The Saab 37 Viggen is a retired Swedish single-seat, single-engine, short-medium range combat aircraft. Development work on the type was initiated at Saab in 1952 and, following the selection of a radical delta wing configuration, the resulting aircraft performed its first flight on 8 February 1967 and entered service in 21 June 1971. It was the first canard design produced in quantity. The Viggen was also the most advanced[vague] fighter jet in Europe until the introduction of the Panavia Tornado into operational service in 1981.

Several distinct variants of the Viggen were produced to perform the roles of strike fighter (AJ 37), aerial reconnaissance (SF 37), maritime patrol aircraft (SH 37) and a two-seat trainer (SK 37). In the late 1970s, the all-weather fighter-interceptor aircraft JA 37 variant was introduced. In November 2005, the Viggen was retired from service by the Swedish Air Force, the only operator, having been replaced by the newer Saab JAS 39 Gripen.

The Viggen was powered by a single Volvo RM8 turbofan. This was essentially a licence-built variant of the Pratt & Whitney JT8D engine that powered commercial airliners of the 1960s, with an afterburner added for the Viggen. The airframe also incorporated a thrust reverser to use during landings and land manoeuvres, which, combined with the aircraft having flight capabilities approaching a limited STOL-like performance, enabled operations from 500 m airstrips with minimal support. The thrust reverser could be pre-selected in the air to engage when the nose-wheel strut was compressed after touchdown via a pneumatic trigger.

For furthr details on the origins, development and design, and operational history, clcik here.

The Gripen has a delta wing and canard configuration with relaxed stability design and fly-by-wire flight controls. Various versions have been built, grouped as A-, C- and E-series.

Gripen A- and C-series are powered by the GE F404G engine (previously designated Volvo RM12) and the E-series is powered by the GE F414G engine, and has a top speed of Mach 2. Later aircraft are modified for NATO interoperability standards and to undertake air to air refuelling.

The Gripen is a multirole fighter aircraft, intended as a light-weight and agile aerial platform with advanced, highly adaptable avionics. It has canard control surfaces that contribute a positive lift force at all speeds, while the generous lift from the delta wing compensates for the rear stabiliser producing negative lift at high speeds, increasing induced drag. Being intentionally unstable and employing digital fly-by-wire flight controls to maintain stability removes many flight restrictions, improves manoeuvrability, and reduces drag. The Gripen also has good short takeoff performance, being able to maintain a high sink rate and strengthened to withstand the stresses of short landings. A pair of air brakes are located on the sides of the rear fuselage; the canards also angle downward to act as air brakes and decrease landing distance. It is capable of flying at a 70–80 degrees angle of attack.

For details of the development, design, operational history and variants, click here.

Specifications below are for the JAS 39C and 39D models, variances highlighted.

In February of 2019, the Pakistan Air Force launched retaliatory airstrikes on Indian military installations at Indian Administered Jammu and Kashmir in response to India's violation of Pakistani airspace and the bombing of a wooded area at Balakot. While fighter jets from various PAF squadrons executed the airstrikes, Saab-2000 Erieye AWACS along with DA-20 EW supported them throughout the operation.

The Erieye AEW&C mission system radar is an active, phased-array, pulse-doppler sensor that can feed an onboard operator architecture or downlink data (via an associated datalink subsystem) to a ground-based air defence network. The system employs a large aperture, dual-sided antenna array housed in a dorsal 'plank' fairing. The antenna is fixed, and the beam is electronically scanned, which provides for improved detection and significantly enhanced tracking performance compared with radar-dome antenna systems. Erieye detects and tracks air and sea targets out to the horizon, and sometimes beyond this due to anomalous propagation — instrumented range has been measured at 450 kilometres (280 mi). Typical detection range against fighter-sized targets is approximately 425 kilometres (264 mi), in a 150° broadside sector, both sides of the aircraft. Outside these sectors, performance is reduced in forward and aft directions.

Other system features include: Adaptive waveform generation (including digital, phase-coded pulse compression); Signal processing and target tracking; track while scan (TWS); low side lobe values (throughout the system's angular coverage); low- and medium-pulse repetition frequency operating modes; frequency agility; Air-to-air and sea surveillance modes; and target radar cross-section display.

It is still in service in upgraded form with the Indian Air Force.

Originally conceived in the 1960s as a jet trainer with a light ground attack capability, the requirement for the aircraft soon changed to include supersonic performance, reconnaissance and tactical nuclear strike roles. A carrier-based variant was also planned for French Navy service, but this was cancelled in favour of the cheaper Dassault Super Étendard. The aircraft were manufactured by SEPECAT (Société Européenne de Production de l'avion Ecole de Combat et d'Appui Tactique), a joint venture between Breguet and the British Aircraft Corporation, one of the first major joint-Anglo-French military aircraft programmes.

The Jaguar is an orthodox single-seat, swept-wing, twin-engine monoplane design, with tall tricycle-type retractable landing gear. In its original configuration, it had a maximum take-off weight in the 15 tonne class; and could manage a combat radius on internal fuel alone of 850 km (530 mi), giving the Jaguar a greater operational range than competitor aircraft such as the Mikoyan MiG-27. The aircraft had hardpoints fitted for an external weapons load of up to 10,000 lb (4,500 kg), typical weapons fitted included the MATRA LR.F2 rocket pod, BAP 100-mm bombs, MATRA AS37 anti-radar missiles, AIM-9 Sidewinder missiles, and Rockeye cluster bombs. The RAF's Jaguars gained several new weapons during the Gulf War, including CRV7 high-velocity rockets and American CBU-87 cluster bombs. Finally, the Jaguar was equipped with either a pair of French DEFA cannons, or alternatively British ADEN cannons.

For details of operational history and variants, click here.

The Shaanxi Y-8 or Yunshuji-8 (Chinese: 运-8; pinyin: Yùn Bā) aircraft is a medium size medium range transport aircraft produced by Shaanxi Aircraft Corporation in China, based on the Soviet Antonov An-12. It has become one of China's most popular military and civilian transport/cargo aircraft, with many variants produced and exported. Although the An-12 is no longer made in Ukraine, the Chinese Y-8 continues to be upgraded and produced. An estimated 169 Y-8 aircraft had been built by 2010.

In the 1960s, China purchased several An-12 aircraft from the Soviet Union, along with license to assemble the aircraft locally. However, due to the Sino-Soviet split, the Soviet Union withdrew its technical assistance. The Xi'an Aircraft Company and Xi'an Aircraft Design Institute worked to reverse engineer the An-12 for local production.

Design of the aircraft was completed by February 1972. Major features of the Y-8 included a glazed nose and tail turret derived from that of the H-6 bomber, a roller-type palletized-cargo-handling device instead of the overhead conveyor, and a gaseous oxygen system as opposed to a liquid oxygen system. The original Y-8 inherited the An-12's twin 23mm cannon tail turret, but this was removed on subsequent variants.

The Y-8 equipped with four turboprop engines mounted under the leading edges of non-swept wings. The wings are attached high on the fuselage, and the tricycle landing gear is equipped with low pressure tires. The earliest versions used for the transportation of freight or troops had two side-hinged, inward-opening doors, while later variants used a rearward-facing ramp to facilitate loading and unloading of the payload. Some specialized versions omit the cargo ramp entirely.

