mercoledì 5 febbraio 2020

Il Sukhoi Su-57 "Prizrac" (Сухой Су-57 in caratteri cirillici, nome in codice NATO "Felon")



Il Sukhoi Su-57 (Сухой Су-57 in caratteri cirillici, nome in codice NATO "Felon"), è un prototipo di caccia multiruolo monoposto di 5ª generazione con caratteristiche stealth sviluppato da Sukhoi per l'aeronautica militare russa.
Noto anche come PAK FA (in russo: Перспективный авиационный комплекс фронтовой авиации, Perspektivnyi Aviatsionnyi Kompleks Frontovoi Aviatsyi, cioè Futuro Sistema Aereo di Prima Linea), o anche come T-50, l'aeromobile è stato ufficialmente denominato "Su-57" nell'agosto del 2017.



Sviluppo

Sono presenti due versioni: il monoposto designato come Su-57 e il biposto, designato come Fifth Generation Fighter Aircraft (FGFA), al cui sviluppo partecipa anche l'India. Avrà il compito di sostituire i MiG-29 Fulcrum e Su-27 Flanker e confrontarsi con i rivali statunitensi F-22, F-35 e quelli cinesi Chengdu J-20.
Lo sviluppo di questo velivolo è curato da un consorzio capeggiato da Sukhoi e la realizzazione avviene insieme con la Novosibirsk Aircraft Production Association (NAPO) e la Komsomolsk-na-Amur Aircraft Production Association (KnAAPO).
La base area presso la quale vengono effettuati i test di sviluppo è Akhtubinsk, nelle vicinanze della città di Volgograd nel sud della Russia.
Il Su-57 dovrebbe entrare in servizio nel primo semestre del 2019, con quasi tre anni di ritardo rispetto alle previsioni. Secondo le stime russe gli Su-57 dovrebbero essere costruiti in un numero totale compreso tra 800 e 1 000 esemplari, il governo russo ha intenzione di dotarsi di almeno 450 Su-57 entro il 2040; ma vista la difficile situazione economica del paese e l'elevatissimo prezzo dei caccia di 5ª generazione, difficilmente si raggiungeranno tali cifre.


Finora 11 prototipi del Su-57 sono stati completati.
Il primo prototipo ha effettuato con successo il volo inaugurale della durata di 47 minuti il 29 gennaio 2010, dalla base della Komsomolsk-on-Amur Aircraft Production Association nell'aeroporto Dzemgi, con il famoso pilota Sergey Bogdan alla guida. Il secondo prototipo ha volato per la prima volta il 3 marzo del 2011. I primi due prototipi erano privi di radar e sistemi d'armamento. Il terzo, dotato di un nuovo radar AESA, ha volato per la prima volta il 22 novembre 2011. Il quarto prototipo ha volato per la prima volta il 12 dicembre 2012. Il quinto prototipo ha volato il 27 ottobre 2013 pilotato da Yury Vashchuk, Sukhoi Chief Pilot ed eroe della Federazione Russa.
Come dichiarato dalla casa produttrice, il nono prototipo dovrebbe essere praticamente uguale ad un aereo di produzione seriale.
Gli undici prototipi costruiti sino ad ora hanno superato i test senza particolari problemi (alla fine del 2013 si è conclusa la fase preliminare dei test, nel 2014 sono cominciati i test statali).
A fine febbraio 2018 la Russia ha inviato 4 prototipi del SU-57 nella base russa in Siria di Hmeimim per probabili test operativi.
Il 15 maggio 2019, Vladimir Putin ha annunciato l'acquisto da parte del Ministero della Difesa della Russia di 76 SU-57, che dovrebbero entrare in servizio con tre gruppi aerei entro il 2028. Il valore del contratto è stimato in 170 miliardi di rubli - circa trentacinque milioni di dollari di valore per singolo esemplare - il che lo rende il più grande nella storia dell'aviazione russa e garantisce il pieno utilizzo della capacità della fabbrica di aeromobili di Komsomol'sk-na-Amure per almeno un decennio. L'accordo definitivo dovrebbe essere sottoscritto alla presenza del presidente alla fiera aerospaziale MAKS-2019 del 19 agosto 2019.
Il giorno 24 dicembre del 2019, durante un volo di collaudo, si è registrato il primo incidente in volo che ha coinvolto un Su-57. Secondo le notizie fornite dalla TASS il velivolo ha avuto problemi ai propri "sistemi di controllo" ed è entrato in vite ad un'altitudine di circa 26 000 piedi (7 900 metri); dopo una discesa di circa 4 000 m il pilota ha deciso di eiettarsi, salvandosi la vita.



Tecnica

Avionica

L'Su-57 è stato dotato di un nuovo radar AESA, come dichiarato dalla stessa casa costruttrice in un comunicato stampa dell'8 agosto 2012. Il radar, che è stato sviluppato dal Tikhomirov Scientific Research Institute of Instrument Design utilizzando nanotecnologie realizzate in Russia, comprende elementi attivi nella banda X sul fronte, ai lati dell'aereo e sul posteriore, e due elementi attivi nella banda L nelle ali. Nella suite dei sensori è stato previsto anche un sensore per gli infrarossi.



Stealth

L'Su-57 sarà il primo velivolo stealth in servizio presso l'aviazione Russa.
Come per tutti gli aerei invisibili ai radar, anche l'Su-57 utilizza delle geometrie particolari delle ali e degli alettoni, materiali compositi, speciali verniciature, mentre i compressori dei motori sono nascosti da una serpentina e particolari elementi per bloccare le onde dei radar.
Essendo l'aereo ancora in fase di sviluppo è difficile determinare la reale efficacia delle soluzioni adottate, ma secondo le analisi di molti esperti dovrebbe avere delle performance in linea con la produzione occidentale.



Armamento

Il progetto del caccia prevede sia l'utilizzo di armamenti esterni collegati alle ali, che di due alloggiamenti interni di ampie dimensioni ricavati nella fusoliera del velivolo, studiati per mantenere al meglio l'invisibilità ai radar, oltre ad un probabile cannoncino frontale. L'Su 57 ha una capacità di carico di armamenti di 7500 kg.



Motori

I motori attualmente utilizzati dal Su-57 (versione modificata degli AL-41F montata sui SU-35) consentono al caccia di ottenere velocità supersoniche senza l'utilizzo di post-bruciatori. L'attuale modello è anche dotato di un sistema vettoriale tridimensionale della spinta, che unitamente al controllo digitale di motori ed aerodinamica garantisce al caccia una elevatissima manovrabilità. I motori appositamente pensati per il SU-57 (Izdeliye-30) sono ancora in fase di sviluppo.



Varianti

FGFA

Variante biposto sviluppata in collaborazione con l'India per l'Aeronautica militare.

UCAV

Nell'agosto 2013, l'azienda russa OAK ha dichiarato di essere in fase di sviluppo per un drone pesante da combattimento basato sul progetto dell'Su-57.

Utilizzatori
  • Russia - Vozdušno-kosmičeskie sily 12 ordinati nel 2018 che saranno consegnati a partire dal 2019. 
  • Algeria - Algerian Air Force – 14 aerei ordinati.


ENGLISH

The Sukhoi Su-57 (Russian: Сухой Су-57; NATO reporting name: Felon) is a stealth, single-seat, twin-engine multirole fifth-generation jet fighter being developed since 2002 for air superiority and attack operations. The aircraft is the product of the PAK FA (Russian: ПАК ФА, short for: Перспективный авиационный комплекс фронтовой авиации, romanized: Perspektivny Aviatsionny Kompleks Frontovoy Aviatsii, lit. ''prospective aeronautical complex of front-line air forces''), a fifth-generation fighter programme of the Russian Air Force. Sukhoi's internal name for the aircraft is T-50. The Su-57 is planned to be the first aircraft in Russian military service to use stealth technology. Its maiden flight took place on 29 January 2010 and the first production aircraft is expected to be delivered in 2019 with a second to follow in 2020.
The fighter is designed to have supercruise, supermaneuverability, stealth, and advanced avionics to overcome the prior generation fighter aircraft as well as ground and naval defences. The Su-57 is intended to succeed the MiG-29 and Su-27 in the Russian Air Force.
The prototypes and initial production batch are to be delivered with a highly upgraded Lyulka AL-31 variant, the AL-41F1, as an interim powerplant while an advanced clean-sheet design engine, currently designated the izdeliye 30, currently in final stages of development and expected to be available after 2020.[18] The aircraft is expected to have a service life of up to 35 years.



