Wing area: 20.6 m² (221.74 ft²)
Airfoil: TsAGI S-10 / TsAGI SR-3
Empty weight: 3,580 kg (7,900 lb)
Loaded weight: 4,960 kg (10,935 lb)
Max takeoff weight: 6,105 kg (13,460 lb)
Fuel capacity: 1,400 L (364 US gal)
Powerplant: 1× Klimov VK-1 turbojet, 26.5 kN (5,950 lbf)

Performance

Maximum speed: 1,075 km/h (668 mph)
Cruise speed: 840 km/h (520 mph)
Range: 1,200 km, 1,975 km with external tanks (745 mi / 1,225 mi)
Service ceiling: 15,500 m (50,850 ft)
Rate of climb: 50 m/s (9,840 ft/min)
Wing loading: 240.8 kg/m² (49.3 lb/ft²)
Thrust/weight: 0.54

Armament

2x 23mm cannons, 23x115mm, (80 rounds per gun ,160 rounds total), and 1x 37 mm cannon (40 rounds total)
Note: All bullets were armor piercing and highly explosive

2x 100 kg (220 lb) bombs, drop tanks, or unguided rockets on underwing hardpoints.

Rockwell B-1 Lancer- History

Debut of the first B-1B outside of a hangar in Palmdale, California, 1984. For the full description page, click here.

History...

The B-1 was conceived as the Advanced Manned Strategic Aircraft (AMSA) program circa 1965. AMSA was the last in a series of programs through the 1960s that looked at replacing the B-52 Stratofortress with a multi-role supersonic aircraft capable of long-range bombing and missile launching with nuclear weapons. A series of cancellations led to its service introduction being greatly delayed, until the later half of the 1980s, over twenty years after the program first started.

1. The B-70 Valkyrie

In 1955, the USAF released system requirements for a heavy bomber with the B-52's range and payload capabilities, and the supersonic speed of the B-58, in order to replace both of these bombers by 1965. The initial requirements called for a Mach 0.9 cruise speed with a Mach 2+ dash capability. The designs that met this specification were considered unrealistically large, requiring new hangars to hold them and reinforced runways to launch them.

During the design phase new fuels and techniques evolved that would allow an aircraft with similar range to cruise all the way to its target at high speeds. The Air Force asked for new proposals based on these advances, and this work would eventually lead to the B-70 Valkyrie. The Valkyrie was a large six-engine bomber designed to fly at very high altitudes at Mach 3 to avoid defending interceptors, the only effective anti-bomber weapon at that time. Altitude alone was proving so difficult a problem that Soviet interceptors continued to fail to intercept the Lockheed U-2, running out of fuel before reaching a suitable firing point. Given the speed and altitude of the B-70, the defense would have only a few minutes to respond to an attack, and even small numbers of B-70s attacking simultaneously would ensure that most would fly right by the interceptors, regardless of how much warning time they had.

The introduction of effective anti-aircraft missiles rendered this mode of operation dangerous. Unlike a manned interceptor that maneuvers within a plane while climbing, missiles flew straight up and could reach the B-70s altitude in a few minutes. The only concern became speed; as long as the target did not fly out of range before the missile reached it an attack was possible, and a powerful radar giving the operators some "lead time" could easily solve this problem. This was proven in convincing fashion by the downing of Gary Powers' U-2 in 1960.

2. Redefined Role

In response to the missile threat, military planners switched to low-altitude penetration. By carefully selecting the line of approach to a target, and routing the flight path around known anti-aircraft sites, the radar's line-of-sight operation worked in the bomber's advantage by hiding it from view below the landscape. Aircraft speed became much less important. The targets themselves often had defenses located nearby to prevent this sort of approach all the way in, but stand-off weapons such as cruise missiles and the AGM-69 SRAM provided an attack capability from outside of the defensive missile's range. Low-altitude flight also made the bombers very difficult to detect from aircraft at higher altitudes, including interceptors, as radar systems of that generation could not "look down" due to the clutter that resulted from ground reflections.