The Y-8 is capable of carrying troops, dropping supplies, parachute drops, and functioning as an air ambulance. It also can be used for commercial uses as a freighter. It is capable of hauling 20 tons of cargo, approximately 96 soldiers, or about 82 paratroopers in the cargo compartment which is 13.5 metres long, 3 metres wide and 2.4 metres high. It can also carry 60 severely wounded soldiers with their stretchers, 20 slightly injured soldiers and 3 medical attendants. Many variants for specialized roles have been built, but information on them can be vague or difficult to obtain due to the secretive nature of the Chinese military.

For more information on the development, operational history and 44 variants of the Pegasus, click here.

The Shenyang FC-31 Gyrfalcon (Chinese: 鹘鹰; pinyin: Gǔ yīng), also known as the J-31 or J-35, is a Chinese prototype mid-sized twinjet 5th-generation fighter aircraft developed by Shenyang Aircraft Corporation (SAC). The official nickname published by SAC is "Gyrfalcon", though it has also been referred to as the "F-60" or "J-21 Snowy Owl" (Chinese: 雪鸮) in some media reports, or "Falcon Hawk" by some military enthusiasts. J-XX nomenclatures in the Chinese military are reserved for programs launched and financed by the People's Liberation Army, while the FC-31 plane was developed independently as a private venture by the aircraft manufacturer.

While the Chengdu J-20 stealth fighter was officially endorsed by the People's Liberation Army Air Force after Chengdu Aerospace Corporation's proposal won the PLAAF bid for the next-generation jet fighter, Shenyang Aircraft Corporation pressed on and developed a private project aiming to secure potential export customers.

A photo of a model labeled F-60 was posted on the Internet in September 2011. In June 2012, photos and phone camera video clips started to emerge on internet regarding a heavily overwrapped fighter plane airframe (widely suspected to be the F-60 prototype) being road-transferred on a highway, earning the nickname "the zongzi plane" (Chinese: 粽子机) among Chinese netizens, though some suspect it of merely being an L-15 trainer aircraft. Pictures of a possibly fully assembled aircraft parking on an airfield emerged on 15 or 16 September 2012. The F-60 is reported to be the export version, where the J-31 would be the domestic Chinese version of the same fighter. Chinese aviation expert Xu Yongling has called the J-31 an export-oriented low-end latest generation warplane.

It is very likely that the J-31 will be inducted as a carrier-based naval fighter. In an interview with China's state-run media, FC-31's chief designer Sun Cong expressed that the aircraft would follow his J-15 onto China's aircraft carriers. However, officials from AVIC only said that the aircraft was intended for export as a competitor to the   

F-35. There has also been reports that the PLAN has urged Shenyang to develop a carrier-compatible version of 

J-31. 

In 2015, Jiangsu A-Star Aviation Industries Company marketed its EOTS-86 infra-red search and track as a possible addition to the J-31. An improved prototype, with modifications to the vertical stabilizers, wings, and airframe, an electro-optical targeting system, a larger payload, improvements in stealth, and upgraded electronics, made its maiden flight in December 2016.

In November 2018, an Aviation Week article stated that the FC-31 program has received government funding and is being sought after by both the PLANAF and PLAAF, according to official sources. In June 2020, reports surfaced that a third variant of FC-31, albeit a more production-ready version with smoother lines, a bigger radome for a bigger radar, and a closer alignment of control surfaces to reduce the radar signature, had been developed. The "new fighter" has been referred to by some as J-35.

On October 29, 2021, the modified carrier-based variant of the FC-31, dubbed J-35 by commentators, made its maiden flight. It is intended to operate from the forthcoming Type 003 aircraft carrier with an electromagnetic catapult system. The naval variant is based on the second prototype of the FC-31, but also includes a catapult launch bar and a folding wing mechanism.

For further details, click here.

The Shenyang J-15 (Chinese: 歼-15; pinyin: Jiān-Shíwǔ), also known as Feisha (Chinese: 飞鲨; pinyin: fēi shā; lit. 'Flying Shark'; NATO reporting name: Flanker-X2, Flanker-K) is a Chinese all-weather, twin-engine, carrier-based 4.5 generation multirole fighter aircraft developed by the Shenyang Aircraft Corporation (SAC) and the 601 Institute, specifically for the People's Liberation Army Naval Air Force (PLANAF) to serve on People's Liberation Army Navy's (PLAN) aircraft carriers.

The aircraft entered active service with the PLAN in 2013. An improved variant, named J-15T, incorporating CATOBAR launch capability, modern fifth-generation avionics, entered active service in the South China Sea in October 2024.

In 2001, the T-10K-3, an unfinished prototype of the Su-33, was acquired by SAC from Ukraine[8] and is claimed to have been studied extensively and reverse-engineered, with development on the J-15 beginning immediately afterward.

China had sought to purchase Su-33s from Russia on several occasions—an unsuccessful offer was made as late as March 2009—but negotiations collapsed in 2006 after it was discovered that China had developed a modified version of the Sukhoi Su-27SK, designated the Shenyang J-11B, in violation of intellectual property agreements.

However, according to Chinese sources, the reason China withdrew from talks was that Russia wanted large payments to re-open Su-33 production lines and insisted on a Chinese purchase of at least 50 Su-33s, about which China was reluctant, as it believed the aircraft would become outdated in a few years. China hence decided on an indigenous variant instead of continuing to assemble the J-11, the licensed Chinese version of Su-27.

The J-15 program was officially started in 2006 with the codename Flying Shark. The program goal was to develop a naval-capable fighter aircraft from the Shenyang J-11, with technologies reverse-engineered from T-10K-3, a Soviet Su-33 prototype that had been acquired from Ukraine. The first J-15 prototype made its maiden flight on August 31, 2009, believed to have been powered by Russian-supplied Saturn AL-31 turbofan engines. Video and still images of the flight were released in July 2010, showing the same basic airframe design as the Su-33.

On May 7, 2010, the aircraft conducted its first takeoff from a simulated ski-jump on land. On November 25, 2012, the aircraft successfully performed its first takeoff and landing on Liaoning, China's first operational aircraft carrier. The twin-seat variant, J-15S, made its maiden flight on November 4, 2012.

After conclusion of the flight-test phase, in 2013 the first 24 J-15 aircraft were delivered to the Naval Aviation’s Carrier Fighter Group.

For more details of development, design, operational history, and 5 variants, click here.

The Short Belfast (or Shorts Belfast) is a heavy lift turboprop freighter that was built by British manufacturer Short Brothers at Belfast.

Only 10 aircraft were constructed, all of which entered service with the Royal Air Force (RAF), who operated it under the designation Short Belfast C.1.

Upon its entry into service, the Belfast held the distinction of becoming the largest aircraft that the British military had ever operated up to that time. It was also notable for being the first aircraft to be designed from the onset to be equipped with full 'blind landing' automatic landing system equipment. Following the formation of RAF Strike Command and a reorganisation of transport assets, the RAF decided to retire all of its Belfast transports by the end of 1976.

Shortly after the type had been retired by the RAF, five Belfasts were sold and placed into civilian service with the cargo airline TAC HeavyLift. These civilian aircraft were used for the charter transport of various goods, including to the RAF. One Belfast is on display at the RAF Museum Cosford. A Belfast formerly operated by Heavylift Cargo is lying abandoned at Cairns Airport in Australia and is the subject of a legal dispute for fees between the airport and the current owner of the aircraft, Flying Tigers.