Development

Origins

In 1979, the Soviet Union outlined a need for a next-generation aircraft intended to enter service in the 1990s. The project was designated the I-90 (Russian: Истребитель, Istrebitel, "Fighter") and required the fighter to have substantial ground attack capabilities and would eventually replace the MiG-29s and Su-27s in frontline tactical aviation service. The subsequent programme designed to meet these requirements, the MFI (Russian: МФИ, Russian: Многофункциональный фронтовой истребитель, Mnogofunksionalni Frontovoy Istrebitel, "Multifunctional Frontline Fighter"), resulted in Mikoyan's selection to develop the MiG 1.44. Though not a participant in the MFI, Sukhoi started its own programme in 1983 to develop technologies for a next-generation fighter aircraft, resulting in the S-37, later designated Su-47. Due to a lack of funds after the collapse of the Soviet Union, the MiG 1.44 programme was repeatedly delayed and the first flight of the prototype did not occur until 2000, nine years behind schedule. The MiG 1.44 was subsequently cancelled and a new programme for a next-generation fighter, PAK FA, was initiated. The programme requirements reflected the capabilities of Western fighter aircraft, such as the Eurofighter Typhoon and F-22 Raptor. In 2002, Sukhoi was selected over Mikoyan as the winner of the PAK FA competition and would lead the design of the new aircraft; Mikoyan continued to develop its proposal as the LMFS (Russian: ЛМФС, Russian: Легкий многофункциональный фронтальный самолёт, Liogkiy Mnogofunktsionalniy Frontovoi Samolyet, "Light Multifunctional Frontline Fighter") which was designed to be smaller and more affordable.
To reduce the PAK FA's developmental risk and spread out associated costs, as well as to bridge the gap between it and older previous generation fighters, some of its technology and features, such as propulsion and avionics, were implemented in the Sukhoi Su-35S fighter, an advanced variant of the Su-27. The Novosibirsk Aircraft Production Association (NAPO) is manufacturing the new multi-role fighter at Komsomol'sk-on-Amur along with Komsomolsk-on-Amur Aircraft Production Association (KnAAPO), and final assembly is to take place at Komsomol'sk-on-Amur. Following a competition held in 2003, the Tekhnokompleks Scientific and Production Center, Ramenskoye Instrument Building Design Bureau, the Tikhomirov Scientific Research Institute of Instrument Design (NIIP), the Ural Optical and Mechanical Plant (UOMZ) in Yekaterinburg, the Polet firm in Nizhny Novgorod and the Central Scientific Research Radio Engineering Institute in Moscow were selected for the development of the PAK-FA's avionics suite. NPO Saturn is the lead contractor for the interim engines; Saturn and MMPP Salyut will compete for the definitive second stage engines. In 2004, the fighter's conceptual design was completed and approved by Russia's Defense Ministry, with Alexander Davidenko selected as the Chief designer.[1] Funding of the programme began in 2005.
On 8 August 2007, Russian Air Force Commander-in-Chief (CinC) Alexander Zelin was quoted by Russian news agencies that the programme's development stage was complete and construction of the first aircraft for flight testing would begin. Three flyable prototypes were planned to be built by 2009. In 2009, the aircraft's design was officially approved.



Procurement

In 2007, Russia and India agreed to jointly develop the Fifth Generation Fighter Aircraft Programme (FGFA) for India. In September 2010, it was reported that India and Russia had agreed on a preliminary design contract where each country was to invest $6 billion; development of the FGFA fighter was expected to take 8–10 years. The agreement on the preliminary design was to be signed in December 2010. India planned on acquiring a modified version for its FGFA programme. It originally planned on buying 166 single-seat and 48 two-seat fighters, but later changed it to 214 single-seat fighters, and later decreased its purchasing size to 144 fighters by 2012. In early 2018, India pulled out of the FGFA project, which it believed did not meet its requirements for stealth, combat avionics, radars and sensors by that time. This news lead some observers to question the future of the whole Su-57 project.
The Russian Air Force was expected to procure more than 150 fighters for PAK FA with the first fighter to be delivered in 2016. In 2011, the Russian Defence Ministry planned on purchasing the first 10 evaluation aircraft after 2012 and then 60 production standard aircraft after 2016. In December 2014, the Russian Air Force planned to receive 55 fighters by 2020. Russian Deputy Minister of Defence Yury Borisov stated in 2015 that the Air Force would slow production, reduce its initial order to 12 fighters, and retain large fleets of fourth-generation fighters due to the nation's economy.
Russian Air Force Commander-in-Chief Viktor Bondarev stated that the fighter planned to enter serial production in 2017, after all trials would be completed. In 2017, Deputy Minister Yury Borisov stated that the Su-57 would most likely enter service in 2018, due to implementation of more advanced engines, and further testing. He also stated that it would be part of the new 2018-2027 state armament programme. Actual number of aircraft to be delivered is yet unknown.
On 30 June 2018, it was reported that an order for 12 aircraft was agreed, with deliveries to the ranks of the Russian Armed Forces starting in 2019. The first aircraft will join fighter regiments at the Lipetsk Air Center. At the same time, the Deputy Prime Minister for Defence and Space Industry Yury Borisov stated that "Today, the Su-35 is one of the world's best fighters, so there is no reason for us to speed up work on mass production of the fifth-generation fighter." Borisov's statement caused confusion among observers. Some interpreted the fifth generation fighter he referenced as the FGFA, the exported variant of the Su-57, while others interpreted it to be directly alluding to the Su-57 itself. This also led to predictions and concerns about the project's future: some have interpreted it as reiteration that the Su-57 program would continue as previously planned, others interpreted it as the Su-57 program would not be mass-produced, and some believe it to be an implicit announcement of the project's cancellation. The slowing of procurement could be because of the current slow growth of the Russian economy, while the future patches' procurement are for an unknown future; the Russian military could be waiting for the more powerful Saturn izdeliye 30 engine to be ready for serial production.
On 22 August 2018, during the International Military-Technical Forum «ARMY-2018», the Russian Defence Ministry and the JSC Sukhoi signed the first contract for delivery of two serial Su-57 fighters. The deliveries of the first two such aircraft are scheduled for 2019 and 2020, respectively.
Russian Defence Ministry planned to conclude a second contract for 13 more aircraft in 2020. However, on 15 May 2019, Russian President Vladimir Putin announced that 76 aircraft will be purchased and delivered to the Air Force by 2028. This came after the price of the Su-57 and equipment was reduced by 20%. The contract for the 76 aircraft was formally signed on 27 June 2019 at the International Military-Technical Forum «ARMY-2019». The same month, General Director of Tactical Missiles Corporation (KRTV) Boris Obnosov reported, a contract for serial production of ammunition for Su-57 fighters was signed, and is being inducted.
JSC Sukhoi has started the serial production of the aircraft in late July 2019.