Operations at low levels would limit the B-70 to subsonic speed, while dramatically decreasing its range due to much higher fuel requirements. The result would be an aircraft with similar speed but much less range than the B-52 it would have replaced. This was not a purely theoretical issue, this exact problem had actually occurred with the B-58, another high-speed aircraft that was forced into the low-level role to avoid missile defenses. The design had "spent" a lot in gaining medium-range Mach 2 performance, but at low altitudes it had strictly subsonic performance and such dramatically reduced range that it limited the selection of targets that could be assigned to it. The "outdated" B-52 outperformed it, as it would have the B-70.

Unsuited for this new role, the viability of the B-70 as a bomber was questioned. Citing high cost, a growing ICBM force, and poor survivability against missiles, the operational fleet was canceled in 1961 by President John F. Kennedy, and the program was changed to a supersonic research program.

3. AMSA

The first such study was known as the Subsonic Low Altitude Bomber (SLAB), which was completed in 1961. This was followed by the similar Extended Range Strike Aircraft (ERSA), which added a Variable-sweep wing planform, something then very much in vogue in the aviation industry. ERSA envisioned a relatively small aircraft with a 10,000 lb (4,500 kg) load and a range of 8,750 nautical miles (16,200 km), with 2,500 nmi (4,600 km) being flown at low altitudes. In August 1963 the similar Low-Altitude Manned Penetrator (LAMP) design was completed, which called for an aircraft with a 20,000 lb (9,000 kg) load and somewhat shorter range of 7,150 nautical miles (13,200 km).

These all culminated in the October 1963 Advanced Manned Precision Strike System (AMPSS), which led to industry studies at Boeing, General Dynamics, and North American. In mid-1964, the USAF had revised its requirements and retitled the project as Advanced Manned Strategic Aircraft (AMSA), which differed from AMPSS primarily in that it also demanded a high-speed high-altitude capability, albeit slower than the Valkyrie at about Mach 2. Rockwell engineers joked that the new name actually stood for "America's Most Studied Aircraft", given the lengthy series of design studies.

However, the A.M.S>A. project was cancelled by opposition from many high-ranked staff who preferred I.C.B.M. (Intercontinental Ballistic Missile) over long-range bombers.

4. B-1A Program



The B-1A in flight showing its underside. For the full description page, click here.

President Richard Nixon re-established the program after taking office, in keeping with his flexible response strategy that required a broad range of options short of general nuclear war. Secretary of Defense Melvin Laird reviewed the programs and decided to lower the numbers of FB-111s claiming it lacked the required range, and recommended that the AMSA design studies be accelerated. In April 1969 the program officially became the B-1A. This was the first entry in the new bomber designation series, first created in 1962.

Rockwell's design featured a number of features common to 1960s U.S. designs. These included the use of variable-sweep wings in order to provide both high lift during takeoff and landing, and low drag during a high-speed dash phase. With the wings set to their widest position the aircraft had considerably better lift and power than the B-52, allowing it to operate from a much wider variety of bases. Penetration of the U.S.S.R.'s defenses would take place in a dash, crossing them as quickly as possible before entering into the less defended "heartland" where speeds could be reduced again. The large size and fuel capacity of the design would allow this dash portion of the flight to be relatively long.

In order to achieve the required Mach 2 performance at high altitudes, the air intake inlets were variable. In addition, the exhaust nozzles were fully variable. Initially, it had been expected that a Mach 1.2 performance could be achieved at low altitude, which required that titanium be used in critical areas in the fuselage and wing structure. However, this low altitude performance requirement was lowered to only Mach 0.85, reducing the amount of titanium, and the overall cost.

Overall it had a range similar to that of the B-52, although more of the flight could be low-level. A combination of flying lower due to better navigation systems and a greatly reduced radar cross section made it much safer from attack by missiles, and the latter also improved its odds against fighters as well. In situations where fighters were the expected competition (i.e. outside the USSR), its high-speed dash was a potentially useful technique the B-52 could not match. A convincing B-52 replacement had arrived.