The Short Belfast was a large heavy-lift strategic transport aircraft. It featured a high-mounted wing, which carried a total of four Rolls-Royce Tyne turboprop engines. According to aerospace publication Flight International, the design of the assemblies of the surfaces of both the tail and wing of the Belfast had been derived from the Bristol Britannia. One of the major changes to the wing was its conversion to a wet wing, which was performed by Canadair. There are few other common elements between the Belfast and the Britannia, although there had been a much greater proportion intended during initial designs for the aircraft.

For more details of the development, design and operational history of the Belfast, click here.

The SIAI-Marchetti S.211 (later Aermacchi S-211) is a turbofan-powered military trainer aircraft designed and originally marketed by Italian aviation manufacturer SIAI-Marchetti.

SIAI-Marchetti started to develop the S-211 in 1976 as a private venture initiative, announcing its existence during the following year. On 10 April 1981, the first prototype performed its maiden flight. The Singapore Air Force placed the first order for ten aircraft in 1983. Some 60 aircraft have been sold to air forces around the world. Following Aermacchi's purchase of SIAI-Marchetti in 1997, the former has held the production rights to the type. An extensively redesigned and modernised derivative, the Aermacchi M-345, has been developed by Alenia Aermacchi, and is set to enter service during 2020.

During 1976, Italian aircraft company SIAI-Marchetti commenced work on what would become the S-211; the project was undertaken as a private venture to develop a new basic trainer aircraft. SIAI-Marchetti planned to offer the type to the company's existing customer base, consisting of various air forces around the world that operated their SF.260, a piston-engined trainer. The programme's existence was formally announced in Paris during 1977, reportedly, customer interest was strong enough to justify the construction of two prototypes, the first of which flew on 10 April 1981. During 1983, the Singapore Air Force placed the first order for the S-211, procuring a batch of ten aircraft.

The S-211A was a slightly modified and updated variant of the S-211, was a losing contender in the United States Air Force's Joint Primary Aircraft Training System (JPATS) aircraft selection. Among the seven aircraft to enter, the Raytheon/Pilatus entry emerged as the winner, being produced as the T-6 Texan II. The S-211 team was initially partnered with American aircraft company Grumman; following its merger with Northrop Corporation in 1994, SIAI-Marchetti worked with Northrop Grumman on the S-211A up until the selection.

The S-211 is a compact two-seat shoulder-wing monoplane, possessing a full aerobatic capability. It is furnished with a retractable tricycle landing gear and is powered by a single Pratt & Whitney Canada JT15D-4C turbofan powerplant. The S-211 has been principally used as a basic trainer aircraft, the student and instructor being seated in a tandem arrangement; the front and rear cockpits are fully duplicated, the latter being elevated above the former to provide the occupant with improved forward visibility. Additionally, the aircraft was designed to perform a secondary close air support (CAS) capability, being equipped with four underwing hard points, facilitating the carriage of various armaments and other external stores, including sensor apparatus and photographic equipment for undertaking aerial reconnaissance missions. Some models feature an additional hard point on the underside of the fuselage.

The airframe is largely composed of several composite materials, which includes Kevlar, Nomex and carbon fibre, while extensive use of structural bonding was made during construction. The flight controls feature manually operated push-pull rod primary controls; many other systems, such as the air brake, landing gear, compressor, and boosted ailerons, are hydraulically-actuated at a nominal operating pressure of 200 bar (3,000 psi).

21 ex-RSAF S-211s were retired and sold to the IAP Group Australia in December 2009 (including a cannibalised airframe), fifteen have since been sold off and placed on the Australian civil registry. (Update: A check of the Australian Register on 09/11/2021 reveals 49 registered S.211's)

For more details of the development, design, operational history and variants, click here.

The Sikorsky CH-37 Mojave (company designation S-56) is an American large heavy-lift helicopter of the 1950s.

The S-56 came into being as an assault transport for the United States Marine Corps (USMC), with a capacity of 26 fully equipped Marines. An order for the aircraft was placed in 1951 using the U.S. Navy/U.S. Marine Corps designation of the time of HR2S. The first prototype, the XHR2S-1 flew in 1953 and production deliveries of the HR2S-1 began in July 1956 to Marine Helicopter Squadron One (HMX-1), with a total of sixty aircraft being produced.

The United States Army evaluated the prototype in 1954 and ordered 94 examples as the CH-37A, the first being delivered in summer 1956. All Marine Corps and Army examples were delivered by mid-1960. Army examples were all upgraded to CH-37B status in the early 1960s, being given Lear auto-stabilization equipment and the ability to load and unload while hovering. In the 1962 unification of United States military aircraft designations, the USMC examples were redesignated from HR2S-1 to CH-37C.

At the time of delivery, the CH-37 was the largest helicopter in the Western world and it was Sikorsky's first twin-engine helicopter. Two Pratt & Whitney R-2800 Double Wasp radial engines were mounted in outboard pods that also contained the retractable landing gear. This left the fuselage free for cargo, which could be loaded and unloaded through large clamshell doors in the nose. The early models could carry a payload of either three M422 Mighty Mites (a lightweight jeep-like vehicle) or 26 troops. For storage, the main rotor blades folded back on the fuselage and the tail rotor mast folded forward on the fuselage.

The CH-37 was one of the last heavy helicopters to use piston engines, which were larger, heavier and less powerful than the turboshaft engines subsequently employed in later military helicopters. This accounted for the type's fairly short service life, all being withdrawn from service by the late 1960s, replaced in Army service by the distantly related CH-54 Tarhe and in the Marine Corps by the CH-53 Sea Stallion.

Four CH-37Bs were deployed to Vietnam in September 1965 to assist in the recovery of downed U.S. aircraft, serving in this role from Marble Mountain Air Facility until May 1967.[2] They were very successful at this role, recovering over US$7.5 million worth of equipment, some of which was retrieved from behind enemy lines. The CH-37 was also used to recover film capsules descending from space by parachute.

Variants

XHR2S-1
Prototype Assault Transport for the US Marine Corps, powered by two 1,900 hp (1,400 kW) R-2800-54 engines, four built.
HR2S-1
Production model for USMC with modified engine nacelles, twin mainwheels and dorsal fin, redesignated CH-37C in 1962, 55 built (order for additional 36 cancelled).
HR2S-1W
Airborne early warning aircraft for the US Navy, two built.
YH-37
One HR2S-1 helicopter evaluated by the US Army.
H-37A Mojave
Military transport version of the HR2S for the US Army, changes included dorsal fin and modified rotor head fairing, redesignated CH-37A in 1962, 94 built.
H-37B Mojave
All but four of the H-37As were modified with a redesigned cargo door, automatic stabilization equipment and crashproof fuel cells. Later redesignated CH-37B.
CH-37A
H-37A redesignated in 1962.
CH-37B
H-37B redesignated in 1962.
CH-37C
HR2S-1 redesignated in 1962.
S-56
Sikorsky company designation for H-37.

Originally developed for use by the United States Marine Corps, it is currently in service with Germany, Iran, Israel, and Mexico. The United States Air Force operated the HH-53 "Super Jolly Green Giant" during the late– and post–Vietnam-War era, updating most of them as the MH-53 Pave Low.