Flight testing

The prototype's maiden flight was repeatedly postponed from early 2007 after encountering unspecified technical problems. In August 2009, Alexander Zelin acknowledged that problems with the engine and in technical research remained unsolved. On 28 February 2009, Mikhail Pogosyan announced that the air-frame was almost finished and that the first prototype should be ready by August 2009. On 20 August 2009, Pogosyan said that the first flight would be by year's end. Konstantin Makiyenko, deputy head of the Moscow-based Centre for Analysis of Strategies and Technologies said that "even with delays", the aircraft would likely make its first flight by January or February, adding that it would take five to ten years for commercial production.
Flight testing was further delayed when Deputy Prime Minister Sergei Ivanov announced in December 2009 that the first trials would begin in 2010. The first taxi test was successfully completed on 24 December 2009. Flight testing began with T-50-1, the first prototype aircraft, on 29 January 2010. Piloted by Hero of the Russian Federation Sergey Bogdan, the aircraft's 47-minute maiden flight took place at KnAAPO's Dzemgi Airport in the Russian Far East. The second prototype, T-50-2, was originally planned to fly in late 2010, but this was pushed back to March 2011. The first two prototypes lacked radar and weapon control systems. On 14 March 2011, the fighter achieved supersonic flight at a test range near Komsomolsk-on-Amur. The T-50 was displayed publicly for the first time at the 2011 MAKS Airshow.
The third and fourth prototypes first flew in November 2011 and December 2012, respectively, and lack the pitot tube found on earlier aircraft. By the end of 2013, five prototypes were flown, with the fifth prototype having its first flight on 27 October 2013; with this flight the programme has amassed more than 450 flights. The first aircraft for state test trials was delivered on 21 February 2014.
Testing would reveal that the initial prototypes did not have adequate fatigue life, with early cracks forming in the fuselage. The five initial prototypes required additional structural reinforcements in order to continue flight tests. The aircraft subsequently underwent a structural redesign, with increased composite material usage, reinforced airframe to meet full life cycle requirements, elongated tail "sting", and slightly greater wingspan; the sixth flyable prototype was the first of the redesigned "second stage" aircraft, with the five prior prototypes considered "first stage" vehicles.
A total of ten flying and three non-flying prototypes were built for flight tests and initial combat trials. Five flying and two non-flying prototypes comprise the "first stage" aircraft design, with the two non-flying prototypes testing static flight loads and avionics integration. The first two flying prototypes tested flight characteristics, while the second two prototypes conducted airborne tests of avionics systems, including the radar and electronic warfare suite. The second prototype has since been used to test the second stage izdeliye 30 engine. The fifth prototype was severely damaged by an in-flight fire, and the remains were combined with parts cannibalized from the sixth prototype in order to return the aircraft to flight status. The starting with the sixth flying aircraft, five more of the structurally redesigned "second stage" aircraft were built, as well as one non-flying prototype to test flight loads on the new structure. The last two prototypes were test articles of production aircraft. Issues and accidents during the testing resulted in repeated delays to the programme, with the first production aircraft originally planned for delivery in 2015; this has been delayed multiple times, and the date is now expected to be in 2020.



Design

Overview

The Su-57 is intended to be a fifth-generation multirole fighter aircraft and the first operational stealth aircraft for the Russian Air Force. Although most information is classified, sources within the Sukhoi company and Defence Ministry have openly stated that the aircraft is to be stealthy, supermaneuverable, have supercruise capability, incorporate substantial amounts of composite materials, and possess advanced avionics such as active phased-array radar and sensor fusion.
The aircraft has a blended wing body fuselage and incorporates all-moving horizontal and vertical stabilizers; the vertical stabilizers toe inwards to serve as the aircraft's airbrake. The aircraft incorporates thrust vectoring and has adjustable leading–edge vortex controllers (LEVCONs) designed to control vortices generated by the leading edge root extensions, and can provide trim and improve high angle of attack behaviour, including a quick stall recovery if the thrust vectoring system fails. The advanced flight control system and thrust vectoring nozzles make the aircraft 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 Su-57 has a climb rate ranging from 330 m/s (1,100 ft/s) to 361 m/s (1,180 ft/s). The aircraft makes extensive use of composites, with the material comprising 25% of the structural weight and almost 70% of the outer surface.
Weapons are housed in two tandem main weapons bays between the engine nacelles and smaller bulged, triangular-section bays near the wing root. Internal weapons carriage eliminates drag from external stores and enables higher performance compared to external carriage, as well as enhancing stealth. The Su-57's aerodynamics and engines enable it to achieve Mach 2 and fly supersonic without afterburners, or supercruise, a significant kinematic advantage over prior 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. Extendable refueling probe is available to further increase its range. In the Su-57's design, Sukhoi addressed what it considered to be the F-22's limitations, such as its inability to use thrust vectoring to induce roll and yaw moments and a lack of space for weapons bays between the engines, and complications for stall recovery if thrust vectoring fails.

Stealth

The Su-57 is planned to be the first operational aircraft in Russian Air Force service to use stealth technology. Similar to other stealth fighters such as the F-22, the airframe incorporates planform edge alignment to reduce its radar cross-section (RCS); the leading and trailing edges of the wings and control surfaces and the serrated edges of skin panels are carefully angled to reduce the number of directions the radar waves can be reflected. Weapons are carried internally in weapons bays within the airframe and antennas are recessed from the surface of the skin to preserve the aircraft's stealthy shape. The infrared search-and-track sensor housing is turned backwards when not in use and its rear is treated with radar-absorbent material (RAM) to reduce its radar return. To mask the significant RCS contribution of the engine face, the walls of the inlet ducts are coated with RAM and the partial serpentine ducts obscure most of the engines’ fan and inlet guide-vanes (IGV); the remaining exposed engine face is masked by a radar blocker similar in principle to that used on the F/A-18E/F. According to Sukhoi's radar blocker patent, the slanted blocker grid is placed in front of the IGV at a distance of 0.7—1.2 times the diameter of the duct. The fuselage of the aircraft is coated with RAM to absorb radar emissions and reduce the reflection back to the source.
Due to the extensive use of polymeric carbon plastics composites, the aircraft has four times fewer parts compared to the Su-27, weighs less and is easier to mass-produce. The aircraft canopy is made of composite material and 70-90 nm thick metal oxide layers with enhanced radar wave absorbing to minimize the radar return of the cockpit by 30% and protect the pilot from the impact of ultraviolet and thermal radiation. The Su-57's design emphasizes frontal stealth, with RCS-reducing features most apparent in the forward hemisphere; the shaping of the aft fuselage, the seams between parts, and rivets are much less optimized for radar stealth compared to the F-22. However, during MAKS 2019 the craftsmanship of the fuselage was actually finer than expected and looked smooth despite the rivets.
The combined effect of airframe shape and RAM of the production aircraft is estimated to have reduced the aircraft's RCS to a value thirty times smaller than that of the Su-27. Sukhoi's patent for the Su-57's stealth features cites an average RCS of approximately 0.1 to 1 m2, compared to the Su-27's of approximately 10 to 15 m2. Like other stealth fighters, the Su-57's low observability measures are chiefly effective against high-frequency (between 3 and 30 GHz) radars, usually found on other aircraft. The effects of Rayleigh scattering and resonance mean that low-frequency radars, employed by weather radars and early-warning radars are more likely to detect the Su-57 due to its size. Such radars are also large, susceptible to clutter and are less precise.