5. Another cancellation

When Carter took office in 1977 he ordered a review of the entire program. By this point the projected cost of the program had risen to over $100 million per aircraft, although this was lifetime cost over 20 years. He was informed of the relatively new work on stealth aircraft that had started in 1975, and decided that this was a far better avenue of approach than the B-1. Pentagon officials also stated that the ALCM launched from the existing B-52 fleet would give the USAF equal capability of penetrating Soviet airspace. With a 1,500 statute mile (2,400 km) range, the ALCM could be launched well outside the range of any Soviet defenses, and penetrate at low altitude just like a bomber, but in much greater numbers. A small number of B-52 operating outside interception range could launch hundreds of ALCMs, saturating the defense. A program to improve the B-52 and develop and deploy the ALCM would cost perhaps 20% of the price to deploy the planned 244 B-1A's.

On June 30th, 1977 Carter announced that the B-1A would be cancelled in favor of ICBMs, SLBMs, and a fleet of modernized B-52s armed with ALCMs. Carter called it "one of the most difficult decisions that I've made since I've been in office." No mention of the stealth work was made public, the program being top secret, but today it is known that he authorized the Advanced Technology Bomber (ATB) project in early 1978, which eventually led to the B-2 Spirit.

Flight tests of the four B-1A prototypes for the B-1A program continued through April 1981. The program included 70 flights totalling 378 hours. A top speed of Mach 2.22 was reached by the second B-1A. Engine testing also continued during this time with the YF101 engines totalling almost 7,600 hours.

6. Shifting priorities

It was during this period that the Soviets, also acting in proxy through Cuba, started to exert themselves in several new theaters of action, in particular the Cuban support in Angola starting in 1975 and the Soviet invasion of Afghanistan in 1979. The U.S. strategy to this point was containment and a conventional and nuclear war in Europe, which almost all military planning had been focused on. These newer actions revealed that the military was simply incapable of supporting any sort of effort outside these narrow confines.

The Army responded by accelerating its Rapid Deployment Force concept, but suffered from major problems with airlift and sealift capability. While gaming a USSR-led invasion of Iran from Afghanistan, then considered (incorrectly) to be a major Soviet goal, it was discovered that only small numbers of units could be in the field in anything close to a week. In order to slow an advance while this happened they relied on air power, but critically the Iran-Afghanistan border was outside the U.S. Navy's range, leaving this role to the Air Force. They, in turn, had limited capability to offer ground support in many areas that were outside of the range of friendly airbases. Although the B-52 had the range to support on-demand global missions, the B-52's long runway requirements dramatically limited the forward basing possibilities. In real-world scenarios the capabilities of this force against any given potential target was limited, something the B-1 would be better prepared to handle due to its better takeoff performance and range.

During the 1980 presidential campaign, Ronald Reagan campaigned heavily on the platform that Carter was weak on defense, using the cancellation of the B-1 program as a prime example, a theme he continued using into the 1980s. During this time Carter's defense secretary, Harold Brown, announced the stealth bomber project, apparently implying that this was the reason for the B-1 cancellation. Brown later denied this claim, stating Carter was simply opposed to any military buildup. Although Reagan's primary attack on Carter's decision was now rendered moot, he immediately changed his complaint saying that Carter was giving away secrets and politicizing The Pentagon, charges that led to a round of sparring between Brown and Reagan in the press. Interestingly, it was Brown that had led the original AMSA program, but later came to prefer the cruise missile after taking the job of Defense Secretary in 1977.

7. B-1B program

On taking office, Reagan was faced with the same decision as Carter before; whether to continue with the B-1 for the short term, or to wait for the development of the ATB, a much more advanced aircraft. He decided to do both. Air Force studies suggested that the existing B-52 fleet with ALCM would remain a credible threat until 1985 , as it was predicted that 75% of the B-52 force would survive to attack its targets. After this period the introduction of the SA-10 missile, MiG-31 interceptor and the first Soviet AWACS systems would make them increasingly vulnerable.