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

The Sea Stallion has a fuselage design similar to, but much larger than, the Sikorsky S-61R series. It has a passenger door on the right side of the fuselage behind the cockpit and a power-operated rear loading ramp. The fuselage is watertight, though not intended for amphibious use, and is only intended to land on water in emergencies. The Stallion has mechanical flight controls which are backed by three independent hydraulic systems. Armor protects crew and vital systems. The CH-53A carries a crew of four; pilot, copilot, crew chief, and an aerial observer, a load of 38 troops, 24 litters with medical attendants, an internal cargo load of 8,000 pounds (3,600 kg) or an external load of 13,000 pounds (5,900 kg) on the single-point sling hook. The CH-53A is equipped with a pair of 7.62×51mm NATO M60 machine guns that point out to each side of the fuselage.

The CH-53A features a six-bladed main rotor and four-bladed tail rotor developed from those used on the S-64 Skycrane. To save space on board naval vessels, the tail boom and the rotors folded. Initially, the CH-53 was powered by twin General Electric T64-6 turboshaft engines providing 2,850 shaft horsepower (2,130 kW) each, each engine being located on the upper fuselage. 

The CH-53D features uprated engines, initially T64-GE-412 with 3,695 shp (2,755 kW) then the T64-413 with 3,925 shp (2,927 kW) with an uprated transmission. Its interior added seats to allow for 55 troops. CH-53Ds are generally armed with twin .50 BMG (12.7 mm) M2/XM218 machine guns. In later years, CH-53Ds have been fitted with defensive countermeasures including an AN/ALE-39 chaff dispenser and an AN/ALQ-157 infrared countermeasure.

For more details, including the 14 variants, click here.

Specifications below are for the CH-53D model.

The Sikorsky S-97 Raider is a high-speed scout and attack compound helicopter based on the Advancing Blade Concept (ABC) with a coaxial rotor system under development by Sikorsky Aircraft. Sikorsky planned to offer it for the United States Army's Armed Aerial Scout program, along with other possible uses. The S-97 made its maiden flight on 22 May 2015.

Sikorsky's earliest attempt at a fast compound helicopter with stiff coaxial rotors was the Sikorsky S-69 (XH-59A) flown in the 1970s. Its top speed was over 260 knots but its excessive fuel consumption, vibration and complexity requiring the full-time attention of two pilots led to the program's cancellation. These problems were largely solved on another attempt by the Sikorsky X2 technology demonstrator in 2010. First proposed in response to a Request for Information for the Armed Aerial Scout (AAS) program in March 2010, the S-97 was formally launched on 20 October 2010. It was intended as a contender for a United States Army's requirement to replace the Bell OH-58D Kiowa Warrior. Other military roles are possible, the U.S. Special Operations Command having expressed interest in the S-97 as a replacement for the MH-6 Little Bird, and the possibility of adapting it for civilian applications also exists.

Sikorsky plans to build two prototypes of the S-97 as demonstrators. One prototype (P1) will be used for flight testing, while the second (P2) is planned for use as a demonstrator. The first prototype was planned to fly in late 2013 or early 2014. Sikorsky started construction of the two prototypes in October 2012. In September 2013, Sikorsky began final assembly of the first S-97 following delivery of the single-piece, all-composite fuselage by Aurora Flight Sciences. In February 2014, construction of the first S-97 prototype was one-quarter complete. Simulated bird strikes testing had been conducted on the fuselage at speeds of up to 235 kn (435 km/h; 270 mph), the S-97's expected maximum flight speed. Drop tests were also performed to ensure the fuel tanks' safety in the event of a crash. Sikorsky is exploring civil applications for the S-97, such as transporting personnel between offshore oil platforms.

Sikorsky and partner Boeing are to use the S-97's technology and design process as a basis to develop the SB-1 Defiant, a high-speed rigid rotor co-axial rotorcraft, for the army's Joint Multi-Role Technology Demonstrator (JMR TD) program. The JMR TD is the precursor to the army's estimated US$100 billion Future Vertical Lift (FVL) program to replace the UH-60 Black Hawk utility helicopter and AH-64 Apache attack helicopter.

Sikorsky targeted the S-97 for the AAS program, aiming for the helicopter to fly before the Army downselected. Sikorsky invested $150 million and its 54 suppliers[16] (who provide 90% of the parts) spent the remainder of a total of $200 million on two prototypes; production models aim to meet the program's $15 million unit cost target. However, the Army ended the AAS program in late 2013. Budget projections for FY 2015 included retiring the U.S. Army's OH-58 Kiowa fleet and transferring AH-64 Apache attack helicopters from U.S. Army Reserve and U.S. Army National Guard to the active Army to perform the aerial scout role. Sikorsky suggested the possibility of buying the S-97 to replace lost Apache for armed helicopter needs. Sikorsky proposes S-97 as FVL-CS1; the light scout helicopter.

On 5 May 2014, Sikorsky opened the S-97 production hangar during the rollout of the CH-53K King Stallion. At that point, the mostly-composite airframe was almost assembled, including some of the electrical wiring and avionics, missing elements were the transmission, drive train, engine, coaxial rotor, and pusher propeller. The S-97's first military customer is aimed to be the U.S. Special Operations Command to replace the MH-6M Little Bird. Unspecified foreign militaries have shown interest in the S-97; it may be difficult to get approval for export for a next-generation helicopter if the US military does not yet have it. The Raider is a prototype, so the first customer would need to finance a production development program. Its avionics were powered on in June 2014, with rollout on 2 October 2014.

For details of design and operational history, click here.

Sikorsky submitted the S-70 design for the United States Army's Utility Tactical Transport Aircraft System (UTTAS) competition in 1972. The Army designated the prototype as the YUH-60A and selected the Black Hawk as the winner of the program in 1976, after a fly-off competition with the Boeing Vertol YUH-61.

Named after the Native American war leader Black Hawk, the UH-60A entered service with the U.S. Army in 1979, to replace the Bell UH-1 Iroquois as the Army's tactical transport helicopter. This was followed by the fielding of electronic warfare and special operations variants of the Black Hawk. Improved UH-60L and UH-60M utility variants have also been developed. Modified versions have also been developed for the U.S. Navy, Air Force, and Coast Guard. In addition to U.S. Army use, the UH-60 family has been exported to several nations. Black Hawks have served in combat during conflicts in Grenada, Panama, Iraq, Somalia, the Balkans, Afghanistan, and other areas in the Middle East.

The UH-60 features four-blade main and tail rotors, and is powered by two General Electric T700 turboshaft engines. The main rotor is fully articulated and has elastomeric bearings in the rotor head. The tail rotor is canted and features a rigid crossbeam. The helicopter has a long, low profile shape to meet the Army's requirement for transporting aboard a C-130 Hercules, with some disassembly.[26] It can carry 11 troops with equipment, lift 2,600 pounds (1,200 kg) of cargo internally or 9,000 pounds (4,100 kg) of cargo (for UH-60L/M) externally by sling.

The Australian Army and the RAAF operate a total of 39 Blackhawks, serial no's A25-101 - A25-114, and A25-201 - A25-225.

For more details of development and design, operational history and variants, click here.

The Socata TB 30 Epsilon is a light military trainer aircraft produced by SOCATA (then part of Aérospatiale). It is a tandem two-seater with a metal airframe. The first prototype flew on 22 December 1979.