Engines

Pre-production T-50 and initial production batches of the Su-57 will use interim engines, a pair of NPO Saturn izdeliye 117, or AL-41F1 augmented turbofans. Closely related to the Saturn izdeliye 117S engine, or AL-41F1S used by the Su-35S, it is a highly improved and uprated variant of the AL-31 that powers the Su-27 family of aircraft. The AL-41F1 produces 93.1 kN (21,000 lbf) of dry thrust, 147.1 kN (33,067 lbf) of thrust in afterburner, and has a thrust to weight ratio of 10.5:1. The engines have full authority digital engine control (FADEC) and are integrated into the flight control system to facilitate maneuverability and handling.
The two AL-41F1 incorporate thrust vectoring (TVC) nozzles whose rotational axes are each canted at an angle, similar to the nozzle arrangement of the Su-35S. This configuration allows the aircraft to produce thrust vectoring moments about all three rotational axes, pitch, yaw and roll. Thrust vectoring nozzles themselves operate in only one plane; the canting allows the aircraft to produce both roll and yaw by vectoring each engine nozzle differently. The engine inlet incorporates variable intake ramps for increased supersonic efficiency and retractable mesh screens to prevent foreign object debris being ingested that would cause engine damage. The AL-41F1 is to also incorporate infrared and RCS reduction measures. In 2014, the Indian Air Force openly expressed concerns over the reliability and performance of the AL-41F1; during the 2011 Moscow Air Show, a T-50 suffered a compressor stall that forced the aircraft to abort takeoff.
Production fighters from 2020 onward will be equipped with a more powerful engine known as the izdeliye 30. Compared to the AL-41F1, the new powerplant will have increased thrust, lower costs, better fuel efficiency, and fewer moving parts. Those features, along with subsequently improved reliability and lower maintenance costs will improve the aircraft performance and reliability. The izdeliye 30 is designed to be 30% lower specific weight than its AL-41F1 predecessor. The new engine is estimated to produce approximately 107 kN (24,054 lbf) of dry thrust and 176 kN (39,556 lbf) in afterburner. Full scale development began in 2011 and the engine's compressor began bench testing in December 2014. The first test engines are planned to be completed in 2016, and flight testing is projected to begin in 2017. According to Deputy Minister Borisov, flight testing with new izdeliye 30 engines will begin at Q4-2017. The new powerplant is designed to be a drop-in replacement for the AL-41F1 with minimal changes to the airframe.
On 5 December 2017, the second Su-57 prototype (T-50-2, bort no. 052), fitted with the izdeliye 30 engine, first took off from the Gromov Flight Research Institute. The 17–minute test flight was carried out by Sergei Bogdan, Sukhoi chief test pilot. The izdeliye 30 engine was installed on the port-side engine position while the AL-41F1 remained on the starboard side. The izdeliye 30 features a new nozzle with serrated flaps compared to conventional ones on the AL-41F1 nozzle. On 8 February 2018, Russian Deputy Minister of Defence Yury Borisov said that the new engine's performance was "...difficult to judge, because all we have had is this one flight. Everything seems normal, but... many flights are to be performed. As a rule, such trials take 2-3 years". By 6 December 2019, Rostec has conducted 16 flights of the Izdeliye 30 engine to check its characteristics in various flight modes, specifically, the operation of the vectoring jet nozzle and the oil system at negative overloads.

Armament

The T-50 prototype has two tandem main internal weapon bays each approximately 4.6 m (15.1 ft) long and 1.0 m (3.3 ft) wide and two small triangular-section weapon bays that protrude under the fuselage near the wing root. Internal carriage of weapons preserves the aircraft's stealth and significantly reduces aerodynamic drag, thus preserving kinematic performance compared to performance with external stores. The Su-57's high cruising speed is expected to substantially increase weapon effectiveness compared to its predecessors. Vympel is developing two ejection launchers for the main bays: the UVKU-50L for missiles weighing up to 300 kg (660 lb) and the UVKU-50U for ordnance weighing up to 700 kg (1,500 lb).
For air-to-air combat, the Su-57 is expected to carry four beyond-visual-range missiles in its two main weapons bays and two short-range missiles in the wing root weapons bays. The primary medium-range missile is the active radar-homing K-77M (izdeliye 180), an upgraded R-77 variant with AESA seeker and conventional rear fins. The short-range missile is the infrared-homing ("heat seeking") K-74M2 (izdeliye 760), an upgraded R-74 variant with reduced cross-section for internal carriage. A clean-sheet design short-range missile designated K-MD (izdeliye 300) is being developed to eventually replace the K-74M2. For longer ranged applications, four large izdeliye 810 beyond-visual-range missiles can be carried, with two in each main weapons bay.
The main bays can also accommodate air-to-ground missiles such as the Kh-38M, as well as multiple 250 kg (550 lb) KAB-250 or 500 kg (1,100 lb) KAB-500 precision guided bombs. The aircraft is also expected to carry further developed and modified variants of Kh-35UE (AS-20 "Kayak") anti-ship missile and Kh-58UShK (AS-11 "Kilter") anti-radiation missile. For missions that do not require stealth, the Su-57 can carry stores on its six external hardpoints. BrahMos Aerospace chief A. Sivathanu Pillai stated that there was a possibility of the installation of BrahMos supersonic cruise missile on the Su-57 FGFA derivative. New hypersonic missile with characteristics similar to the Kh-47M2 Kinzhal ALBM is also being developed for the Su-57. The missile is to have intra-body accommodation and smaller dimensions to allow it to be carried inside the Su-57's main central weapon bays. A new missile appeared to be a derivative of R-77, was displayed during Vympel's 70th anniversary on 18 November 2019. The new missile's length was approximately just 2/3 of R-77's 12 feet length, and thought to be designed to fit inside the triangular wing root bays under the Su-57's wings.
The aircraft has an internally mounted 9A1-4071K (GSh-30-1) 30 mm cannon near the right LEVCON root. The cannon is the lightest in 30mm class with 50 kg weight, and could fire up to 1,800 rounds per minute. The cannon can fire blast-fragmentation, incendiary and armor-piercing tracer rounds and is effective against even lightly armored ground, sea and aerial target up to 800 m for aerial target and 1,800 m for ground target. The cannon is equipped with autonomous water cooling system, where water inside the barrel jacket is vaporized during operation.

Cockpit

The Su-57 has a glass cockpit with two 38 cm (15 in) main multi-functional LCD displays similar to the arrangement of the Su-35S. Positioned around the cockpit are three smaller control panel displays. The cockpit has a wide-angle (30° by 22°) head-up display (HUD). Primary controls are the joystick and a pair of throttles. The aircraft uses a two-piece canopy, with the aft section sliding forward and locking into place. The canopy is treated with special coatings to increase the aircraft's stealth.
The Su-57 employs the NPP Zvezda K-36D-5 ejection seat and the SOZhE-50 life support system, which comprises the anti-g and oxygen generating system. The 30 kg (66 lb) oxygen generating system will provide the pilot with unlimited oxygen supply. The life support system will enable pilots to perform 9-g maneuvers for up to 30 seconds at a time, and the new VKK-17 partial pressure suit will allow safe ejection at altitudes of up to 23,000 m (75,000 ft). In November 2018, the system is said to be at the final stage of test -the stage of state flight tests- and the test pilots are already flying in this equipment. The pilot gear also consisted of a digital helmet which connected to on-board photo and video cameras to improve pilot's situational awareness. It also features pupil's movement detection system to allow automatic targeting unlike previous Soviet fighters. There also a survival kit consisting a pan, antenna, signal mirror, 16 cubes of sugar, first aid kit, two match boxes, a signal pistol with charges, 1.5-liter bottle of water, machete knife, radio beacon, and portable radio. The pilot could use the survival kit's container as a boat or water-proof sleeping bag if necessary.

