A Weapon Systems Officer ( WSO ), nicknamed " Wizzo ", is an air flight officer directly involved in all air operations and weapon systems of a military aircraft.
160-566: Historically, aircrew duties in military aircraft were highly specialised and rigid, because the relevant controls, instruments/displays, and/or weapons were concentrated in front of particular seats, panels or positions. That included two-seat variants of fighter or attack/strike aircraft (including late 20th century types such as the F-4 Phantom II , A-6 Intruder , F-111 Aardvark , F-14 Tomcat , Panavia Tornado , Su-24 Fencer and Su-30MK Flanker-C , Dassault Mirage 2000N/2000D ). From
320-540: A Global Positioning System (GPS) receiver beginning in 1995. The B-1's defensive electronics include the Eaton AN/ALQ-161A radar warning and defensive jamming equipment, which has three sets of antennas; one at the front base of each wing and the third rear-facing in the tail radome . Also in the tail radome is the AN/ALQ-153 missile approach warning system ( pulse-Doppler radar ). The ALQ-161
480-543: A forward looking infrared (FLIR) sensor, optical camera and laser rangefinder / designator . The Pave Tack pod allowed the F-111 to designate targets and drop laser-guided bombs on them. Australian RF-111Cs carried a pallet of sensors and cameras for aerial reconnaissance use. The FB-111 could carry two AGM-69 SRAM air-to-surface nuclear missiles in its weapons bay. General Dynamics trialed an arrangement with two AIM-9 Sidewinder air-to-air missiles carried on rails in
640-668: A tandem -seat aircraft for low-level penetration ground-attack, while the Navy wanted a shorter, high altitude interceptor with side-by-side seating to allow the pilot and radar operator to share the radar display. Also, the USAF wanted the aircraft designed for 7.33 g with Mach 2.5 speed at altitude and Mach 1.2 speed at low level with an approximate length of 70 ft (21.3 m). The Navy had less strenuous requirements of 6 g with Mach 2 speed at altitude and high subsonic speed (approx. Mach 0.9) at low level with
800-551: A FAD fighter, the Navy started with the subsonic , straight-winged aircraft, the Douglas F6D Missileer in the late 1950s. The Missileer was designed to carry six long-range missiles and loiter for five hours, but would be defenseless after firing its missiles. The program was formally canceled in 1961. The Navy had tried variable geometry wings with the XF10F Jaguar , but abandoned it in the early 1950s. It
960-678: A bomber that would combine the Mach 2 speed of the B-58 Hustler with the range and payload of the B-52, ultimately replacing both. After a long series of studies, North American Rockwell (subsequently renamed Rockwell International , B-1 division later acquired by Boeing ) won the design contest for what emerged as the B-1A. Prototypes of this version could fly Mach 2.2 at high altitude and long distances at Mach 0.85 at very low altitudes. The program
1120-515: A ceiling price of $ 529 million along with provisions for deficiency correction amongst other operational clauses and performance criteria. General Dynamics' design team was led by Robert H. Widmer . Recognizing its lack of experience with carrier-based fighters, General Dynamics teamed with Grumman in November 1963 for the assembly and testing of the F-111B. In addition, Grumman would also build
1280-512: A combined $ 2.2 billion for the development and production of 100 new B-1 bombers. Numerous changes were made to the design to make it better suited to the now expected missions, resulting in the 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. This reduced the B-1B's radar cross-section which
1440-593: A detachment of six aircraft from the 474th Tactical Fighter Wing (474th TFW Roadrunners) were sent in March 1968 to Southeast Asia for Combat Lancer testing in real combat conditions in the Vietnam War . During the deployment, 55 night missions were flown against targets in North Vietnam, but two aircraft had been lost. 66–0022 was lost on 28 March, and 66-0017 on 30 March. Replacement aircraft left Nellis, but
1600-536: A final instrument checkride. After primary the SNFO is compared to his or her shipmates and selected for either land-based naval aircraft or tailhook aircraft. Those SNFOs destined for the carrier-based E-2C or E-2D Hawkeye will be known as air control officers and combat information center officers, while those destined for the EA-18G Growler (USN only) will be electronic warfare officers (EWO). Those destined for
1760-594: A heart for transplant. The aircraft landed at Bradley International Airport to deliver the organ to a waiting ambulance. On 14 April 1986, 18 F-111s and approximately 25 Navy aircraft conducted air strikes against Libya under Operation El Dorado Canyon . The 18 F-111s of the 48th Tactical Fighter Wing and 4 EF-111As from the 20th Tactical Fighter Wing flew what turned out to be the longest fighter combat mission in history. The round-trip flight between RAF Lakenheath / RAF Upper Heyford , United Kingdom and Libya of 6,400 miles (10,300 km) spanned 13 hours. One F-111
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#17327835788251920-671: A length of 56 ft (17.1 m). The Navy also wanted the aircraft with a nose large enough for a 48 in (1.2 m) diameter radar dish. McNamara developed a basic set of requirements for TFX based largely on the USAF's requirements and, on 1 September 1961, ordered the USAF to develop it. Nevertheless, a request for proposals (RFP) for the TFX was provided to industry in October 1961. In December, proposals were received from Boeing , General Dynamics , Lockheed , McDonnell , North American and Republic . The evaluation group found all
2080-430: A long-distance record for the aircraft, which demonstrated its ability to conduct extended mission lengths to strike anywhere in the world and return to base without any stops. The National Aeronautic Association recognized the B-1B for completing one of the 10 most memorable record flights for 1994. The B-1 has been upgraded since production, beginning with the "Conventional Mission Upgrade Program" (CMUP), which added
2240-622: A major cause of the aircraft's protracted development and weight increases. The F-111A and F-111B shared the same airframe structural components and Pratt & Whitney TF30-P-1 turbofan engines. They featured side-by-side crew seating in an escape capsule as required by the Navy. The F-111B 's nose was 8.5 feet (2.59 m) shorter as the aircraft could fit on existing carrier elevator decks, and had 3.5-foot-longer (1.07 m) wingtips to improve on-station endurance time; it also carried an AN/AWG-9 Pulse-Doppler radar to guide its AIM-54 Phoenix missiles. The USAF's F-111A would be equipped with
2400-460: A major, lieutenant colonel, or colonel; regardless of rank, the WSO would be the mission commander if he/she is qualified. Currently, all USN WSOs begin their training as student naval flight officers (SNFO) at NAS Pensacola , Florida . Training begins with Introductory Flight Screening, where the WSO flies a Cessna 172 or Piper PA-28 variant to show they are competent enough in aviation to continue
2560-591: A new MIL-STD-1760 smart-weapons interface to enable the use of precision-guided conventional weapons. CMUP was delivered through a series of upgrades: In 2007, the Sniper XR targeting pod was integrated on the B-1 fleet. The pod is mounted on an external hardpoint at the aircraft's chin near the forward bomb bay. Following accelerated testing, the Sniper pod was fielded in summer 2008. Future precision munitions include
2720-521: A new "super-Foxbat" (almost certainly referring to the MiG-31 ) that had look-down/shoot-down radar in order to attack cruise missiles. This would also make any low-level penetration aircraft "visible" and easy to attack. Given that the B-1's armament suite was similar to the B-52, and it then appeared no more likely to survive Soviet airspace than the B-52, the program was increasingly questioned. In particular, Senator William Proxmire continually derided
2880-584: A new attitude indicator. The IBS upgrades were completed in 2020. In August 2019, the Air Force unveiled a modification to the B-1B to allow it to carry more weapons internally and externally. Using the moveable forward bulkhead, space in the intermediate bay was increased from 180 to 269 in (457 to 683 cm). Expanding the internal bay to make use of the Common Strategic Rotary Launcher (CSRL), as well as utilizing six of
3040-494: A nuclear war broke out. Following inspections and repairs they were returned to duty beginning on 6 February 1991. By 1991, the B-1 had a fledgling conventional capability, forty of them able to drop the 500-pound (230 kg) Mk-82 General Purpose (GP) bomb, although mostly from low altitude. Despite being cleared for this role, the problems with the engines prevented their use in Operation Desert Storm during