In 1978, the French Air Force (Armée de l'Air) published a requirement for a new basic trainer aircraft to partially replace the Fouga Magister in the early parts of the syllabus for pilot training. The new aircraft was expected to have tandem seating, be powered by a 224 kW (300 hp) piston engine and have a three-hour endurance. Similar designs were proposed by the SOCATA subsidiary of Aérospatiale (based on their TB 10 Tobago light aircraft) and by GEPAL (the GEPAL Mk II). The SOCATA proposal, the TB 30B, was chosen in February 1979.

The first of two prototypes flew on 22 December 1979, but testing showed that the Epsilon had poor handling and it was redesigned with a new swept back fin supplemented by a ventral strake and a larger tailplane, while the wing was fitted with elliptical tips increasing the wingspan from 7.40 m (24 ft 33⁄8 in) to 7.59 m (24 ft 113⁄4 in). The first prototype flew again with these changes on 31 October 1980, and it was soon found that the handling problems had been fixed.

The Epsilon is a low winged cantilever monoplane of all metal construction. It is powered by a Lycoming O-540 flat-six piston engine driving a two-blade propeller, and is fitted with a retractable nosewheel undercarriage. The pilot and instructor are sat in tandem under a sliding Plexiglas canopy, with cockpit layout designed to aid transition to the Dassault/Dornier Alpha Jet to which French students graduate after completing the Epsilon part of their training syllabus.

The first prototype was modified into a testbed for the Turbomeca TP 319 Arrius turboprop engine, flying in this form on 9 November 1985. The testbed was then modified into a dedicated turboprop trainer, the TB 31 Oméga, powered by a 360 kW (483 shp) Arrius 1A2 and fitted with ejection seats, returning to flight on 30 April 1989. While it was offered for the United States Air Force/United States Navy Joint Primary Aircraft Training System competition to replace the Beechcraft T-34 Mentor and Cessna T-37 Tweet, it was rejected, with no sales resulting.

The Armée de l'Air placed an initial order for 30 Epsilons in 1981, with further contracts following with a total of 150 ordered. First deliveries started in 1983, with the first training courses based on the Epsilon starting in September 1984.

Export orders were received from Togo for three armed Epsilons in 1984, delivered in 1986 (with a fourth supplied later to replace a crashed aircraft) and from Portugal in 1987 for 18 aircraft, to be assembled in Portugal by OGMA.

Variants
TB 30 Epsilon: Military trainer aircraft
TB 31 Oméga: Proposed turboprop powered version of the TB 30 Epsilon. Only one aircraft built

The Sud-Ouest Aviation (SNCASO) S.O. 4050 Vautour (French for vulture) is a French jet-powered multirole aircraft. The Vautour served as a bomber, ground attack, reconnaissance and interceptor aircraft.

Developed and manufactured by aircraft company Sud Aviation, the Vautour was operated by France's Armée de l'Air, having been originally designed in response to a requirement for a jet aircraft for bombing, low-level attack and all-weather interception. The Vautour was used in the Force de frappe under the Commandement des forces aériennes stratégiques; each aircraft was suitable for the carriage of a nuclear weapon. The shortcomings of the type as a bomber, such as its lack of radar or other advanced navigation/attack systems, led to the type being replaced by the more capable Dassault Mirage IV. The Vautour never saw combat with the French Air Force.

The only other user was the Israeli Air Force (IAF), for which the Vautour undertook various mission and roles, including combat. Vautours were used during the wars between Israel and its neighbors, including the Six-Day War and the War of Attrition. Only one air-to-air kill was recorded by a Vautour; the type was used more for bombing and ground strafing and was reportedly considered by Israel to be comparable to the Soviet-built Ilyushin Il-28 medium bombers used by its regional adversaries. During the early 1970s, the Israeli Vautours were replaced by Douglas A-4 Skyhawks.

The Sud Aviation Vautour was a jet-propelled mid-sized combat aircraft, typically employed as a bomber and attack aircraft, as well as having some usage as an interceptor.[1] In terms of its basic configuration, it had a shoulder-wing monoplane configuration, furnished with a 35° swept wing and a "flying" tail. Power was provided by a pair of SNECMA Atar 101 turbojet engines, which were carried in pods located underneath the wings.[10] The Vautour was equipped with a bicycle-type landing gear configuration in which the main units were located upon the underside of the fore and aft fuselage, these were augmented by smaller stabilizing gear set into bottom of the engine pods. The internal space of the central fuselage was largely dedicated to a large 5 m (16 ft) weapons bay, along with substantial internal fuel tankage.

The Vautour IIB bomber lacked any sort of radar arrangement or many of the contemporary navigational aids and attack systems that were installed upon several aircraft performing the same role during this era. Aiming of the armaments was performed by a bombardier, who would principally perform his bomb-aiming function using a Second World War-vintage American-built Norden bombsight. The navigator/bombardier position was within the nose section, which was glazed to provide external visibility.[3] Both the Vautour IIB and IIA models were restricted to performing missions only under clear-weather operations during daylight. The Vautour IIN interceptor model was not as restrictive, having some capacity to conduct both nighttime and adverse weather operations, having been furnished with a radar system. During its service in Israel, where the weather of the local climate was generally favorable and daylight missions commonplace, the Vautour's lack of advanced targeting and navigation equipment was found to be not a crippling limitation. However, when operated in Europe, these restrictions were considered to be a major disadvantage. As a result, the French AdA never deployed their single-seat Vautour IIA fleet in a frontline capacity; the majority of its IIB bombers were quickly converted to the improved Vautour IIBR standard, which was used to perform photo reconnaissance missions instead.

The Vautour was capable of being equipped with various armaments. In Israeli service, it was typically armed with a pair of 30 mm cannons, as well as up to four removable underwing rocket pods, containing up to 19 air-to-ground rockets each; up to 3,000 kg (6,600 lb) of bombs or alternatively a maximum of 232 68 mm rockets could be accommodated internally in the bomb bay. 4,000 kg (8,800 lb) of bombs could also be mounted externally.[6] The Vautour IIB bomber could be used to carry nuclear weapons in addition to its conventional arsenal. The internal bomb bay of an aircraft could contain either one AN-11 or one AN-22 nuclear bomb; in AdA service, the primary carrier of nuclear weapons would quickly be changed to the newer and more capable Dassault Mirage IV, which supplemented and eventually replace the Vautour IIB bomber.

For operational history and variants, click here.

The Sukhoi Su-17 (izdeliye S-32) is a variable-sweep wing fighter-bomber developed for the Soviet military. Its NATO reporting name is "Fitter". Developed from the Sukhoi Su-7, the Su-17 was the first variable-sweep wing aircraft to enter Soviet service and was featured updated avionics. The aircraft also has variants which were designed to be exported to non-Soviet states such as the Sukhoi Su-22 and the less popular Su-20.

It was produced from 1967-1990. The Su-17/20/22 series had a long career and has been operated by many air forces, including those of the Russian Federation, former Soviet republics, former Warsaw Pact, countries in the Arab world, Angola, and Peru. The Russian Federation retired its fleet in 1998.

Although the Su-17 was capable of carrying nuclear weapons, it was used in roles ranging from close-air support to ground attack.

Shortly after the Su-7 fighter-bomber was put into service, the Sukhoi Design Bureau was ordered to develop a modernization program. The program would be aimed primarily at updating on-board avionics and takeoff/landing characteristics. The concept of variable-geometry wings - something gaining wider attention at that time - was adopted. The program was to be led by Sukhoi's head designer, Nikolay Zyrin.