Avionics

The main avionics systems are the Sh-121 (Russian: Ш-121) multifunctional integrated radio electronic system (MIRES) and the 101KS "Atoll" (Russian: 101КС "Атолл") electro-optical system.
The Sh-121 consists of the N036 Byelka radar system and L402 Himalayas electronic countermeasures system. Developed by Tikhomirov NIIP Institute, the N036 consists of the main nose-mounted N036-1-01 X band active electronically scanned array (AESA) radar, or active phased array radar (Russian: Активная фазированная антенная решётка, Aktivnaya Fazirovannaya Antennaya Reshotka, Russian: АФАР, AFAR) in Russian nomenclature, with 1,552 T/R modules and two side-looking N036B-1-01 X-band AESA radars with 358 T/R modules embedded in the cheeks of the forward fuselage for increased angular coverage. Moreover, the side-looking radar could enable Su-57 to employ extreme beaming tactic (fighter turns 90 degrees away / perpendicular to an enemy's pulse doppler radar array, so enemy's radar would not detect / misinterpret it as a non-moving object) while still able to guide its own missile. The suite also has two N036L-1-01 L band transceivers on the wing's leading edge extensions that are not only used to handle the N036Sh Pokosnik (Reaper) friend-or-foe identification system but also for electronic warfare purposes. Computer processing of the X- and L-band signals by the N036UVS computer and processor enable the system's information to be significantly enhanced.
In 2012, ground tests of the N036 radar began on the third T-50 prototype aircraft. The L402 Himalayas electronic countermeasures (ECM) suite made by the Kaluga Research Radio Engineering Institute uses both its own arrays and that of the N036 radar system. One of its arrays is mounted in the dorsal sting between the two engines. The system was mounted on the aircraft in 2014. Radio telephone communication and encrypted data exchange among various aircraft and also command centers (ground and sea-based and airborne) will be provided by S-111 system, developed by Polyot. The system will be based on modular concept and could be installed not only on Su-57, but also on various aircraft, helicopter, and drones. "Its effective range of operation is up to 1,500 kilometres (930 mi)" a spokesman said. "The system's reliability is guaranteed by the multiple redundancy of the main functions and cutting edge technical solutions, as well as a wide range of radio channels."
The UOMZ' 101KS "Atoll" electro-optical system consisted of:
The 101KS-V infra-red search and track turret mounted on the starboard side in front of the cockpit. This sensor can detect, identify, and track multiple airborne targets simultaneously.
The 101KS-O Directional Infrared Counter Measures system has sensors housed in turrets mounted on the dorsal spine and forward fuselage under the cockpit and uses modulated laser-based countermeasures to confuse or destroy heat-seeking missiles' tracking mechanism. Judging from its position, the system allegedly intended not only as a self-protection against MANPADS but also air-to-air missile. In this regard, Su-57 could be something of a pioneer, while similar DIRCM capabilities haven't been ported over to the latest generations of high-flying western fighter aircraft.
The 101KS-U ultraviolet missile approach warning sensors (MAWS) against infra-red homing missiles. MAWS using ultraviolet technology can operate under all weather conditions and will not be affected by solar clutter. It provides good directional information of the incoming missile for good decoy dispensing decision making, maneuvering and to cue the DIRCM system into action.
The 101KS-P, a high-resolution thermal imager, provides low-altitude piloting and landing in night conditions. It is installed in front of the compartments of short-range missiles and is not used for targeting purposes but for efficient low altitude flight and night landing operations.
The 101KS-N (наземная = Ground) advanced stabilised navigation and targeting system integrated into the airframe underside of forward fuselage: scannig mirror and automatic tracking unit, laser rangefinder/target indicator and laser spot tracker.
Optional 101KS-N external navigation and targeting pod. It will have similar function to the AN/AAQ28 Litening and AN/AAQ33 Sniper advanced targeting pods of the US military and will be mounted under the air intake.

In 2014, Concern Radio-Electronic Technologies (KRET) announced it has created an upgraded BINS-SP2M strapdown inertial navigation system, developed by its two enterprises, Moscow Institute of Electromechanics and Automatics (MIEA) and Ramensky Instrument Engineering Plant (RPZ). Built on the basis of laser gyros and quartz accelerometers, it autonomously processes navigation and flight information, determines position and motion parameters in the absence of satellite navigation, and can integrate with GLONASS. It is guaranteed to last at least 10,000 hours, and can be utilized universally not only in airborne, but also in marine and terrestrial equipment. In 2016, KRET announced it is developing multifunctional video processing system called "Okhotnik" (Hunter), to increase the Su-57's target detection range as well as to improve automatic detection and tracking of targets.
In April 2017, UAC announced that a new next-generation integrated avionics suite has started flight-testing. According to Dmitry Gribov, a chief designer of the new complex, the new avionics suite—called the ИМА БК, the Russian acronym for Интегрированная модульная авионика боевого комплекса (integrated modular avionics combat systems)—will replace a system designed in 2004 called Багет (Baguette) used on the Su-35. The still-in-development system has more than 4 million lines of code. The IMA BK makes use of indigenous Russian multi-core microprocessors and a new indigenous real-time operating system called "BagrOS-4000". The new avionic suite also makes use of fiber-optic channels with a throughput of more than 8 Gbit/s, which is up from 100 Mbit/sec for traditional copper wires. The new IMA BK integrated avionics suite is designed to automatically detect, identify, and track the most dangerous targets and offer the pilot the best solution to engage an enemy. The new system will take control of almost all of the key sensors of the aircraft—radar, navigation and communication that in previous aircraft were controlled by separate computers—simultaneously performs the role of an electronic pilot, electronic navigator and electronic flight engineer.
A monitoring system mimicking living organism's nervous system will allow real-time assessment of the aircraft's condition and predict the remaining 'life' of the composite parts of the aircraft by combining optical fibers with sensitivity to mechanical influences with aircraft's network system. The information about aircraft's condition will be transmitted via laser beam through the optical fiber woven into the structure. It will decrease aircraft's maintenance costs and allow parts to be repaired preemptively, thus improving flight safety.


Possible role

Since the Russian military doctrine is very different from the US's military doctrine, this fighter follows a different design philosophy. The Aerospace Forces' main roles are to provide support for ground troops at a tactical level and air defense. With the Su-57's forward-optimized stealth and infrared sensor, the aircraft could be considered as a counter-stealth fighter meant to get as close as possible to adversary stealth jets before engaging them, diminishing the enemy's stealth advantage and forcing them to a close quarter dogfight, where it has the theoretical advantage due to its 3-D thrust vectoring and supermaneuverability.
According to Bill Sweetman, the Su-57's high operational speed and altitude combined with its standoff weaponry could be hinting at its role as a "sort of airborne sniper", designed to fly fast and high to engage enemy support aircraft. This claim is supported by Russia's intentions to adapt the new R-37M (Izdeliye 810) air-to-air missile with range of more than 300 km to the Su-57's armament, giving it a role similar to the MiG-31BM interceptors. Newly designed anti-ship weapons could also enable the Su-57 to perform as a maritime strike aircraft.

Operational history

Russia

Testing and trials

The 929th State Flight Test Centre (GLITS) received its first T-50 prototype for further testing and state trials in March 2014, and Russian Air Force Commander-in-Chief Lieutenant General Viktor Bondarev said that deliveries of initial production T-50 fighter were expected to begin in 2016. External weapon trials started in May 2014. In the event, the 2016 date for production was missed.
On 8 February 2018, then Deputy Minister of Defence Yury Borisov said that the first stage of state trials had been concluded and that the combat trials were on schedule. During the interview, he also reported that the contract for an initial batch of 12 aircraft was to be signed in 2018. First two serial units were ordered in August 2018, with term of delivery by 2020. State trials are to be complete in 2019.
On 27 September 2019, Russian MoD released a video showcasing the first flight of Okhotnik alongside Su-57. Reportedly the UAV operated autonomously and flew for more than 30 minutes interacting with the Su-57 to test extending the fighter's radar and target designation range for use of long-range air-launched weapons from the outside of enemy air defenses.

Syrian combat evaluation

On 21 February 2018, two Su-57s performed first international flight as they were spotted landing at the Russian Khmeimim air base in Syria. The aircraft were deployed along with four Sukhoi Su-35 fighters, four Sukhoi Su-25s, and one Beriev A-50 AEW&C aircraft. Three days later two more Su-57s were reported to have arrived in Syria. The deployment was criticised by some experts as overly risky, especially after reports of drone attacks at Khmeimim air base. Military correspondent of Komsomolskaya Pravda Viktor Baranets was cited as saying that according to his information the Su-57s have "excellently" carried out their mission in Eastern Ghouta. On 1 March 2018, the Russian Defence Minister Sergey Shoygu confirmed that the two Su-57s indeed spent two days in Syria and successfully completed a trials program, including combat trials during which parameters of weapons work were monitored. On 25 May 2018, the Russian Defence Ministry disclosed that during the February 2018 deployment to Syria, a Su-57 fired a cruise missile in combat, likely a Kh-59MK2. On 18 November 2018, the Russian Defence Ministry posted an extended video of the fighters' flights, and announced that Su-57 performed 10 flights during its deployment to Syria. However, the video did not specify when the test flights took place.
On 18 December 2019, Chief of the Russian General Staff, Valery Gerasimov said that Russian Defense Ministry has once again tested Su-57 in Syria, and all tasks have been successfully fulfilled.