3200-504: A powerful tactical aircraft which could be used against ground troops along with strategic targets from high altitudes. The much smaller bomb bay of the B-70 would have made it much less useful in this role. Although effective, the B-52 was not ideal for the low-level role. This led to a number of aircraft designs known as penetrators , which were tuned specifically for long-range low-altitude flight. The first of these designs to see operation
3360-663: A safe counterforce option because the bombers could be quickly launched into safe loitering areas where they could not be attacked. However, the introduction of the SLBM made moot the mobility and survivability argument, and a newer generation of ICBMs, such as the Minuteman III , had the accuracy and speed needed to attack point targets. During this time, ICBMs were seen as a less costly option based on their lower unit cost, but development costs were much higher. Secretary of Defense Robert McNamara preferred ICBMs over bombers for
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#17327835788253520-619: A second display aids with threat evasion and targeting, and acts as a back-up display. CITS saw a new diagnostic system installed that allows crew to monitor over 9,000 parameters on the aircraft. Other additions are to replace the two spinning mass gyroscopic inertial navigation system with ring laser gyroscopic systems and a GPS antenna, replacement of the APQ-164 radar with the Scalable Agile Beam Radar – Global Strike ( SABR-GS ) active electronically scanned array , and
3680-510: A speed advantage at low altitudes. The USAF's Tactical Air Command (TAC) was largely concerned with the fighter-bomber and deep strike/ interdiction roles. TAC was in the process of receiving its latest design, the Republic F-105 Thunderchief , which was designed to deliver nuclear weapons fast and far, but required long runways. A simpler variable geometry wing configuration with the pivot points farther out from
3840-514: A trapeze arrangement from the bay, but this was not adopted. Early F-111 models had radars equipped to guide the AIM-7 Sparrow medium-range air-to-air missile, but it was never fitted. Each wing was equipped with four underwing pylons. The inner two pylons on each wing rotated to align with the fuselage, while the outer two were fixed. Each pylon had a capacity of 5,000 pounds (2,300 kilograms). Various bombs and missiles could be carried on
4000-590: A troubled development and Navy requirements changed to a maneuverable aircraft for dogfighting. The swing-wing configuration, TF-30 engines, AIM-54 Phoenix air-to-air missiles and AWG-9 radar developed for the F-111B were used on its replacement, the Grumman F-14 Tomcat. The Tomcat was large enough to carry the AWG-9 and Phoenix missiles while exceeding both the F-111's and the F-4's maneuverability. The F-111C
4160-439: Is Mach 1.25 (about 950 mph or 1,530 km/h at altitude), but its low-level speed increased to Mach 0.92 (700 mph, 1,130 km/h). The speed of the current version of the aircraft is limited by the need to avoid damage to its structure and air intakes. To help lower its radar cross-section, the B-1B uses serpentine air intake ducts (see S-duct ) and fixed intake ramps , which limit its speed compared to
4320-422: Is a retired supersonic, medium-range, multirole combat aircraft. Production models of the F-111 had roles that included attack (e.g. interdiction ), strategic bombing (including nuclear weapons capabilities), reconnaissance and electronic warfare . Aardvark comes from a South African animal that has a long nose and hugs the terrain. It is an Afrikaans word that translates literally as "earth pig"—hence
4480-690: Is a supersonic variable-sweep wing , heavy bomber used by the United States Air Force . It has been nicknamed the "Bone" (from "B-One"). As of 2024 , it is one of the United States Air Force's three strategic bombers , along with the B-2 Spirit and the B-52 Stratofortress . Its 75,000-pound (34,000 kg) payload is the heaviest of any U.S. bomber. The B-1 was first envisioned in the 1960s as
4640-550: Is 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. Each AN/ALE-49 dispenser has a capacity of 12 MJU-23A/B flares. The MJU-23A/B flare is one of the world's largest infrared countermeasure flares at a weight of over 3.3 pounds (1.5 kg). The B-1 has also been equipped to carry the ALE-50 towed decoy system . Also aiding
4800-591: Is the export version for Australia, combining the F-111A with longer F-111B wings and strengthened FB-111A landing gear. Australia ordered 24 F-111s and, following delays, the Royal Australian Air Force accepted the aircraft in 1973. Four were converted to the RF-111C reconnaissance variant in 1979–80. Australia also purchased four ex-USAF F-111As and converted them into F-111Cs. In the 1990s,
4960-624: Is where all the training comes together to culminate in the SWSO receiving his or her wings of gold. In the T-45C, a USN single-engine jet trainer, SWSOs learn advanced instrument flying, radar navigation, and composite visual/radar navigation. SWSOs also receive instruction in Air-to-Ground strike training, Air-to-Air intercept training, Basic Fighter Maneuvering, and Close Air Support. A/G Training takes place on both VR and IR routes that criss-cross
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5120-466: The 435th Fighter Training Squadron at Randolph Air Force Base , Texas or the 49th Fighter Training Squadron at Columbus Air Force Base , Mississippi. WSOs also learn about the culture of being a young aircrew member in a USAF fighter squadron. The course lasts approximately eight weeks. EWO USAF WSOs selected for the B-1B, B-52H , and some F-15E selectees will become electronic warfare officers (EWOs) by attending this 12-week training program at
5280-572: The 563d Flying Training Squadron at Randolph Air Force Base, Texas. A similar program for USN EWOs in the EA-18G and USMC ECMOs in the EA-6B is conducted at the Center for Information Dominance at Corry Station , Florida. In both programs, students learn the basics of radar theory, electronic attack, and electronic defense. General Dynamics F-111 Aardvark The General Dynamics F-111 Aardvark
5440-678: The B-1B Lancer bomber, there are 2 weapon systems officers manning crew positions aft of the pilot and co-pilot. They are known as the Offensive Systems Officer (OSO), and the Defensive Systems Officer (DSO). WSOs also flew in the now-retired F-111 Aardvark strike bomber, flown by the US Air Force and Royal Australian Air Force , and the now retired USAF EF-111A Raven airborne jammer. In
5600-823: The Boeing F/A-18E/F Super Hornet as an interim measure until the Lockheed Martin F-35 Lightning II became available. The May 1960 U-2 incident , in which an American CIA U-2 reconnaissance plane was shot down over the USSR, stunned the United States government. Besides greatly damaging US–Soviet relations, the incident showed that the Soviet Union had developed a surface-to-air missile that could reach aircraft above 60,000 feet (18,000 meters). Consequently,
5760-563: The Case–Church Amendment . The 347th TFW was stationed at Korat Royal Thai Air Force Base from 12 July 1974 until 30 June 1975. In May 1975, 347th TFW F-111s provided air support during the Mayaguez incident . One of the most unusual missions occurred on 14 February 1986, when two FB-111s of the 509th Bombardment Wing were dispatched from then Pease Air Force Base , New Hampshire to Tinker Air Force Base , Oklahoma to pick up
5920-718: The F/A-18F Super Hornet strike fighter from that jet's aft seat. Prior to the introduction of the F/A-18F, they were known as Radar Intercept Officers (RIO) in the aft seats of the F-4 Phantom II and F-14 Tomcat ; as Bombardier/Navigators (B/N) in the right seat of the A-6 Intruder and the A-3 Skywarrior and in the aft seat in the A-5 Vigilante ; and Reconnaissance Attack Navigators (RAN) in
6080-702: The General Dynamics F-16 Fighting Falcon . It is also the basis for the non- afterburning GE F118 used in the B-2 Spirit and the U-2S . The F101 engine core is also used in the CFM56 civil engine. The nose-gear door is the location for ground-crew control of the auxiliary power unit (APU) which can be used during a scramble for quick-starting the APU. The B-1's main computer is
6240-1000: The General Electric AN/APQ-113 attack radar mated to a separate Texas Instruments AN/APQ-110 terrain-following radar lower in the nose and a Litton AJQ-20 inertial navigation and nav/attack system. The terrain-following radar (TFR) was integrated into the automatic flight control system, allowing for "hands-off" flight at high speeds and low levels (down to 200 ft or 61 m). A total of 159 F-111As were produced, including 30 pre-production aircraft that were rebuilt to production standards. 42 F-111As were converted to EF-111A Ravens for an electronic warfare tactical electronic jamming role. In 1982, four surviving F-111As were provided to Australia as attrition replacements and modified to F-111C standard, including its longer-span wings and reinforced landing gear. Three pre-production F-111A were used by NASA for various tests. The 13th F-111A received new wing designs for