During the FY81 budget funds were given to a new study for a bomber for the 1990s time-frame. These studies led to the Long-Range Combat Aircraft (LRCA) project which compared the B-1, F-111 and ATB as possible solutions. An emphasis was placed on the design being multi-role, as opposed to a purely strategic weapon. At the time it was believed the B-1 could be in operation before the B-2, covering the time period between the B-52s increasing vulnerability and the introduction of the ATB. Reagan decided the best solution was to purchase both the B-1 and ATB, and this eventually led to Reagan's October 2nd, 1981 announcement that a new version of the B-1 was being ordered to fill the LRCA role.

Numerous changes were made to the design to better fit it to real-world missions, resulting in the new B-1B. These changes included a reduction in maximum speed, which allowed the variable-aspect intake ramps to be replaced by simpler fixed geometry intake ramps in the newer design. This made the B version more radar-stealthy because the compressor faces of the engines, major radar reflectors, would be partially hidden. Low-altitude speed was somewhat improved, from about Mach 0.85 to 0.92. This left the B-1B with the capability for speeds of about Mach 1.25 "at altitude," a reduction from the B-1A's Mach 2 performance. In order to deal with the introduction of the MiG-31 and other aircraft with look-down capability, the B-1B's electronic warfare suite was significantly upgraded. These changes, along with the rampant inflation of the U.S. economy during the time, dramatically increased the nominal price to about $200 million total projected lifetime cost per completed airframe.

Opposition to the plan was widespread within Congress. Critics pointed out that many of the original problems with the concept remained. In particular it seemed the B-52 fit with electronics similar to the B-1B would be equally able to avoid interception, as the speed advantage of the B-1 was now minimal. It also appeared that the "interim" time frame served by the B-1B would be less than a decade, being rendered obsolete shortly after introduction by the much more capable ATB design. The primary argument in favor of the B-1 was its large conventional payload, and that its takeoff performance allowed it to operate with a credible bombload from a much wider variety of airfields. The debate remained rancorous. But the Air Force very astutely spread production subcontracts across many congressional districts, making the aircraft more popular on Capitol Hill
.
The first production model of the revised B-1B first flew in October 1984, and the first B-1B, "The Star of Abilene", was delivered to Dyess Air Force Base, Abilene, Texas, in June, 1985, with initial operational capability on October 1st, 1986. The 100th and final B-1B was delivered May 2nd, 1988.

Operational History...

The USAF Strategic Air Command (SAC) had B-1 Lancers in service from 1986 through 1992, when SAC was re-organized out of existence. During that time the "Bone" was on limited alert, and the backbone of SAC's alert bombers remained B-52H models. In late 1990 engine fires in two Lancers caused the grounding of the fleet. The cause was traced back to problems in the first-stage fan. Aircraft were placed on "limited alert", meaning they were grounded unless a nuclear war broke out. They were returned to duty one-at-a-time starting in January 1991 as they were inspected and repaired. It was not until mid-April that the fleet was once again declared airworthy.

Originally designed strictly for nuclear war, the B-1's development as an effective conventional bomber was delayed until the 1990s. By 1991, the B-1 had a fledgling conventional capability, forty of them able to drop the 500 lb (230 kg) Mk-82 General Purpose (GP) bomb, although mostly from low altitude. Although cleared for this role, the problems with the engines precluded their use in Operation Desert Storm. Also, B-1s were reserved for strategic nuclear strike missions at this time.

After the absorption of Strategic Air Command (SAC) into Air Combat Command in 1992, the B-1 began to truly develop conventionally. A key part of this development was the start-up of the B-1 Weapons School Division, also in 1992. By the mid-1990s, the B-1 could employ GP weapons as well as various CBUs. By the end of the 1990s, with the advent of the "Block D" upgrade, the B-1 boasted a full array of guided and unguided munitions. This development has continued through the present.

Operationally, the B-1 was first used in combat in support of operations against Iraq during Operation Desert Fox in December 1998, employing unguided GP weapons. B-1s have been subsequently used in Operation Allied Force (Kosovo) and most notably in Operation Enduring Freedom in Afghanistan and the 2003 invasion of Iraq. In both conflicts, the B-1 employed its full array of conventional weapons, most notably the GBU-31, 2,000 lb (900 kg) Joint Direct Attack Munition (JDAM). During OEF, the B-1 improved its mission capable rate to 79%. The B-1 continues to be used in combat to the present day. The most recent addition to its arsenal is the GBU-38, a 500 lb (230 kg) JDAM. The use of the GBU-38 reduces undesired collateral damage and is very useful in urban Close Air Support.