Algeria

On 27 December 2019, it was reported Algeria has signed a contract for 14 aircraft as part of large military deal that also includes purchase of Su-34 and Su-35 fighters. The decision was reportedly taken in summer 2019, when Algerian delegation personally inspected the fighter at the 2019 MAKS air show in Moscow.

Potential operators

Turkey

In May 2018, Turkish media Yeni Safak stated that Turkey might evaluate Su-57 purchase if the US cancels F-35 deliveries due to Turkey's S-400 purchase. However, internal source stated that the possibility of Su-57 purchase was based on expert's opinion and not reflecting the official position of Ankara. While on 30 June 2018, Turkey received its first F-35 in a ceremony at Lockheed Martin's facilities in Texas,[217] the US ultimately expelled Turkey from the F-35 fighter programme after the first S-400 delivery in July 2019.
In May 2019, Sergey Chemezov, CEO of Rostec, said that Russia was ready to cooperate with Turkey on the export and local production of the Su-57.[219] On 30 August 2019, President Erdogan confirmed Turkey and Russia are negotiating possible Su-57 fighter deliveries, after personally inspecting the aircraft at the 2019 MAKS air show. On 14 September 2019, a Sukhoi Su-57 fighter reportedly landed in Turkey for the 2019 Technofest festival held in Istanbul.

Others

During Dubai Air Show in the UAE on 18 November 2019, Sergey Chemezov, in charge of Rostec, talked about the possibility of "localization" of portions of the Su-57 supply chain within other countries that decide to buy those jets, including '...United Arab Emirates, India or Turkey...', depends on the capabilities of the defense industrial base of the customer in question.

Variants

FGFA

The completed joint Indian/Russian versions of the single-seat or two-seat FGFA will differ from the current T-50 flying prototypes in 43 ways with improvements to stealth, supercruise, sensors, networking, and combat avionics.
In March 2010, Sukhoi director Mikhail Pogosyan projected a market for 1,000 fighter aircraft over the next four decades, which will be produced in a joint venture with India, 200 each for Russia and India and 600 for other countries. He has also said that the Indian contribution would be in the form of joint work under the current agreement rather than as a joint venture. In June 2010, the Indian Air Force planned to receive 50 of the single-seat "Russian version" before receiving the two-seat FGFA. Then in an October 2012 interview the Chief of Air Staff of India, NAK Browne, said that the IAF will purchase 144 of the single-seat FGFA. To reduce development costs and timelines, the IAF plans to begin induction of the FGFA in 2020.
In April 2018, it was reported that India is withdrawing from the program. India has become increasingly disappointed with the project's progress after years of negotiations, delays, and struggles with Russia. India is also not satisfied with the capabilities of Su-57, the basis of the FGFA with one of the main issues being the Su-57's insufficient stealth design.
On 9 July 2019, during a meeting with IAF representatives, Russia offers India to resume its participation in Su-57 program. Deputy Director of Russia’s Federal Service for Military and Technical Cooperation Vladimir Drozhzhov told that "Russia is open to that... We are ready and are proposing this program to our Indian partners". IAF Air Chief Marshall Birender Singh Dhanoa during an interview with Russian Ministry of Defense's official newspaper Krasnaya Zvezda (Red Star), stated that while Su-57 is currently not being considered for the IAF, but the combat aircraft can be evaluated once it joins active service with the Russian Air Force.

Other versions

Alexei Fedorov has said that any decision on applying fifth-generation technologies to produce a smaller fighter (comparable to the F-35) must wait until after the heavy fighter, based on the T-50, is completed.
A naval version of the Su-57 was proposed for the Project 23000E or Shtorm supercarrier. Models of the aircraft carrier project are showing Su-57 on board, with folding wings and stabilators. The Su-57 should be able to use the takeoff ramp as well as the Electromagnetic Aircraft Launch System.
The aircraft is used as a testbed for integration with UAVs as well as various subsystems (including weapon, control and navigation systems) being developed for Russia's future sixth-generation combat system, both in manned and unmanned version. In January 2019, it was reported the third flyable Su-57 prototype (bort. no 053) is being used for interaction with the Sukhoi S-70 Okhotnik UCAV, and testing of its avionics systems.

Export

Sukhoi states that the main export advantage of the PAK FA is its lower cost than current US fifth generation jet fighters. Russia was reported to be offering the PAK FA for South Korea's next generation jet fighter. South Korea's defence procurement agency confirmed that the Sukhoi PAK FA was a candidate for the Republic of Korea Air Force's next-generation fighter (F-X Phase 3) aircraft; however, Sukhoi did not submit a bid by the January 2012 deadline.
The PAK FA was slated to be introduced for export in 2022 with the introduction of the Sukhoi/HAL FGFA, the primary export version, for the Indian Air Force. Ruslan Pukhov, director of the Centre for Analysis of Strategies and Technologies, has projected that Vietnam will be the second export customer for the fighter. In 2012, Russian Defence Minister Anatoly Serdyukov said that Russia and India would jointly build the export version of the T-50 starting in 2020. Mikhail Pogosyan, the head of United Aircraft Corporation, said in 2013 that the Russian PAK FA and the Sukhoi/HAL FGFA will use "identical onboard systems and avionics".
In 2013, Russia offered Brazil participation and joint production in a next-generation fighter based on the T-50.
On 28 March 2019, an export version dubbed Su-57E was first promoted to international customers during the 2019 Langkawi International Maritime and Aerospace Exhibition. The aircraft was officially unveiled at the 2019 MAKS International Aviation and Space Salon. Su-57E was first publicly displayed in August 2019 at the 2019 MAKS International Aviation and Space Salon held in Moscow.

Operators
  • Algeria - Algerian Air Force – 14 aircraft on order.
  • Russia -  Russian Air Force – 78 aircraft on order.

Accidents

On 10 June 2014, the fifth flying prototype, aircraft T-50-5, was severely damaged by an engine fire after landing. The pilot managed to escape unharmed. Sukhoi stated that the aircraft will be repaired, and that the fire "will not affect the timing of the T-50 test program".
On 24 December 2019, the first serial Su-57 (bort number "01 blue") crashed 110–120 km away from the Dzyomgi Airport, Khabarovsk Krai, during the final stage of its factory trials due to malfunction of the control system. The pilot ejected and was recovered by helicopter. According to TASS, the test flight was carried out at the altitude of 8,000 meters when the malfunction occurred, causing the airplane to enter a rapid spiral descent. When all attempts to stabilize the airplane into a horizontal flight using the manual flight control system failed, the pilot ejected at the altitude of 2,000 meters.

Specifications (Su-57)

General characteristics
  • Crew: 1
  • Length: 20.1 m (65 ft 11 in)
  • Wingspan: 14.1 m (46 ft 3 in)
  • Height: 4.74 m (15 ft 7 in)
  • Wing area: 78.8 m2 (848 sq ft)
  • Empty weight: 18,000 kg (39,683 lb)
  • Gross weight: 25,000 kg (55,116 lb) typical mission weight, 29,270 kg (64,530 lb) at full load
  • Max takeoff weight: 35,000 kg (77,162 lb)
  • Fuel capacity: 10,300 kg (22,700 lb) internally
  • Powerplant: 2 × Saturn AL-41F1 (initial production) turbofans with thrust vectoring, 93.1 kN (20,900 lbf) thrust each dry, 147.2 kN (33,100 lbf) with afterburner
  • Powerplant: 2 × izdeliye 30 (later production) turbofans with thrust vectoring, 107.9 kN (24,300 lbf) thrust each dry, 176.6 kN (39,700 lbf) with afterburner.