6400-471: The Gulf War . B-1s were primarily reserved for strategic nuclear strike missions at this time, providing the role of airborne nuclear deterrent against the Soviet Union. The B-52 was more suited to the role of conventional warfare and it was used by coalition forces instead. Originally designed strictly for nuclear war, the B-1's development as an effective conventional bomber was delayed. The collapse of
6560-885: The IBM AP-101 , which was also used on the Space Shuttle orbiter and the B-52 bomber. The computer is programmed with the JOVIAL programming language . The Lancer'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 indication (GMTI), and terrain-following radar modes, Doppler navigation , radar altimeter , and an inertial navigation suite. The B-1B Block D upgrade added
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6720-796: The Operation Linebacker II aerial offensive against the North Vietnamese, who called the aircraft "Whispering Death". They also supported regional aerial operations against other communist forces such as Operation Phou Phiang III during the Laotian Civil War in Laos . Crews described their flying in Vietnam as "speed is life", "one pass, haul ass", and "you do more than one pass in a target area you die". The F-111's ability with terrain-following radar ("the best in
6880-537: The Poseidon MRA1 maritime patrol aircraft. Non-commissioned Aircrew can serve as a WSOp (Weapon Systems Operator), an umbrella term for the various specialist aircrew responsible for assisting the pilot in operating the mission systems of the aircraft (e.g. linguists, loadmasters, crewman). In the United States Navy , WSOs are naval flight officers responsible for manning the weapon systems of
7040-748: The Small Diameter Bomb . The USAF commenced the Integrated Battle Station (IBS) modification in 2012 as a combination of three separate upgrades when it realised the benefits of completing them concurrently; the Fully Integrated Data Link (FIDL), Vertical Situational Display Unit (VSDU) and Central Integrated Test System (CITS). FIDL enables electronic data sharing, eliminating the need to enter information between systems by hand. VSDU replaces existing flight instruments with multifunction color displays,
7200-537: The U.S. Air Force , "WSO" also refers to a USAF combat systems officer (CSO, formerly NOT USAF navigator) who is the aft crew member in the F-15E Strike Eagle . In the B-52, the CSO crew members on the lower deck of the aircraft who were previously designated as navigator and radar navigator (bombardier) are now known as weapon systems officers while the CSO on the upper deck is an electronic warfare officer. In
7360-618: The United States Air Force Strategic Air Command (SAC) and the RAF Bomber Command 's plans to send subsonic, high-altitude Boeing B-47 Stratojet and V bomber formations into the USSR were realized to be much less viable. By 1960, SAC had begun moving to low-level penetration , which greatly reduced radar detection distances. At the time, SAMs were ineffective against low-flying aircraft while interceptor aircraft had less of
7520-565: The VT-10 Wildcats. Training begins with several weeks of ground school followed by remnants of the "super-fo" program from the U.S. Navy where the SNFO takes front seat of the new T-6 Texan II for six "contact" flights where the student will become familiar with the T-6. The SNFO is treated like a pilot training student for these six flights. After Contacts, the SNFO goes back to academics to learn instrument flying rules . Primary ends with
7680-580: The 1970s onward an aircraft with two-member crews, such as the F-15E Strike Eagle , F/A-18F Super Hornet or Su-34 Fullback and Dassault Rafale B have often featured programmable multi-function displays . These programs allow roles to be more flexible than previous generation aircraft. Multiple crew members can be responsible for detecting, targeting and engaging air-to-air or ground targets, communications, datalinks and/or defensive systems. Roles can be customized based on experience, expertise, workload, tactics, and weapons being employed. Pilots usually retain
7840-479: The 1990s; the last F-111Fs were withdrawn in 1996 while the remaining EF-111s also departed in 1998. The F-111 was replaced in USAF service by the F-15E Strike Eagle for medium-range precision strike missions, while the supersonic bomber role has been assumed by the B-1B Lancer . The RAAF continued to operate the type up until December 2010, when the last F-111C was retired; its role was transitioned to
8000-422: The AN/APQ-113 attack radar and the AN/APQ-110 terrain-following radar and air-to-ground armament. During September 1963, the F-111A mockup was inspected. On 15 October 1964, the first test F-111A was rolled out of Plant 4 of General Dynamics' facility in Fort Worth, Texas; it was powered by YTF30-P-1 turbofans and used a set of ejector seats as the escape capsule was not yet available. On 21 December 1964,
8160-465: The Air Force portion of the deterrent force and felt a new expensive bomber was not needed. McNamara limited the AMSA program to studies and component development beginning in 1964. Program studies continued; IBM and Autonetics were awarded AMSA advanced avionics study contracts in 1968. McNamara remained opposed to the program in favor of upgrading the existing B-52 fleet and adding nearly 300 FB-111s for shorter range roles then being filled by
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#17327835788258320-403: The Australians have a bomber that can put a bomb through that window on to the table here in front of us?" Australian F-111s were ready to attack Indonesian forces during the establishment of East Timor 's independence and the deployment of the Australian-led International Force for East Timor . In 2006, an RAAF F-111 scuttled the North Korean ship Pong Su on 23 March 2006. Because of
8480-401: The B-1 in public, arguing it was an outlandishly expensive dinosaur. During the 1976 federal election campaign, Jimmy Carter made it one of the Democratic Party's platforms, saying "The B-1 bomber is an example of a proposed system which should not be funded and would be wasteful of taxpayers' dollars." When Carter took office in 1977 he ordered a review of the entire program. By this point
8640-513: The B-1's survivability is its relatively low RCS. Although not technically a stealth aircraft, thanks to the aircraft's structure, serpentine intake paths and use of radar-absorbent material its RCS is about 1/50th that of the similar sized B-52. This is approximately 26 ft or 2.4 m , comparable to that of a small fighter aircraft . The B-1 holds 61 FAI world records for speed, payload, distance, and time-to-climb in different aircraft weight classes. In November 1993, three B-1Bs set
8800-442: The B-1A. Vanes in the intake ducts serve to deflect and shield radar returns from the highly reflective engine compressor blades. The B-1A's engine was modified slightly to produce the GE F101-102 for the B-1B, with an emphasis on durability, and increased efficiency. The core from this engine was subsequently used in several other engines, including the GE F110 used in the F-14 Tomcat , F-15K/SG variants and later versions of
8960-415: The B-1B would be less than a decade, being rendered obsolete shortly after the introduction of a much more capable ATB design. The primary argument in favor of the B-1 was its large conventional weapon payload, and that its takeoff performance allowed it to operate with a credible bomb load from a much wider variety of airfields. Production subcontracts were spread across many congressional districts, making
9120-425: The B-52, allowing it to operate from a wider variety of bases. Penetration of the Soviet Union's defenses would take place at supersonic speed , crossing them as quickly as possible before entering the more sparsely defended interior of the country where speeds could be reduced again. The large size and fuel capacity of the design would allow the "dash" portion of the flight to be relatively long. In order to achieve
9280-409: The B-52, but less range. Because of this, and a growing shift to the intercontinental ballistic missile (ICBM) force, the B-70 bomber program was cancelled in 1961 by President John F. Kennedy , and the two XB-70 prototypes were used in a supersonic research program. Although never intended for the low-level role, the B-52's flexibility allowed it to outlast its intended successor as the nature of