In 1963 the Sukhoi OKB with input from TsAGI created a variable-sweep wing technology demonstrator. The S-22I (also known as the Su-7IG, NATO designation "Fitter-B"), converted from a production Su-7BM, had fixed inner portions of the wing with movable outer segments that could be swept to 28°, 45°, or 62°. The S-22I first took off (with Vladimir Ilyushin at the controls) on 2 August 1966. It was later demonstrated at the air parade in Domodedovo in July 1967.

Flight testing revealed that the configuration improved both take-off/landing characteristics, range and endurance. Handling was generally better than the fixed wing Su-7, with the exception that buffeting at high angles of attack to warn of imminent stall no longer occurred.

For further details of the deveopment, operational history and variants of the series, click here.

The photos on this page feature the Su-22 of the Polish Air Force, and the specifications below are for the Su-17M4.

The Sukhoi Su-24 (NATO reporting name: Fencer) is a supersonic, all-weather tactical bomber developed in the Soviet Union. The aircraft has a variable-sweep wing, twin engines and a side-by-side seating arrangement for its crew of two. It was the first of the USSR's aircraft to carry an integrated digital navigation/attack system.

The Su-24 started development in the early 1960s and entered full production in 1967. Production ceased in 1993. It remains in service with the Russian Aerospace Forces, Syrian Air Force, Ukrainian Air Force, Algerian Air Force and various other air forces to which it was exported.

The Su-24 has a shoulder-mounted variable geometry wing outboard of a relatively small fixed wing glove, swept at 69°. The wing has four sweep settings: 16° for takeoff and landing, 35° and 45° for cruise at different altitudes, and 69° for minimum aspect ratio and wing area in low-level dashes. The variable geometry wing provides excellent STOL performance, allowing a landing speed of 230 kilometers per hour (140 mph), even lower than the Sukhoi Su-17 despite substantially greater takeoff weight. Its high wing loading provides a stable low-level ride and minimal gust response.

The Su-24 has two Saturn/Lyulka AL-21F-3A afterburning turbojet engines with 109.8 kN (24,700 lbf) thrust each, fed with air from two rectangular side-mounted intakes with splitter plates/boundary-layer diverters.

In early Su-24 ("Fencer A" according to NATO) aircraft these intakes had variable ramps, allowing a maximum speed of 2,320 kilometers per hour (1,440 mph), Mach 2.18, at altitude and a ceiling of 17,500 meters (57,400 ft). Because the Su-24 is used almost exclusively for low-level missions, the actuators for the variable intakes were removed to reduce weight and maintenance. This has no effect on low-level performance, but absolute maximum speed and altitude are cut to Mach 1.35 and 11,000 meters (36,000 ft). The earliest Su-24 had a box-like rear fuselage, which was soon changed in production to a rear exhaust shroud more closely shaped around the engines to reduce drag. The revised aircraft also gained three side-by-side antenna fairings in the nose, a repositioned braking chute, and a new ram-air inlet at the base of the tail fin. The revised aircraft were dubbed "Fencer-B" by NATO, but did not merit a new Soviet designation.

For more details, including operational history and variants, click here.

The Sukhoi Su-25 Grach (Russian: Грач (rook); NATO reporting name: Frogfoot) is a subsonic, single-seat, twin-engine jet aircraft developed in the Soviet Union by Sukhoi. It was designed to provide close air support for Soviet Ground Forces. The first prototype made its maiden flight on 22 February 1975. After testing, the aircraft went into series production in 1978 in Tbilisi in the Georgian Soviet Socialist Republic.

Early variants included the Su-25UB two-seat trainer, the Su-25BM for target-towing, and the Su-25K for export customers. Some aircraft were upgraded to the Su-25SM standard in 2012. The Su-25T and the Su-25TM (also known as the Su-39) were further developments, not produced in significant numbers. The Su-25, and the Su-34, were the only armoured, fixed-wing aircraft in production in 2007. Su-25s are in service with Russia, other CIS members, and export customers.

Since entering service 40 years ago, the Su-25 has seen combat in several conflicts. The type was heavily involved in the Soviet–Afghan War, flying counter-insurgency missions against the Afghan Mujahideen. The Iraqi Air Force employed it against Iran during the 1980–88 Iran–Iraq War. Most were later destroyed or flown to Iran in the 1991 Persian Gulf War. The Georgian Air Force used Su-25s during the Abkhazia War from 1992 to 1993. The Macedonian Air Force used Su-25s against Albanian insurgents in the 2001 Macedonia conflict and, in 2008, Georgia and Russia both used Su-25s in the Russo-Georgian War. African states, including the Ivory Coast, Chad, and Sudan have used the Su-25 in local insurgencies and civil wars. Recently, the Su-25 has seen service in the Russian intervention in the Syrian Civil War, the clashes of the 2020 Nagorno-Karabakh War, and the 2022 Russian invasion of Ukraine. The aircraft above is a Su-25 of the Ukrainian Air Force.

The Su-25 has a conventional aerodynamic layout with a shoulder-mounted trapezoidal wing and a traditional tailplane and rudder. Several metals are used in the construction of the airframe: 60% aluminium, 19% steel, 13.5% titanium, 2% magnesium alloy and 5.5% other materials.

All versions of the Su-25 have a metal cantilever wing, of moderate sweep, high aspect ratio and equipped with high-lift devices. The wing consists of two cantilever sections attached to a central torsion box, forming a single unit with the fuselage. The air brakes are housed in fairings at the tip of each wing. Each wing has five hardpoints for weapons carriage, with the attachment points mounted on load-bearing ribs and spars. Each wing also features a five-section leading edge slat, a two-section flap and an aileron.

For more details of development, design, operational history and variants, click here.

The Su-27 entered service with the Soviet Air Forces in 1985. The primary role was long range air defence against American SAC B-1B and B-52G/H bombers, protecting the Soviet coast from aircraft carriers and flying long range fighter escort for Soviet heavy bombers such as the Tu-95 "Bear", Tu-22M "Backfire" and Tu-160 "Blackjack".

The Su-27's basic design is aerodynamically similar to the MiG-29, but it is substantially larger. The wing blends into the fuselage at the leading edge extensions and is essentially a cross between a swept wing and a cropped delta (the delta wing with tips cropped for missile rails or ECM pods). The fighter is also an example of a tailed delta wing configuration, retaining conventional horizontal tailplanes.

The Su-27 had the Soviet Union's first operational fly-by-wire control system, based on the Sukhoi OKB's experience with the T-4 bomber project. Combined with relatively low wing loading and powerful basic flight controls, it makes for an exceptionally agile aircraft, controllable even at very low speeds and high angle of attack. In airshows the aircraft has demonstrated its maneuverability with a Cobra (Pugachev’s Cobra) or dynamic deceleration – briefly sustained level flight at a 120° angle of attack.

The naval version of the 'Flanker', the Su-27K (or Su-33), incorporates canards for additional lift, reducing takeoff distances. These canards have also been incorporated in some Su-30s, the Su-35, and the Su-37.

For more details on the Su-27, click here.

Specifications below are for the Su-27SK mmodel.

The Sukhoi Su-30 (Russian: Сухой Су-30; NATO reporting name: Flanker-C/G/H) is a twin-engine, two-seat supermaneuverable fighter aircraft developed in the Soviet Union by Russia's Sukhoi Aviation Corporation. It is a multirole fighter for all-weather, air-to-air and air interdiction missions.