Performance
  • Maximum speed: Mach 2 (2,120 km/h; 1,320 mph) at altitude
  • Supercruise: Mach 1.6 (1,710 km/h; 1,060 mph) at altitude
  • Range: 3,500 km (2,200 mi, 1,900 nmi) subsonic, 4,500 km from 2 outboard fuel tanks
  • Supersonic range: 1,500 km (930 mi, 810 nmi)
  • Service ceiling: 20,000 m (66,000 ft)
  • g limits: +9.0
  • Wing loading: 317 kg/m2 (65 lb/sq ft) typical mission weight
  • Thrust/weight:
  • AL-41F1: 1.02 (1.19 at typical mission weight)
  • izdeliye 30: 1.15–1.2 (1.36 at typical mission weight).

Armament

  • Guns: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon in right LEVCON root
  • Hardpoints: 12 hardpoints (6 × internal, 6 × external)
  • Air-to-air missiles:
  • 4 × RVV-MD
  • 2 × R-73
  • R-37M
  • Air-to-surface missiles:
  • 4 × Kh-38ME, Kh-59MK2
  • Anti-ship missiles:
  • 2 × Kh-35E, 31 etс.
  • Anti-radiation missiles:
  • 4 × Kh-58UShKE
  • 250, 500, 1500 kg guided bombs
  • Anti-tank "Drill" 500 kg cluster-bomb + active homing.

Avionics

  • Sh-121 multifunctional integrated radio electronic system (MIRES)
  • Byelka radar (400 km, 60 targets of 16 hit)
  • N036-1-01: Frontal X-band active electronically scanned array (AESA) radar
  • N036B-1-01: Cheek X-band AESA radars for increased angular coverage
  • N036L-1-01: Slat L-band arrays for IFF
  • L402 Himalayas electronic countermeasure suite
  • 101KS Atoll electro-optical targeting system
  • 101KS-O: Laser Directional Infrared Counter Measures
  • 101KS-V: Infra-red search and track
  • 101KS-U: Ultraviolet missile approach warning system
  • 101KS-N: advanced stabilised navigation and targeting system
  • 101KS-N: optional external Targeting pod
  • 101KS-P: thermal imager for low altitude flying and night landing.


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La P.A.N. è in fervente attesa del nuovo M-345 HET, il sostituto del mitico MB 339!



L’addestratore basico M-345 HET (High Efficiency Trainer), inizialmente presentato come M-311, è un monogetto sviluppato dall'azienda aeronautica italiana Leonardo nei primi anni duemila ed attualmente in fase di commercializzazione.



Storia del progetto

Aermacchi M-311

Nei primi anni duemila l'allora Alenia Aeronautica decise di avviare lo sviluppo di un nuovo modello di aereo militare a getto biposto finalizzato all'addestramento basico dei futuri piloti destinati ad operare con aerei da combattimento di ultima generazione. A questo scopo l'ufficio di progettazione attinse all'esperienza già impiegata nello sviluppo del precedente SIAI-Marchetti S-211A, versione appositamente ideata negli anni novanta, in joint venture con la statunitense Grumman, per partecipare al concorso JPATS per un nuovo addestratore indetto dall'USAF e dall'U.S. Navy, presentandone un aggiornamento con avionica avanzata, completamente digitale, ed equipaggiata con glass cockpit ed Head Up Display.
Il nuovo modello, indicato come M-311, riproponeva l'impostazione del suo predecessore, un velivolo monomotore a getto, con cabina di pilotaggio biposto in tandem chiusa da un lungo cupolino e ala monoplana a freccia posizionata medio-alta sulla fusoliera. L'azienda ne annunciò lo sviluppo nel 2004 e come per altri velivoli dalle simili caratteristiche ne era previsto lo sviluppo e commercializzazione di una variante armata destinata a missioni di supporto aereo ravvicinato. Rispetto al S-211, da cui derivava, la struttura era stata rinforzata, soluzione necessaria per compensare le sollecitazioni date dal nuovo propulsore che garantiva una spinta maggiore del 30%. Presentava inoltre una nuova aerodinamica, con modifiche alle estremità alari e alla parte inferiore della fusoliera, dotata di una nuova pinna ventrale, e integrava nella cabina di pilotaggio avionica avanzata. Il preesistente primo prototipo del S-211A (I-PATS, C.S. X619) venne quindi modificato secondo le nuove specifiche e portato in volo per la prima volta il 1 giugno 2005.



Aermacchi M-345

L'M311 venne ridesignato M-345 nel 2012, per sottolinearne la complementarità con il successivo addestratore avanzato M-346. La più recente configurazione, M-345 HET (High Efficiency Trainer), ha beneficiato di varie modifiche, come ad esempio l'impiego di tettuccio, seggiolini e altre parti in comune con l'M-346, un musetto più allungato ed un motore più moderno, sempre turbofan, con un valore di spinta attorno ai 1 600 kgf (Williams FJ44-4M). Il nuovo prototipo viene portato in volo per la prima volta il 29 dicembre 2016 dall'aeroporto di Varese-Venegono, ai comandi dei piloti collaudatori Quirino Bucci e Giacomo Iannelli della Divisione Velivoli di Leonardo Aircraft. Nel dicembre 2018 è stato effettuato il primo volo anche dal primo modello di serie del M-345 HET.



Impiego operativo

Nel 2013 l'Alenia Aermacchi M-345 HET fu inizialmente designato dall'Aeronautica Militare quale successore, a partire dal 2017, degli Aermacchi MB-339A e MB-339PAN utilizzati dalle Frecce Tricolori. La sostituzione prevista è stata però inizialmente fermata dal governo nel 2014, in quanto considerata non prioritaria.
Nel 2017 la Leonardo ha firmato con il Ministero della Difesa italiano un contratto relativo alla fornitura di un primo lotto di 5 velivoli da addestramento M-345 HET, di cui la prima consegna è prevista per il 2020. L'Aeronautica Militare ha previsto un fabbisogno totale di 45 M-345 per sostituire progressivamente gli Aermacchi MB-339.



Utilizzatori:
  • Italia - Aeronautica Militare - 5 ordinati il 13 gennaio 2017. Prevista un'acquisizione iniziale di 45 velivoli. Ulteriori 13 esemplari sono stati ordinati a giugno 2019, con consegne a partire dal 2020.

Il velivolo da addestramento di nuova generazione

L’Aermacchi M-345, sviluppato sfruttando la consolidata esperienza acquisita negli ultimi 60 anni dalla Divisione Velivoli nella progettazione e produzione della sua ampia famiglia di velivoli da addestramento, offre le superiori prestazioni e l'efficacia addestrativa tipiche di un aereo a getto a costi paragonabili a quelli di addestratori turboelica di elevata potenza. Destinato alle fasi basico-avanzate del syllabus per l’addestramento dei piloti, l'M-345 garantisce elevata efficienza e bassi costi di acquisizione e operativi.



Elevata efficienza

La riduzione dei costi di esercizio è determinata dall’elevata vita a fatica e dal basso livello di manutenzione richiesto, quest'ultimo reso possibile dal sistema di monitoraggio di struttura e impianti (HUMS) che elimina le attività di manutenzione più onerose. L'efficienza operativa è garantita dai sistemi di rifornimento a pressione a punto singolo e di generazione di ossigeno a bordo (OBOGS), che riducono la necessità di supporto a terra.



Avionica

Progettata sulla più recente esperienza dell’M-346 Advanced Jet Trainer e in linea con gli standard dei più moderni jet da combattimento, l'avionica dell’M-345 include la più moderna interfaccia uomo-macchina con i comandi HOTAS, i display per la presentazione dati a testa alta (HUD) e multifunzione (MFD), mentre il sistema integrato di bordo per la simulazione all’addestramento tattico (ETTS) consente di simulare durante il volo l'intero spettro delle attività di addestramento.