9440-421: The B-58. He again vetoed funding for AMSA aircraft development in 1968. President Richard Nixon reestablished the AMSA program after taking office, keeping with his administration's flexible response strategy that required a broad range of options short of general nuclear war . Nixon's Secretary of Defense, Melvin Laird , reviewed the programs and decided to lower the numbers of FB-111s, since they lacked
9600-632: The EF-111 electronic warfare variant in 1998. The Australian government ordered 24 F-111C aircraft to replace the RAAF's English Electric Canberras in the bombing and tactical strike role. While the first aircraft was officially handed over in September 1968, structural issues delayed the entry into service. The first F-111C was accepted at Nellis Air Force Base on 15 March 1973. The RAAF's first six F-111Cs arrived at RAAF Base Amberley on 1 July 1973, and three subsequent flights of six F-111s arrived on 27 July, 28 September and 4 December. F-111Cs were allocated to No. 1 Squadron and No. 6 Squadron , under
9760-413: The EF-111 electronic warfare versions were later developed for the USAF. Production of the F-111 ended in 1976, following the completion of 563 aircraft. The F-111 was an all-weather attack aircraft, capable of low-level penetration of enemy defenses to deliver ordnance on the target. The F-111 featured variable-geometry wings, an internal weapons bay and a cockpit with side-by-side seating. The cockpit
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#17327835788259920-436: The F-111 and XB-70. It used a crew escape capsule , that ejected as a unit to improve crew survivability if the crew had to abandon the aircraft at high speed. Additionally, the design featured large variable-sweep wings in order to provide both more lift during takeoff and landing, and lower drag during a high-speed dash phase. With the wings set to their widest position the aircraft had a much better airfield performance than
10080-427: The F-111 and began operating the F-111C in 1973. As early as March 1968, the USAF were deploying F-111s into active combat situations; the type saw heavy use during the latter half of the Vietnam War to conduct low-level ground-attack missions, flying in excess of 4,000 combat missions while incurring only six combat losses in the theatre. The F-111s also participated in the Gulf War (Operation Desert Storm) in 1991;
10240-462: The F-111 were troubled by compressor surges and stalls across certain portions of the flight regime. General Dynamics had elected to use an uncommon spike-shaped variable intake for the engine for the performance. Studies performed by NASA, the USAF, and General Dynamics led to the engine inlet being redesigned; modifications were implemented between 1965 and 1966, culminating with the "Triple Plow I" and "Triple Plow II" designs. During February 1965,
10400-419: The F-111, the WSO (EWO in the EF-111) was seated directly to the right of the pilot/aircraft commander. The WSO integrates with the pilot to collectively achieve and maintain crew efficiency, situational awareness and mission effectiveness. In the U.S. Air Force fighter aircraft such as the F-15E Strike Eagle, the WSO can pilot the aircraft when required, although this is typically during non-tactical portions of
10560-487: The F-111. Early A-models used the TF30-P-1 engine. Most A-models used the TF30-P-3 engine with 12,000 lbf (53 kN) dry and 18,500 lbf (82 kN) afterburning thrust and "Triple Plow I" variable intakes, providing a maximum speed of Mach 2.3 (1,450 mph, 2,300 km/h) at altitude. The variant had a maximum takeoff weight of 92,500 lb (42,000 kg) and an empty weight of 45,200 lb (20,500 kg). The F-111A's Mark I avionics suite included
10720-414: The F-111A achieved a speed of Mach 1.3 while flying with an interim intake design. On 18 May 1965, the F-111B made its first flight; it was also equipped with ejector seats initially. Separately, cracks in the F-111's wing attach points were first discovered in 1968 during ground fatigue testing; during the following year, the crash of an F-111 was attributed to a cracked wingbox. On 22 December 1969,
10880-429: The F-111A made its first flight from Carswell Air Force Base , Texas. Lasting for 22 minutes, less than planned due to a flap malfunction, this initial flight was considered to be satisfactory overall; category I testing commenced immediately thereafter. Early flights of the F-111, which included supersonic flights, demonstrated favorably simplistic maintenance requirements, amongst other qualities. Various changes to
11040-524: The F-111C underwent a comprehensive digital avionics upgrade program (AUP) which introduced new nav/attack systems (PAVE TACK Laser/infrared targeting system) and digital flight control computers. Later, the C model was upgraded with a unique version of the TF-30 engine known as the P-108. This local version mated the P-109 engine to a P-107 afterburner, delivering 20,840 lb of thrust and significantly increased reliability. The RAAF retired its last F-111Cs in December 2010 after 37 years of service. The F-111D
11200-423: The F-111Fs completed 3.2 successful strike missions for every unsuccessful one, better than any other U.S. strike aircraft used in the operation. RAAF F-111s never saw offensive action, but were deployed periodically as a deterrent, such as for the Australian-led International Force East Timor . Being relatively expensive to maintain amid post- Cold War budget cuts, the USAF elected to retire its F-111 fleet during
11360-452: The F-15E in their ability to withstand the g-forces routinely experienced by fighter aircrew. SERE The Survival, Evasion, Resistance and Escape (SERE) training course trains all USAF aircrew basic survival skills, combat evasion, and techniques to resist exploitation if captured. WSOs also learn how to survive an aircraft ejection over land. For USAF personnel, the three-week course is taught at Fairchild Air Force Base , Washington and
11520-639: The F/A-18F Super Hornet (USN Only) or the F/A-18D Hornet (USMC only) will become WSOs. Intermediate picks up where Primary ends for USAF SWSOs. After the instrument phase of training, students move to visual navigation (VNAV) "low levels" at 2000'AGL, and finish in the T-6 with a final training block called "forms" (formation flying). Forms consist of four flights of learning the basics of close in formation flying. After forms, SWSOs head back to ground school to learn an entirely new aircraft,
11680-619: The MiG-31 interceptor and the first effective Soviet Airborne Early Warning and Control (AWACS) systems would make the B-52 increasingly vulnerable. During 1981, funds were allocated to a new study for a bomber for the 1990s time-frame which led to developing the Long-Range Combat Aircraft (LRCA) project. The LRCA evaluated the B-1, F-111, and ATB as possible solutions; an emphasis was placed on multi-role capabilities, as opposed to purely strategic operations. In 1981, it
11840-428: The Navy found both submissions unacceptable for its operations. Two more rounds of updates to the proposals were conducted, with Boeing being picked by the selection board. In November 1962, McNamara selected General Dynamics' proposal due to its greater commonality between USAF and Navy versions. The Boeing aircraft shared less than half of the major structural components. On 21 December 1962, General Dynamics signed
12000-423: The TFX contract. A congressional investigation into the procurement processed was conducted, but did not change the selection. On 1 May 1964, the definitized contract was issued for the program, including flight testing, spares, ground equipment, training devices, static and fatigue test data, and the production of an initial 23 F-111 aircraft; it was structured as a fixed price incentive fee (FPIF) contract with
12160-624: The Transonic Aircraft Technology and Advanced Fighter Technology Integration programs in the 1970s and 1980s. It retired to the United States Air Force Museum at Wright-Patterson Air Force Base in 1989. Unconverted F-111As were mothballed at Aerospace Maintenance and Regeneration Center at Davis-Monthan Air Force Base in June 1991. The F-111B was to be a fleet air defense (FAD) fighter for
12320-701: The U.S. Rockwell B-1 Lancer bomber (1974); and the European Panavia Tornado (1974). The Sukhoi Su-24 was very similar to the F-111. The U.S. Navy's role intended for the F-111B was instead filled by another variable-geometry design, the Grumman F-14 Tomcat . The first of six initial production F-111s was delivered on 17 July 1967 to fighter squadrons at Nellis Air Force Base . These aircraft were used for crew training. 428th Tactical Fighter Squadron achieved initial operational capability on 28 April 1968. After early testing,