The Su-30 started as an internal development project in the Sukhoi Su-27 family by Sukhoi. The design plan was revamped and the name was made official by the Russian Defense Ministry in 1996. Of the Flanker family, the Su-27, Su-30, Su-33, Su-34 and Su-35 have been ordered into limited or serial production by the Russian Defense Ministry. The Su-30 has two distinct version branches, manufactured by competing organisations: KnAAPO and the Irkut Corporation, both of which come under the Sukhoi aerospace group's umbrella.

KnAAPO manufactures the Su-30MKK and the Su-30MK2, which were designed for and sold to China, and later Indonesia, Uganda, Venezuela, and Vietnam. Due to KnAAPO's involvement from the early stages of developing the Su-35, these are basically a two-seat version of the mid-1990s Su-35. The Chinese chose an older but lighter radar so the canards could be omitted in return for increased payload. It is a fighter with both air supremacy and attack capabilities, generally similar to the U.S. F-15E Strike Eagle.

Irkut traditionally served the Soviet Air Defense and, in the early years of Flanker development, was given the responsibility of manufacturing the Su-27UB, the two-seat trainer version. When India showed interests in the Su-30, Irkut offered the multirole Su-30MKI, which originated as the Su-27UB modified with avionics appropriate for fighters. Along with its ground-attack capabilities, the series adds features for the air-superiority role, such as canards, thrust-vectoring, and a long-range phased-array radar. Its derivatives include the Su-30MKM, MKA, and SM for Malaysia, Algeria, and Russia respectively. The Russian Air Force operates several Su-30s and has ordered the Su-30SM variant as well.

While the original Su-27 had good range, it still did not have enough range for the Soviet Air Defense Forces (PVO, as opposed to VVS – the Soviet Air Force). The Air Defense Forces needed to cover the vast expanse of the Soviet Union. Hence, development began in 1986 on the Su-27PU, an improved-capability variant of the Su-27 capable of serving as a long-range interceptor or airborne command post.

The two-seat Su-27UB combat trainer was selected as the basis for the Su-27PU, because it had the performance of a single-seat Su-27 with seating for two crew members. A "proof-of-concept" demonstrator flew 6 June 1987, and this success led to the kick-off of development work on two Su-27PU prototypes. The first Su-27PU flew at Irkutsk on 31 December 1989, and the first of three pre-production models flew on 14 April 1992.

The Su-30 is a multirole fighter. It has a two-seat cockpit with an airbrake behind the canopy. It can serve as an air superiority fighter and as a strike fighter.

For more information on design, operational histories with a number of countries, and a long list of variants, click here.

The Sukhoi Su-34 (Russian: Сухой Су-34; NATO reporting name: Fullback) is a Soviet-origin Russian twin-engine, twin-seat, all-weather supersonic medium-range fighter-bomber/strike aircraft. It first flew in 1990, intended for the Soviet Air Forces, and it entered service in 2014 with the Russian Air Force.

Based on the Sukhoi Su-27 Flanker air superiority fighter, the Su-34 has an armored cockpit for side-by-side seating of its two-person crew. The Su-34 is designed primarily for tactical deployment against ground and naval targets (tactical bombing/attack/interdiction roles, including against small and mobile targets) on solo and group missions in daytime and at night, under favourable and adverse weather conditions and in a hostile environment with counter-fire and electronic warfare (EW) counter-measures deployed, as well as for aerial reconnaissance. The Su-34 will eventually replace the Su-24 tactical strike fighter and the Tu-22M3 long-distance bomber.

The Su-34 shares most of its wing structure, tail, and engine nacelles with the Su-27/Su-30, with canards like the Su-30MKI, Su-33, and Su-27M/35 to increase static instability (higher manoeuvrability) and to reduce trim drag.

The Su-34 is powered by a pair of Saturn AL-31FM1 turbofan engines, the same engines used on the Su-27SM; giving the aircraft a maximum speed of Mach 1.8+ when fully loaded. Although having a slower maximum speed than the standard Su-27, the Su-34 can still handle high G-loads and perform aerobatic maneuvers. When equipped with a full weapons load, the Su-34 has a maximum range of 4,000 kilometres (2,500 mi) without refuelling, this can be extended further via aerial refueling. The airframe is also cleared to perform maneuvers of up to +9 g. The noise level of the Su-34 is two times lower than the level of its predecessors.

The Su-34 is a three-surface design having both a conventional horizontal tailplane at the rear and a canard foreplane in front of the main wings. The foreplane provides both additional lift (force) and greater maneuverability. It has twin tail fins like those of Su-27 from which it is derived. The Su-34 has 12 hardpoints for 8,000 kg (17,600 lb) of ordnance, intended to include the latest Russian precision-guided weapons. It retains the Su-27/Su-30's 30 mm GSh-30-1 cannon, and the ability to carry R-77 air-to-air missiles (6 pcs) and R-73 (also 6), with the air-to-air missiles being primarily for defense against pursuers if detected by the rearward facing radar. The maximum weight of any single munition carried is 4000 kg, its stand-off weapons have range up to 250 kilometres (160 mi). A Khibiny electronic countermeasures (ECM) system is fitted as standard.

For more details of development, design, operational history and variants,click here.

The Sukhoi Su-57 (Russian: Сухой Су-57; NATO reporting name: Felon)[5] is a single-seat, twin-engine stealth multirole fighter aircraft developed by Sukhoi. The aircraft is the product of the PAK FA (Russian: ПАК ФА, short for: Перспективный авиационный комплекс фронтовой авиации, romanized: Perspektivnyy Aviatsionnyy Kompleks Frontovoy Aviatsii, lit. ''prospective aeronautical complex of front-line air forces'') fighter programme, which is intended to be the basis for a family of stealth combat aircraft. Sukhoi's internal designation for the aircraft is T-50. The Su-57 is the first aircraft in Russian military service designed with stealth technology.

A multirole fighter capable of aerial combat as well as ground and maritime strike, the Su-57 incorporates stealth, supermaneuverability, supercruise, integrated avionics, and substantial internal payload capacity. The aircraft is expected to succeed the MiG-29 and Su-27 in the Russian military aviation arms. In addition to serving the Russian armed forces, the aircraft has also been marketed for export. After a protracted development due to various issues that emerged during trials, including the destruction of the first production aircraft in a crash before its delivery, the first aircraft entered service with the Russian Aerospace Forces (VKS) in December 2020. The fighter is expected to have a service life of up to 35 years.

The Su-57 is a fifth-generation multirole fighter aircraft and the first operational stealth aircraft for the Russian armed forces. In addition to stealth, the fighter emphasizes supermaneuverability in all aircraft axes, capacious internal payload bays for multirole versatility, and advanced sensor systems such as active phased-array radar as well as a high degree of integration of these systems. In the Su-57's design, Sukhoi cited the Lockheed Martin F-22 as the baseline for a supermaneuverable stealth fighter, but addressed what the bureau considered to be the limitations, such as the inability to use thrust vectoring to induce roll and yaw moments, a lack of space for weapons bays between the engines resulting in insufficient payload, and complications for stall recovery if thrust vectoring fails.