The B-1 now fills an important niche in the Air Force inventory. The project finished on budget, and the B-1 has higher survivability and speed when compared to the older B-52, which it was intended to replace. With the arrival of limited numbers of B-2s in the 1990s and the continuing use of B-52s, its value has been questioned. However, the capability of a high-speed strike with a large bomb payload for time-sensitive operations is useful, and no new strategic bomber is on the immediate horizon.

The B-1 holds several FAI world records for speed, and time-to-climb in different aircraft weight classes. The National Aeronautic Association recognized the B-1B for completing one of the 10 most memorable record flights for 1994.

Rockwell B-1 Lancer- Design


A B-1 lancer in flight. For the full description page, click here.
The B-1 Lancer is a supersonic United States Air Force strategic bomber with variable-sweep wings. It was introduced on October 1st, 1986, which enough range and payload to be able to replace the B-52 Stratofortress, but was developed into a primary subsonic low-level, long-range penetrator. The Lancer serves as the supersonic-capable bomber of the United States Air Force's long-range bomber force, which comprises of the sub-sonic B-52 Stratofortress, as well as the also sub-sonic, B-2 Spirit.



B-1B drawing.

Design...

The B-1 has a blended wing body configuration, with variable-sweep wing, triangular fin control surfaces and four turbofan engines, to improve range and speed with enhanced survivability. Forward swept wing settings are used for takeoff, landings and high-altitude maximum cruise. Aft swept wing settings are used in high subsonic and supersonic flight. The wings of the B-1B originally were cleared for use at settings of 15, 25, 55, and 67.5 degrees. The 45-degree setting was later cleared in 1998–99 timeframe.

The length of the aircraft presented a serious flexing problem due to air turbulence at low altitude. To alleviate this, Rockwell included small canards near the nose on the B-1. An accelerometer would actuate the canards automatically to counteract turbulence and smooth out the ride.



A B-1B cockpit at night. For the full description page, click here.

Unlike the B-1A, the B-1B made no attempt at Mach 2+ speeds. Its maximum speed at altitude is Mach 1.25 (about 950 mph or 1,530 km/h), but its low-level speed increased to Mach 0.92 (700 mph, 1,130 km/h). Technically, the current version of the aircraft can exceed its speed restriction, but not without risking potential damage to its structure and air intakes. The B-1A's engine was modified slightly to produce the F101-102, with an emphasis on durability, and increased efficiency. The core of this engine has since been re-used in several other engine designs, including the F110 which has seen use in the F-14 Tomcat, F-15K/SG variants and most recent versions of the F-16 Fighting Falcon. It is also the basis for the non-afterburning F118 used in the B-2 Spirit bomber and the U-2S. However its greatest success was forming the core of the extremely popular CFM56 civil engine, which can be found on some versions of practically every small-to-medium sized airliner. It includes with an "Alert Start" panel on the nosegear, which quickly activated the engines upon order to scramble.

The B-1's offensive avionics include the Westinghouse (now Northrop Grumman) AN/APQ-164 forward-looking offensive passive electronically scanned array radar set with electronic beam steering (and a fixed antenna pointed downward for reduced radar observability), synthetic aperture radar, ground moving target indicator (MTI), and terrain-following radar modes, Doppler navigation, radar altimeter, and an inertial navigation suite. From 1995 on, the B-1B Block D upgrade added a Global Positioning System receiver.


The B-1's defensive electronics include the Eaton AN/ALQ-161 radar warning and defensive jamming equipment, linked to a total of eight AN/ALE-49 flare dispensers located on top behind the canopy, which are handled by the AN/ASQ-184 avionics management system. The AN/ALE-49 dispenser has a capacity of 12 MJU-23A/B flares each. The MJU-23A/B flare is one of the world's largest infrared countermeasure flares having a gross weight of ~1170 g. The cylindrical Magnesium/Teflon/Viton pellet has a net weight of ~1470 g. The Plans for a defensive systems upgrade program (DSUP) were cancelled for budgetary reasons. The B-1 has also been equipped to carry the ALE-50 Towed Decoy System. The Lancer has an additional Doppler tail-warning radar to detect aircraft or missiles approaching from the rear.