12480-445: The U.S. Air Force. During the 1980 presidential campaign, Ronald Reagan campaigned heavily on the platform that Carter was weak on defense, citing the cancellation of the B-1 program as an 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. On taking office, Reagan
12640-432: The U.S. Navy, fulfilling a requirement for a carrier-based fighter aircraft armed with heavy, long-range missiles to defend aircraft carriers and their battle groups from Soviet bombers and fighter-bombers equipped with anti-ship missiles. General Dynamics, lacking experience with carrier-based aircraft, partnered with Grumman for this version. Seven F-111Bs were completed for testing but it never entered fleet service. It had
12800-548: The US Navy was to carry two AIM-54 Phoenix long-range air-to-air missiles in the bay. The cannon had a large 2,084-round ammunition tank, and its muzzle was covered by a fairing; however, it was rarely fitted on F-111s. The F-111C and F-111F were equipped to carry the AN/AVQ-26 Pave Tack targeting system on a rotating carriage that kept the pod protected within the weapons bay when not in use. Pave Tack featured
12960-452: The USAF equal capability of penetrating Soviet airspace. With a range of 1,500 miles (2,400 km), the ALCM could be launched well outside the range of any Soviet defenses and penetrate at low altitude like a bomber (with a much lower radar cross-section (RCS) due to smaller size), and in much greater numbers at a lower cost. A small number of B-52s could launch hundreds of ALCMs, saturating
13120-630: The USAF issued requirements for a new bomber combining the payload and range of the Boeing B-52 Stratofortress with the Mach ;2 maximum speed of the Convair B-58 Hustler . In December 1957, the USAF selected North American Aviation 's B-70 Valkyrie for this role, a six-engine bomber that could cruise at Mach 3 at high altitude (70,000 ft or 21,000 m). Soviet Union interceptor aircraft ,
13280-505: The USAF opted to ground the fleet due to this issue, save for those involved in flight testing. The resolution involved the redesigning of the attach structure and necessitated testing to ensure adequate design and workmanship. On 31 July 1970, the grounding was lifted. Category I flight testing of the F-111A, which had started in 1964, continued through to 31 March 1972. Category II tests started in January 1966, while Category III testing
13440-472: The USN T-39 Sabreliner . The T-39 is used as an intermediate instrument and low-level trainer for SWSOs, where they receive a total of eight flights. Students are required to learn the aircraft in a two-week ground school period before they go flight side. In contrast, T-6 ground school is four weeks. Training ends at either VT-10 or VT-4 with the "i-grad" ceremony and top graduate award. VT-86
13600-400: The aft fuselage and the landing gear of the F-111A. The General Dynamics and Grumman team faced ambitious requirements for range, weapons load, and aircraft weight. Thus, the F-111 was designed to incorporate numerous features that were new to production military aircraft, such as variable-geometry wings and afterburning turbofan engines. This use of unfamiliar features has been attributed as
13760-483: The aft seat of the RA-5C Vigilante . In U.S. Naval Aviation ( USN & USMC ), when designated as the mission commander (MC), the WSO is responsible for all phases of the assigned mission, especially if there are multiple aircraft involved. For example, the aircraft pilot could be the junior member of a flight crew such as a USN lieutenant, junior grade/USMC 1st lieutenant or USN lieutenant/USMC captain, and
13920-455: The air war environment changed. The B-52's huge fuel load allowed it to operate at lower altitudes for longer times, and the large airframe allowed the addition of improved radar jamming and deception suites to deal with radars. During the Vietnam War , the concept that all future wars would be nuclear was turned on its head, and the "big belly" modifications increased the B-52's total bomb load to 60,000 pounds (27,000 kg), turning it into
14080-530: The aircraft more popular on Capitol Hill . B-1A No. 1 was disassembled and used for radar testing at the Rome Air Development Center in the former Griffiss Air Force Base , New York . B-1As No. 2 and No. 4 were then modified to include B-1B systems. The first B-1B was completed and began flight testing in March 1983. The first production B-1B was rolled out on 4 September 1984 and first flew on 18 October 1984. The 100th and final B-1B
14240-411: The aircraft presented a flexing problem due to air turbulence at low altitude. To alleviate this, Rockwell included small triangular fin control surfaces or vanes near the nose on the B-1. The B-1's Structural Mode Control System moves the vanes, and lower rudder, to counteract the effects of turbulence and smooth out the ride. Unlike the B-1A, the B-1B cannot reach Mach 2+ speeds; its maximum speed
14400-496: The aircraft's "Pig" nickname during its Australian service. Developed in the 1960s by General Dynamics under Robert McNamara 's TFX Program , the F-111 pioneered variable-sweep wings , afterburning turbofan engines, and automated terrain-following radar for low-level , high-speed flight. Its design influenced later variable-sweep wing aircraft, and some of its advanced features have become commonplace. The F-111 suffered problems during initial development, largely related to
14560-408: The aircraft's centerline was reported by NASA in 1958, which made swing-wings viable. This led USAF leaders to encourage its use. In June 1960, the USAF issued specification SOR 183 for a long-range interdiction/strike aircraft able to penetrate Soviet air defenses at very low altitudes and high speeds. Specifically, it was to be capable of at least 800 miles of low-level flight, 400 of which
14720-476: The airframe to carry more fuel and weapons. Dubbed the B-1B, deliveries of the new variant began in 1985; the plane formally entered service with Strategic Air Command (SAC) as a nuclear bomber the following year. By 1988, all 100 aircraft had been delivered. With the disestablishment of SAC and its reassignment to the Air Combat Command in 1992, the B-1B's nuclear capabilities were disabled and it
14880-526: The best option was to base the design on the USAF requirement, and use a modified version for the Navy. In June 1961, Secretary McNamara ordered the go ahead of Tactical Fighter Experimental (TFX), despite USAF and Navy efforts to keep their programs separate. According to aviation author Peter E. Davis, military officials were disconcerted by McNamara's focus on compromised requirements for financial reasons. The two services could agree only on swing-wing, two-seat, twin-engine design features. The USAF wanted
15040-454: The bomber has been commonly called the "Bone"; a nickname that appears to stem from an early newspaper article on the aircraft wherein its name was phonetically spelled out as "B-ONE" with the hyphen inadvertently omitted. In late 1990, engine fires in two Lancers led to a grounding of the fleet. The cause was traced back to problems in the first-stage fan, and the aircraft were placed on "limited alert"; in other words, they were grounded unless
15200-419: The bomber which, combining both internal and external weapon carriage, could conceivably bring the total number of hypersonic weapons to 31. The second B-1B, "The Star of Abilene", was the first B-1B delivered to SAC in June 1985. Initial operational capability was reached on 1 October 1986 and the B-1B was placed on nuclear alert status. The B-1 received the official name "Lancer" on 15 March 1990. However,
15360-428: The cancellation of the B-70 program had led some to question the need for a new strategic bomber of any sort. The USAF was adamant about retaining bombers as part of the nuclear triad concept that included bombers, ICBMs, and submarine-launched ballistic missiles (SLBMs) in a combined package that complicated any potential defense. They argued that the bomber was needed to attack hardened military targets and to provide
15520-422: The clutter from ground reflections (lack of look-down/shoot-down capability). The switch from high-altitude to low-altitude flight profiles severely affected the B-70, the design of which was tuned for high-altitude performance. Higher aerodynamic drag at low level limited the B-70 to subsonic speed while dramatically decreasing its range. The result would be an aircraft with somewhat higher subsonic speed than
15680-639: The control of No. 82 Wing . In Australia, the F-111 was affectionately known as the "Pig". The purchase proved to be highly successful for the RAAF. Although it never saw combat, the F-111C was the fastest, longest range combat aircraft in Southeast Asia, providing Australia with independent strike capability. Benny Murdani told Kim Beazley that when others became upset with Australia during Indonesian cabinet meetings , Murdani told them "Do you realise