The aircraft has a wide blended wing body fuselage with two widely spaced engines and has all-moving horizontal and vertical stabilisers, with the vertical stabilisers canted for stealth; the trapezoid wings have leading edge flaps, ailerons, and flaperons. The aircraft incorporates thrust vectoring and large leading edge root extensions that shift the aerodynamic center forward, increasing static instability and maneuverability. These extensions have adjustable leading–edge vortex controllers (LEVCONs) designed to control the generated vortices and can provide trim and improve high angle of attack behaviour, including a quick stall recovery if the thrust vectoring system fails. To air-brake, the ailerons deflect up while the flaperons deflect down and the vertical stabilisers toe inward to increase drag. Although majority of the structural materials are alloys with 40.5–44.5% aluminum alloys and 18.6% titanium alloys, the aircraft makes extensive use of composites, with the material comprising 22–26% of the structural weight and approximately 70% of the outer surface.

Designed from the outset as a multirole aircraft, the Su-57 has substantial internal payload capacity. Weapons are housed in two tandem main weapons bays in the large ventral volume between the widely spaced engine nacelles and smaller side bays with bulged triangular-section fairings near the wing root. Internal weapons carriage eliminates drag from external stores and enables higher performance compared to external carriage, as well as preserving the stealth shaping.

The high degree of static instability (or relaxed stability), advanced KSU-50 flight control system, and canted thrust vectoring nozzles make the Su-57 departure-resistant and highly maneuverable in both pitch and yaw, enabling the aircraft to perform very high angles of attack maneuvers such as the Pugachev's Cobra and the bell maneuver, along with doing flat rotations with little altitude loss. The aerodynamics and engines enable it to achieve speeds of Mach 2 and fly supersonic without afterburners (supercruise) giving a significant kinematic advantage and extends the effective range of missiles and bombs over previous generations of aircraft. Combined with a high fuel load, the fighter has a supersonic range of over 1,500 km (930 mi), more than twice that of the Su-27. An extendable refueling probe is available to further increase its range.

For much more detail on development,design, operational history and variants, click here.

The prototype for the eventual production version flew in January 1956 and production aircraft were delivered in 1957. It saw service with the Royal Navy from 1958 until 1969, replaced in service by the Blackburn Buccaneer.

The Scimitar stemmed from a number of designs from Supermarine for a naval jet aircraft, initially to a requirement for an undercarriage-less fighter aircraft to land on flexible "sprung" rubber decks, which would allow for a lighter and simpler structure. Supermarine's design to meet this requirement was the Type 505, featuring a thin, straight wing and a V-tail (or "butterfly tail") to keep the tail surfaces away from the jet exhausts, and to be powered by two Rolls-Royce Avon turbojets, mounted side-by-side in the fuselage. In 1948, the Admiralty had second thoughts about the undercarriage-less fighter and Supermarine reworked their design by including a nosewheel undercarriage, becoming the Type 508. The Vickers-Supermarine Type 508 was the first Scimitar ancestor and shared the layout of the Type 505, i.e. a twin-engined straight-winged type with a V-tail. Pitch control was by moving the whole tail, with elevators for additional pitch control when working in tandem and to replace the rudder on a conventional tail when working differentially. Ailerons were fitted to the wings for lateral control and leading and trailing edge flaps were also fitted to the wings. An order for three Type 508s was placed in November 1947.

Although the Scimitar could operate as a fighter, the interceptor role was covered by the De Havilland Sea Venom and then the de Havilland Sea Vixen. The Scimitar itself was replaced by the Blackburn Buccaneer. The Scimitar was kept initially as a tanker to allow the underpowered Buccaneer S.1 to be launched from aircraft carriers with a useful weapons load. To save weight, the Buccaneer would take off with minimum fuel then top up from a Scimitar. Late in the Scimitar's operational career, examples were flown between 1965 and 1970 by the Fleet Requirements Unit (FRU) based at Bournemouth Airport (Hurn). The FRU was managed by Airwork Services and provided realistic flight operations for land and sea-based naval training units.

Overall the Scimitar suffered from a high loss rate; 39 were lost in a number of accidents, amounting to 51% of the Scimitar's production run.

For more details of the design, developpment, operational history and variants, click here.

The Supermarine Swift is a British single-seat jet fighter aircraft that was operated by the Royal Air Force (RAF). It was developed and manufactured by Supermarine during the 1940s and 1950s. The Swift featured many of the new jet age innovations, such as a swept wing. On 26 September 1953, a Swift F.4 piloted by Commander Mike Lithgow broke the world absolute speed record, reaching a speed of 737.7 mph (1,187 km/h).

After a protracted development period, the Swift entered service as an interceptor aircraft with the RAF in 1954. However, due to a spate of accidents incurred by the type, the Swift was grounded for a time, and had a relatively brief service life. The problems with the Swift led to a public scandal surrounding the development and performance of the aircraft, harming the reputations of the British government, the RAF, and the British aircraft industry.

Ultimately, the less problematic Hawker Hunter assumed much of the role intended for the Swift and only half as many Swifts were manufactured as had once been intended. A later photo reconnaissance variant of the Swift had resolved some of the teething problems, but that proved to be too late for it to regain favour. An advanced derivative of the Swift that was to be capable of transonic speeds, the Supermarine 545, was also under development during the early 1950s. However, it was cancelled in 1955, principally due to the poor performance of the Swift.

During 1945, the Second World War came to a close and a new post-war Labour government, headed by Clement Attlee, came to power in Britain. The incoming Attlee government's initial stance on defence was that no major conflict would occur for at least a decade, and thus there would be no need to develop or to procure any new aircraft until 1957. In accordance with that policy, aside from a small number of exceptions such as what would become the Hawker Sea Hawk for the Royal Navy, the majority of Specifications issued by the Air Ministry for fighter-sized aircraft during the late 1940s were restricted to research purposes. Aviation author Derek Wood refers to this policy as being: "a fatal error of judgement which was to cost Britain a complete generation of fighters and heavy bomber aircraft".

In part, the Swift had its origins in the experimental fighter prototypes that had been developed. Specifically, a number of Supermarine-built prototypes had been ordered under Specification E.41/46, which had sought the production of an experimental fighter aircraft furnished with a swept wing. The first of those prototypes was designated as the Type 510, which was heavily based on the straight-wing Supermarine Attacker, an early jet aircraft which was procured by the Fleet Air Arm (FAA) of the Royal Navy. The principal difference from the Attacker was that it had been modified with a swept wing configuration. During 1948, the Type 510 had conducted its maiden flight, a year after the first navalised prototype Attacker had flown. That flight made it the first British aircraft to fly with both swept wings and a swept tailplane. In trials for the Fleet Air Arm, the Type 510 was also the first swept-wing aircraft to take off from and land on an aircraft carrier.

During the late 1940s, in the face of the emerging Cold War, the RAF came to recognise that it would urgently require the development and procurement of fighters equipped with features such as swept wings. That need was felt to be so pressing that it was willing to accept interim fighter aircraft while more capable fighters were being developed. In 1950, with the outbreak of the Korean War, Britain's heavy involvement in that conflict led to a flurry of orders being placed. In particular, the RAF felt that a pair of proposed fighter aircraft from Hawker Aircraft and Supermarine were of great importance and, in the same year, ordered the proposed fighters "off the drawing board". The Supermarine design was designated as the Type 541, and was essentially an advanced development of the earlier Type 510 experimental aircraft.

For more details of development, design, operational history and variants, click here.