Also aiding the B-1's survivability is its relatively low radar cross-section (RCS). Although not technically a stealth aircraft in a comprehensive sense, thanks to the aircraft's structure, serpentine intake paths and use of radar-absorbent material its RCS is about 1/50th that of the B-52 (probably about 26 ft²/2.4 m²), although the Lancer is not substantially smaller in mass than the Stratofortress.

The B-1 has been upgraded since production through the "Conventional Mission Upgrade Program". This multi-stage program added a new MIL-STD-1760 smart-weapons interface that enables the use of the Joint Direct Attack Munition and other precision-guided conventional weapons, such as the Wind Corrected Munitions Dispenser (WCMD), the AGM-154 Joint Standoff Weapon (JSOW), and the AGM-158 JASSM (Joint Air to Surface Standoff Munition). Future precision munitions include the GBU-39 Small Diameter Bomb. These and other improvements are intended to ensure that the B-1 will be viable through approximately 2020. In addition, the Air Force has recently announced a program to keep the aircraft flying until at least 2040.



B-1B at R.I.A.T. 2004. For the full description page, click here.

Specifications...

1. General characteristics

  • Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer)
  • Length: 146 ft (44.5 m)
  • Wingspan:
    • Extended: 137 ft (41.8 m)
    • Swept: 79 ft (24.1 m)
  • Height: 34 ft (10.4 m)
  • Wing area: 1,950 ft² (181.2 m²)
  • Airfoil: NA69-190-2
  • Empty weight: 192,000 lb (87,100 kg)
  • Loaded weight: 326,000 lb (148,000 kg)
  • Max takeoff weight: 477,000 lb (216,400 kg)
  • Powerplant: 4× General Electric F101-GE-102 augmented turbofans
    • Dry thrust: 14,600 lbf (64.9 kN) each
    • Thrust with afterburner: 30,780 lbf (136.92 kN) each
  • Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank for 1-3 internal weapons bays each

2. Performance

  • Maximum speed: Mach 1.25 (950 mph, 1,529 km/h) at altitude (Mach 0.92, 700 mph, 1,130 km/h at low level)
  • Range: 6,478 nmi (7,456 mi, 11,998 km)
  • Combat radius: 2,993 nmi (3,445 mi, 5,543 km)
  • Service ceiling: 60,000 ft (18,000 m)
  • Wing loading: 167 lb/ft² (816 kg/m²)
  • Thrust/weight: 0.37

3. Armament

  • Hardpoints: six external hardpoints for 59,000 lb (27,000 kg) of ordnance (use for weapons currently restricted by START I treaty) and 3 internal bomb bays for 75,000 lb (34,000 kg) of ordnance to carry from:
  • Missiles:
    • 24× AGM-158 JASSM
    • 12× AGM-154 JSOW
  • Bombs:
    • 84× Mk-82AIR inflatable retarder general purpose bombs
    • 81× Mk-82 low drag general purpose bombs
    • 84× Mk-62 Quickstrike sea mines
    • 8× Mk-65 naval mines
    • 30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)
    • 30× CBU-103/104/105 WCMD
    • 24× GBU-31 JDAM GPS guided bombs
    • 15× GBU-38 JDAM GPS guided bombs (Mk-82 general purpose warhead)
    • 24× Mk-84 general purpose bombs
    • 96× or 144× GBU-39 Small Diameter Bomb GPS guided bombs
    • 16x B61 thermonuclear variable-yield gravity bombs

Avionics

  • 1× Westinghouse AN/APQ-164 forward-looking offensive passive phased-array radar
  • 1× Eaton AN/ALQ-161 radar warning and defensive jamming equipment
  • 1× AN/ASQ-184 defensive management system
  • 1× Lockheed Martin Sniper XR targeting pod.

...

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