15840-489: The course, USAF WSOs learn the basics of surviving an aircraft ejection over water, obtaining food and drinkable water when stranded at sea, combat evasion at sea, and how to be successfully rescued by boat or helicopter. For USN and USMC WSOs, this program was previously completed at NAS Pensacola during their Aviation Preflight Indoctrination (API) training. Centrifuge training This one-day course located at Brooks City-Base , San Antonio, Texas, tests USAF WSOs selected for
16000-441: The decision. NATO commander Alexander Haig described the ALCM as an "attractive alternative" to the B-1. French General Georges Buis stated "The B-1 is a formidable weapon, but not terribly useful. For the price of one bomber, you can have 200 cruise missiles." Flight tests of the four B-1A prototypes for the B-1A program continued through April 1981. The program included 70 flights totaling 378 hours. A top speed of Mach 2.22
16160-405: The defense. A program to improve the B-52 and develop and deploy the ALCM would cost at least 20% less than the planned 244 B-1As. On 30 June 1977, Carter announced that the B-1A would be canceled 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
16320-539: The design due to failures to meet specifications and desired improvements for ease of maintenance and operation. The first B-1A prototype (Air Force serial no. 74–0158) flew on 23 December 1974. As the program continued the per-unit cost continued to rise in part because of high inflation during that period. In 1970, the estimated unit cost was $ 40 million, and by 1975, this figure had climbed to $ 70 million. In 1976, Soviet pilot Viktor Belenko defected to Japan with his MiG-25 "Foxbat" . During debriefing he described
16480-526: The desired 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 , created in 1962. The Air Force issued a request for proposals in November 1969. Proposals were submitted by Boeing, General Dynamics and North American Rockwell in January 1970. In June 1970, North American Rockwell
16640-577: The eight external hardpoints that had been previously out of use to keep in line with the New START Treaty, would increase the B-1B's weapon load from 24 to 40. The configuration also enables it to carry heavier weapons in the 5,000 lb (2,300 kg) range, such as hypersonic missiles; the AGM-183 ARRW is planned for integration onto the bomber. In the future the HAWC could be used by
16800-529: The engines. The F-111's maximum practical weapons load was limited, since the fixed pylons could not be used with the wings fully swept. Tactical F-111s were fitted with shoulder rails on the four inner swiveling pylons to mount AIM-9 Sidewinder air-to-air missiles for self-defense. Australian F-111Cs were equipped to launch the Harpoon anti-ship missile, and the Popeye stand-off missile. FB-111As could carry
16960-634: The engines. A fighter variant intended for the United States Navy , the F-111B , was canceled before production; it was intended for aircraft carrier-based roles, including long-range interception . Several specialized models, such as the FB-111A strategic bomber and the EF-111A electronic warfare aircraft, were also developed. The F-111 entered service in 1967 with the United States Air Force (USAF). The Royal Australian Air Force (RAAF) also ordered
17120-567: The era were subject to " clutter " from stray returns from the ground and other objects, which meant a minimum angle existed above the horizon where they could detect a target. Bombers flying at low altitudes could remain under these angles simply by keeping their distance from the radar sites. This combination of effects made SAMs of the era ineffective against low-flying aircraft. The same effects also meant that low-flying aircraft were difficult to detect by higher-flying interceptors, since their radar systems could not readily pick out aircraft against
17280-422: The fighter world", according to F-111 pilot Richard Crandall) to fly as low as 200 feet (61 m) above ground level at 480 knots (890 km/h) or faster in most weather conditions made it very effective; missions did not require tankers or ECM support, and they could operate in weather that grounded most other aircraft. One F-111 could carry the bomb load of four McDonnell Douglas F-4 Phantom IIs. The worth of
17440-456: The high maintenance time required for every flight hour, the F-111's retirement began with the F-111G models operated by No. 6 Squadron in late 2007. Twenty-four Boeing F/A-18E/F Super Hornets were procured as an interim replacement as the Lockheed Martin F-35 Lightning II program was delayed. The last F-111s were retired on 3 December 2010. The F-111A was the initial production version of
17600-418: The loss of a third F-111A (66-0024) on 22 April halted F-111A combat operations. The squadron returned to the United States in November. The cause of the first two losses is unknown as the wreckages were never recovered. It turned out that the third loss was traced to a failure of a hydraulic control-valve rod for the horizontal stabilizer which caused the aircraft to pitch up uncontrollably. Further inspection of
17760-411: The maintenance budget" —the F-111 was in service with the USAF from 1967 through 1998. The FB-111s were operated by Strategic Air Command from 1969 before conversion to F-111G and transferred to Air Combat Command (ACC) until their retirement in 1993. At a ceremony marking the F-111's USAF retirement, on 27 July 1996, it was officially named Aardvark, its long-standing unofficial name. The USAF retired
17920-453: The military lacked capability outside these narrow confines. The U.S. Department of Defense responded by accelerating its Rapid Deployment Forces concept but suffered from major problems with airlift and sealift capability. In order to slow an enemy invasion of other countries, air power was critical; however the key Iran-Afghanistan border was outside the range of the United States Navy 's carrier-based attack aircraft, leaving this role to
18080-414: The mission (e.g., en route to mission area or returning to base). When designated as the mission commander (MC), the WSO is also responsible for all phases of the assigned mission, especially if there are multiple aircraft involved. For example, the aircraft pilot could be the junior member of a flight crew such as a first lieutenant or captain, and the weapon systems officer could be a senior officer such as
18240-467: The new Triple Plow II intakes, which were located four inches (100 mm) further away from the airframe to prevent engine ingestion of the sluggish boundary layer air that was known to cause stalls in the TF30 turbofans. It had more powerful TF30-P-9 engines with 12,000 lbf (53 kN) dry and 18,500 lbf (82 kN) afterburning thrust. Rockwell B-1 Lancer The Rockwell B-1 Lancer
18400-455: The new aircraft was beginning to show; F-111s flew more than 4,000 combat missions in Vietnam with only six combat losses. From 30 July 1973, F-111As of the 347th Tactical Fighter Wing (347th TFW) were stationed at Takhli Air Base. The 347th TFW conducted bombing missions in Cambodia in support of Khmer Republic forces until 15 August 1973 when US combat support ceased in accordance with
18560-414: The nose are part of an active vibration damping system that smooths out the otherwise bumpy low-altitude ride. The first three B-1As featured the escape capsule that ejected the cockpit with all four crew members inside. The fourth B-1A was equipped with a conventional ejection seat for each crew member. The B-1A mockup review occurred in late October 1971; this resulted in 297 requests for alteration to
18720-404: The nose of the aardvark . The origin of the name has been attributed to F-111A Instructor Pilot Al Mateczun in 1969, as the aircraft had not received an official USAF name. During September 1972, the F-111 returned to Southeast Asia, stationed at Takhli Air Base , Thailand. F-111As from Nellis AFB participated in the final month of Operation Linebacker and later flew 154 low-level missions in
18880-509: The only effective anti-bomber weapon in the 1950s, were already unable to intercept the high-flying Lockheed U-2 ; the Valkyrie would fly at similar altitudes, but much higher speeds, and was expected to fly right by the fighters. By the late 1950s, however, anti-aircraft surface-to-air missiles (SAMs) could threaten high-altitude aircraft, as demonstrated by the 1960 downing of Gary Powers ' U-2. The USAF Strategic Air Command (SAC)
19040-405: The penetrating bunker-buster GBU-28 . Eighteen F-111Es were also deployed during the operation. The US Air Force credited F-111s with destroying more than 1,500 Iraqi tanks and armored vehicles. Their use in the anti-armor role was dubbed " tank plinking ". Expensive to operate—Crandall said that the aircraft "was nine percent of Tactical Air Command's fleet but ate up a whopping 25 percent of
19200-454: The program were enacted throughout 1965; this was chiefly in response to a steep climb in unit costs from $ 4.5 million to $ 6 million. The cause of the cost rises has been attributed, at least partially, to a directive issued to General Dynamics to incorporate improved avionics as well as to work on strategic bomber and aerial reconnaissance variants of the aircraft, the latter of which was eventually cancelled. During April 1965, General Dynamics
19360-400: The project as Advanced Manned Strategic Aircraft (AMSA), which differed from AMPSS primarily in that it also demanded a high-speed high-altitude capability, similar to that of the existing Mach 2-class F-111. Given the lengthy series of design studies, North American Rockwell engineers joked that the new name actually stood for "America's Most Studied Aircraft". The arguments that led to
19520-502: 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 he decided that this was a better approach than the B-1. Pentagon officials also stated that the AGM-86 Air-Launched Cruise Missile (ALCM) launched from the existing B-52 fleet would give
19680-528: The proposals lacking, but Boeing and General Dynamics were selected to submit enhanced designs. Boeing's proposal was recommended by the selection board in January 1962, with the exception of the engine, which was not considered acceptable. Switching to a crew escape capsule, instead of ejection seats and alterations to radar and missile storage were also needed. Both companies provided updated proposals in April 1962. USAF reviewers favored Boeing's offering, while
19840-400: The pylons. Auxiliary fuel drop tanks with 600 US gallons (2,300 litres) capacity each could be fitted. The design of the F-111's fuselage prevented the carriage of external weapons under the fuselage, but two stations were available on the underside for electronic countermeasures (ECM) pods and/or datalink pods; one station was on the weapons bay, and the other on the rear fuselage between
20000-423: The remaining fleet of F-111As revealed 42 aircraft with the same potential failures. It is speculated that this failure could also have contributed to the two earlier losses had the failure caused a pitch down while at low altitude. It was not until 1971 that 474 TFW was fully operational. The word "aardvark" is Afrikaans for "earthpig" and reflects the look of the long nose of the aircraft that might remind one of
20160-473: The required Mach 2 performance at high altitudes, the exhaust nozzles and air intake ramps were 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. The low altitude performance requirement was later lowered to Mach 0.85, reducing the amount of titanium and therefore cost. A pair of small vanes mounted near
20320-684: The responsibility for flying the aircraft in tactical situations. However, the crews of dedicated bomber aircraft usually retain distinct, rigidly-defined and conventional roles. In the Royal Air Force , a WSO is a commissioned officer that operates aircraft mission systems formerly on the Tornado GR4 , Sentinel R1 and Boeing E-3 Sentry , however now on the Reaper MQ-9A drone, the RC-135W Rivet Joint , Shadow R1, and
20480-411: The rigorous training ahead. Then the SNFO starts the U.S. Navy indoctrination course called Aviation Preflight Indoctrination (API) with their student naval aviator (pilot) counterparts. After six weeks of ground school and basic water survival training during API, future SWSOs (Student WSOs), at that point known as student naval flight officers (SNFO) check into the primary Training Squadron for SNFOs,
20640-654: The same conventional ordnance as the tactical variants, but their wing pylons were more commonly used for either fuel tanks or strategic nuclear gravity bombs. They could carry up to four AGM-69 SRAM nuclear missiles on the pylons. The F-111 was the first production variable-geometry wing aircraft. Several other types have followed with similar swing-wing configuration, including the Soviet Sukhoi Su-17 "Fitter" (1965), Mikoyan-Gurevich MiG-23 "Flogger" (1967), Tupolev Tu-22M "Backfire" (1969), Sukhoi Su-24 "Fencer" (1970) and Tupolev Tu-160 "Blackjack" (1981);
20800-524: The south east United States. After completion of the syllabus, track selection takes place. Navy SWSOs select either the F/A-18F Super Hornet, or the E/A-18 Growler. Marine SWSOs by default select the F/A-18D Hornet. The final three months of some of the hardest training at Pensacola will leave the SWSO F/A-18 selectee with their wings of gold. Air Force WSOs no longer train at VT-86. Following
20960-548: The surrounding areas. The counterpart course for USN and USMC WSOs is taught at NAS North Island (academics) and Warner Springs, California (field exercise) for Pacific Fleet personnel and at Brunswick, Maine for Atlantic Fleet personnel. IFF USAF WSOs selected for the F-15E learn basic fighter maneuvers (BFM) and surface attack in the T-38C at Introduction to Fighter Fundamentals (IFF). WSOs complete this training at either
21120-508: The vodka and caviar in Moscow." However, it appears the Soviets were more concerned by large numbers of ALCMs representing a much greater threat than a smaller number of B-1s. Soviet news agency TASS commented that "the implementation of these militaristic plans has seriously complicated efforts for the limitation of the strategic arms race." Western military leaders were generally happy with
21280-580: The weapon systems officer could be a senior officer such as a USN lieutenant commander, commander or captain, or a USMC major, lieutenant colonel, or colonel; this would likely make the WSO the mission commander. As of 2021, the USMC is moving away from the use of the F/A-18 Hornet to the F-35 which does not utilize the WSO position. Hence the last class of USMC WSO's graduated from NAS Pensacola in 2021. In
21440-429: The winging ceremony, USN and USMC WSOs will proceed to a Fleet Replacement Squadron (FRS) and USAF WSOs to a Formal Training Unit (FTU) to complete advanced ground school and flight training to prepare them for their "operational" combat aircraft in the deployable operating forces. Parachuting water survival All USAF aviators with parachutes on the aircraft attend this three-day course at NAS Pensacola, Florida. During
21600-419: Was NASA's simplification which made the variable geometry wings practical. By 1960, increases in aircraft weights required improved high-lift devices , such as variable geometry wings. Variable geometry offered high speeds, and maneuverability with heavier payloads , long range, and the ability to take off and land in shorter distances. The USAF and Navy were both seeking new aircraft when Robert McNamara
21760-452: Was also included in the specification. In the 1950s, the United States Navy sought a long-range, high-endurance interceptor aircraft to protect its carrier battle groups against long-range anti-ship missiles launched from Soviet jet bombers and submarines. The Navy needed a fleet air defense (FAD) fighter with a more powerful radar, and longer range missiles than the F-4 Phantom II to intercept both enemy bombers and missiles. Seeking
21920-403: Was an all-moving stabilator . The F-111 used a three-point landing gear arrangement, with a two-wheel nose gear and two single-wheel main landing gear units. The landing gear door for the main gear, which was positioned in the center of the fuselage, also served as a speed brake in flight. Most F-111 variants included a terrain-following radar system connected to the autopilot. The aircraft
22080-404: Was an upgraded F-111A equipped with newer Mark II avionics, more powerful engines, improved intake geometry, and an early glass cockpit . It was first ordered in 1967 and delivered from 1970–73 after delays due to avionics issues. The F-111D reached initial operational capability in 1972; the sole operator was the 27th TFW stationed at Cannon AFB , New Mexico. 96 were built. The F-111D used
22240-433: Was appointed secretary of defense in January 1961. The aircraft sought by the two armed services shared the need to carry heavy armament and fuel loads, feature high supersonic speed, twin engines and two seats, and probably use variable geometry wings. On 14 February 1961, McNamara formally directed the services to study the development of a single aircraft that would satisfy both requirements. Early studies indicated that
22400-518: Was authorized to produce 431 F-111s, less than half the number of aircraft which had originally been forecast. On 10 May 1967, a new multi-year FPIP contract replaced the prior procurement process, increasing the total aircraft on order to 493 F-111s of multiple models, including 23 F-111Bs intended for the US Navy, 24 F-111Cs for the Royal Australian Air Force , and 50 F-111Ks intended for the Royal Air Force . Early flights of
22560-562: Was awarded the development contract. The original program called for two test airframes, five flyable aircraft, and 40 engines. This was cut in 1971 to one ground and three flight test aircraft. The company changed its name to Rockwell International and named its aircraft division North American Aircraft Operations in 1973. A fourth prototype, built to production standards, was ordered in the fiscal year 1976 budget. Plans called for 240 B-1As to be built, with initial operational capability set for 1979. Rockwell's design had features common to
22720-467: Was aware of these developments and had begun moving its bombers to low-level penetration even before the U-2 incident. This tactic greatly reduces radar detection distances through the use of terrain masking ; using features of the terrain like hills and valleys, the line-of-sight from the radar to the bomber can be broken, rendering the radar (and human observers) incapable of seeing it. Additionally, radars of
22880-504: Was believed the B-1 could be in operation before the ATB, covering the transitional period between the B-52's increasing vulnerability and the ATB's introduction. Reagan decided the best solution was to procure both the B-1 and ATB, and on 2 October 1981 he announced that 100 B-1s were to be ordered to fill the LRCA role. In January 1982, the U.S. Air Force awarded two contracts to Rockwell worth
23040-630: Was canceled in 1977 due to its high cost, the introduction of the AGM-86 cruise missile that flew the same basic speed and distance, and early work on the B-2 stealth bomber. The program was restarted in 1981, largely as an interim measure due to delays in the B-2 stealth bomber program. The B-1A design was altered, reducing top speed to Mach 1.25 at high altitude , increasing low-altitude speed to Mach 0.96, extensively improving electronic components, and upgrading
23200-428: Was completed, which called for an aircraft with a 20,000-pound (9,100 kg) bomb load and somewhat shorter range of 8,230 miles (13,240 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 (later North American Rockwell ). In mid-1964, the USAF had revised its requirements and retitled
23360-961: Was delivered on 2 May 1988; before the last B-1B was delivered, the USAF had determined that the aircraft was vulnerable to Soviet air defenses. In 1996, Rockwell International sold most of its space and defense operations to Boeing, which continues as the primary contractor for the B‑;1 as of 2024. The B-1 has a blended wing body configuration, with variable-sweep wing , four turbofan engines , triangular ride-control fins and cruciform tail . The wings can sweep from 15 degrees to 67.5 degrees (full forward to full sweep). Forward-swept wing settings are used for takeoff , landings and high-altitude economical cruise . Aft-swept wing settings are used in high subsonic and supersonic flight. The B-1's variable-sweep wings and thrust-to-weight ratio provide it with improved takeoff performance, allowing it to use shorter runways than previous bombers. The length of
23520-463: 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. Studies suggested that the existing B-52 fleet with ALCM would remain a credible threat until 1985. It was predicted that 75% of the B-52 force would survive to attack its targets. After 1985, the introduction of the SA-10 missile,
23680-404: Was followed by the similar Extended Range Strike Aircraft (ERSA), which added a variable-sweep wing , then en vogue in the aviation industry. ERSA envisioned a relatively small aircraft with a 10,000-pound (4,500 kg) payload and a range of 10,070 miles (16,210 km) including 2,900 miles (4,700 km) flown at low altitudes. In August 1963, the similar Low-Altitude Manned Penetrator design
23840-473: Was lost over Libya and crashed into the Mediterranean Sea, probably shot down. F-111s participated in the Gulf War (Operation Desert Storm) in 1991. During Desert Storm, F-111Fs completed 3.2 successful strike missions for every unsuccessful one, better than any other U.S. strike aircraft used in the operation. The group of 66 F-111Fs dropped almost 80% of the war's laser-guided bombs, including
24000-560: Was made public with the program being top secret , but it is now known that in early 1978 he authorized the Advanced Technology Bomber (ATB) project, which eventually led to the B-2 Spirit . Domestically, the reaction to the cancellation was split along partisan lines. The Department of Defense was surprised by the announcement; it expected that the number of B-1s ordered would be reduced to around 150. Congressman Robert Dornan (R-CA) claimed, "They're breaking out
24160-588: Was outfitted for conventional bombing. It first served in combat during Operation Desert Fox in 1998 and again during the NATO action in Kosovo the following year. The B-1B has supported U.S. and NATO military forces in Afghanistan and Iraq . As of 2021 the Air Force has 45 B-1Bs. The Northrop Grumman B-21 Raider is to begin replacing the B-1B after 2025; all B-1s are planned to be retired by 2036. In 1955,
24320-474: Was part of an escape crew capsule . The wing sweep varied between 16 degrees and 72.5 degrees (full forward to full sweep). The wing included leading edge slats and double slotted flaps over its full length. The airframe was made up mostly of aluminum alloys with steel, titanium and other materials used in places. The fuselage was made of a semi- monocoque structure with stiffened panels and honeycomb structure panels for skin. The horizontal stabilizer
24480-498: Was powered by two Pratt & Whitney TF30 afterburning turbofan engines. The F-111's variable-geometry wings, escape capsule, terrain following radar and afterburning turbofans were new technologies for production aircraft. The F-111 featured an internal weapons bay that could carry bombs, a removable 20 mm M61 cannon or auxiliary fuel tanks. For bombs, the bay could hold two 750 lb (340 kg) M117 conventional bombs, one nuclear bomb or practice bombs. The F-111B for
24640-745: Was reached by the second B-1A. Engine testing also continued during this time with the YF101 engines totaling almost 7,600 hours. It was during this period that the Soviets started to assert themselves in several new theaters of action, in particular through Cuban proxies during the Angolan Civil War starting in 1975 and the Soviet invasion of Afghanistan in 1979. U.S. strategy to this point had been focused on containing Communism and preparation for war in Europe. The new Soviet actions revealed that
24800-403: Was repeatedly postponed before being cancelled, having been deemed to be unnecessary. During 1968, the F-111B was canceled by the Navy on account of weight and performance issues together with revised tactical requirements. Australia would procure its own model, the F-111C. Subsequently, the improved F-111E, F-111D, and F-111F models were developed for the USAF. The strategic bomber FB-111A and
24960-434: Was seen as a good trade off for the speed decrease. High subsonic speeds at low altitude became a focus area for the revised design, and low-level speeds were increased from about Mach 0.85 to 0.92. The B-1B has a maximum speed of Mach 1.25 at higher altitudes. The B-1B's maximum takeoff weight was increased to 477,000 pounds (216,000 kg) from the B-1A's 395,000 pounds (179,000 kg). The weight increase
25120-478: Was significantly upgraded. Opposition to the plan was widespread within Congress. Critics pointed out that many of the original problems remained in both areas of performance and expense. In particular it seemed the B-52 fitted 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
25280-522: Was the supersonic F-111 fighter-bomber, which used variable-sweep wings for tactical missions. A number of studies on a strategic-range counterpart followed. The first post-B-70 strategic penetrator study was known as the Subsonic Low-Altitude Bomber (SLAB), which was completed in 1961. This produced a design that looked more like an airliner than a bomber, with a large swept wing, T-tail , and large high-bypass engines . This
25440-423: Was to allow for takeoff with a full internal fuel load and for external weapons to be carried. Rockwell engineers were able to reinforce critical areas and lighten non-critical areas of the airframe, so the increase in empty weight was minimal. To deal with the introduction of the MiG-31 equipped with the new Zaslon radar system, and other aircraft with look-down capability, the B-1B's electronic warfare suite
25600-400: Was to be at a speed of no less than Mach 1.2. Furthermore, the specification also called for the aircraft to possess short takeoff and landing (STOL) capabilities to permit operations from short, unprepared airstrips that had a length of no more than 3,000 feet. An internal payload of 1,000lb was to be carried in the primary mission role. A variant suitable for aerial reconnaissance flights
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