Ruoli operativi

Mantenendo nel contempo le proprie superiori caratteristiche da velivolo d’addestramento a getto, grazie alla sua avionica moderna, all’elevata capacità di carico esterno (più di 1.000 kg, 4 piloni subalari) e alle prestazioni, l'M-345 è adatto per svolgere anche ruoli operativi, con la capacità di utilizzare sistemi come il pod cannone, razzi e bombe nella classe delle 500 libbre.



Pattuglia acrobatica Nazionale

L’M-345 HET e sarà il nuovo aereo delle Frecce Tricolori che andrà a sostituire l’Aermacchi MB-339. Questo velivolo, molto apprezzato per le caratteristiche di volo, oltre ad esibirsi nei cieli di tutto il mondo grazie alla pattuglia acrobatica nazionale, costituisce un ottimo biglietto da visita dell’industria aeronautica italiana, prodotto in diverse versioni e venduto a numerose nazioni straniere nel corso degli anni.
Se pensiamo che il suo primo volo è avvenuto nel 1976, ci sembra abbastanza naturale che da un po’ di tempo si pensi alla sua sostituzione nei ranghi della nostra Aeronautica Militare, ed anche per fornire un nuovo aereo da proporre ai clienti stranieri, interessati ad un moderno aeroplano, che possa sempre svolgere i ruoli di addestratore per le future schiere di piloti, e di appoggio ravvicinato alle truppe, in scenari da impiego bellico.
Da qualche anno il gruppo Leonardo è impegnato nella realizzazione e nella promozione del sostituto del MB-339, il M-345 HET. La principale interessata è proprio l’Aeronautica Militare che prevede di fare entrare in linea il nuovo arrivato già a partire dal 2020, con l’intenzione di acquisirne 45, dando molta importanza alle nuove capacità dell’M-345 HET di aumentare l’efficienza nella preparazione dei nuovi piloti, grazie alle prestazioni e alla nuova avionica che apre scenari addestrativi di altissimo livello.
Ed è proprio di queste ore la notizia che il primo aereo M-345 HET (High Efficienti Trainer) di serie, ha spiccato il volo, sotto il controllo dei due collaudatori Quirino Bucci e Giacomo Iannelli. Il test è stato positivo e secondo le prime indiscrezioni, l’aereo ha dimostrato doti eccellenti di risposta nelle varie configurazioni di spinta in cui il motore è stato sottoposto. Ciò dimostra la bontà del propulsore, e il perfetto connubio dell’interfaccia uomo macchina. Inutile dire che le aspettative sono molto alte riguardo questo progetto, che andrà a rinnovare completamente il comparto addestrativo della nostra Aeronautica e costituirà il nuovo aeroplano in servizio anche con le Frecce Tricolori.
Importante il successo sul piano internazionale che vede diverse nazioni pronte all’acquisto del nuovo nato in casa Leonardo. L’aereo ha una velocità massima di 780 Km/h, un autonomia di 1400 Km e una tangenza massima di 12 900 metri. Punto forte del velivolo è la sofisticata elettronica di bordo che permette una notevole flessibilità di utilizzo, abituando sin da subito gli allievi piloti ad ambientarsi con procedure e tecniche di pilotaggio, che troveranno poi nei velivoli dei reparti a cui saranno destinati. Per nulla da trascurare anche l’aspetto economico di esercizio di questo aeroplano, che promette di essere molto più vantaggioso rispetto ai concorrenti a turboelica.



L’apparato propulsivo Williams FJ44 

I Williams FJ44 compongono una famiglia di motori aeronautici turboventola, con doppio compressore, prodotti da Williams International/Rolls-Royce plc destinati al mercato dei business jet. Fino al recente aumento delle vendite di business jet di piccole dimensioni (Very Light Jet), la FJ44 è stata una delle più piccole turboventole disponibili per applicazioni civili. Anche se il progetto è formalmente della Williams International, la Rolls-Royce è stata coinvolta nello sviluppo, nella progettazione e nella produzione di una turbina raffreddata ad aria ad alta pressione per il motore. Il primo volo di un motore FJ44 è stato effettuato il 12 luglio 1988 su un Scaled Composites Triumph.
La Williams FJ33 è un motore più piccolo basato sulla stessa base della FJ44.

Varianti del motore adottato:
  • FJ44-1A
  • FJ44-1AP
  • FJ44-1C
  • FJ44-2A
  • FJ44-2C
  • FJ44-3A
  • FJ44-3A-24
  • FJ44-3AP
  • FJ44-3ATW
  • FJ44-4A
  • FJ44-4M
  • F129: designazione militare di una versione del FJ44 con una spinta di 6.672 kN.

Velivoli utilizzatori del motore
  • Aero L-39NG
  • Alenia Aermacchi M-345
  • Beechcraft Premier I
  • Eviation Jets EV-20 Vantage Jet
  • Cessna CitationJet
  • Grob G180 SPn
  • Hawker 200
  • Lockheed Martin RQ-3 DarkStar
  • Lockheed Martin Polecat
  • Pilatus PC-24
  • Piper PA-47 PiperJet
  • Piper PiperJet Altaire
  • Saab 105
  • Scaled Composites Proteus
  • Scaled Composites Triumph
  • SyberJet SJ30
  • Virgin Atlantic GlobalFlyer
  • Cessna 526 CitationJet.

Il velivolo di serie

Il primo esemplare di serie dell’M-345 High Efficiency Trainer ha effettuato i primi di dicembre 2019 con successo il suo primo volo dall’aeroporto di Venegono Superiore (Varese). Ai comandi del velivolo i piloti della Divisione Velivoli di Leonardo, Quirino Bucci e Giacomo Iannelli.
Il velivolo si è comportato perfettamente confermando le attese previste dai parametri progettuali ed esprimendo performance eccellenti. Il motore, in particolare, ha dimostrato un’ottima reattività alle variazioni di regime, caratteristica che sarà fondamentale per il velivolo nello svolgimento dei vari ruoli di impiego, in particolare quello del volo acrobatico in formazione. Sono stati inoltre testati gli avanzatissimi sistemi di bordo e ho avuto un positivo impatto rispetto all’ottimo livello di integrazione dell’avionica e dell’interfaccia con il pilota.
L’M-345, che ha già suscitato l’interesse di molte Forze Aeree in tutto il mondo, grazie alle sue prestazioni e all’avanzato sistema di addestramento integrato, garantirà un significativo miglioramento dell’efficacia addestrativa e una riduzione dei costi operativi. Si tratta di un velivolo in grado di offrire le superiori prestazioni e l’efficacia tipiche degli aerei a getto a costi comparabili a quelli dei velivoli da addestramento a turboelica di elevata potenza.
Il cliente di lancio dell’M-345 è l’Aeronautica Militare che ha identificato un fabbisogno per fino a 45 nuovi addestratori M-345 (la cui sigla identificativa di forza armata è T-345A) per sostituire progressivamente i 137 MB-339 entrati in linea a partire dal 1982 e anche per rappresentare la nuova piattaforma della Pattuglia Acrobatica Nazionale (PAN).
Ad oggi l’AM ne ha ordinati cinque ed il primo velivolo sarà consegnato ad inizio 2020. I nuovi M-345 andranno ad integrare gli M-346 impiegati per la fase avanzata dell’addestramento dei piloti dell’Aeronautica Militare che attraverso l’International Flight Training School potrà consolidare il processo di crescita e internazionalizzazione della scuola di volo dell’Aeronautica Militare.

ENGLISH

M-345 is a basic-advanced, lightweight trainer jet developed by Alenia Aermacchi for the basic-advanced stage of pilot training. The new aircraft is designed to meet various training requirements of armed forces worldwide.
Based on developments on the M-311 demonstrator, the cost-effective M-345 trainer offers reduced acquisition and lifecycle costs in comparison to heavyweight turboprop trainers.
The maiden flight of M-345 was conducted in December 2016.

M-345 HET (High Efficiency Trainer) variant

M-345 HET is an advanced version of the M-345 jet trainer. Alenia Aermacchi and the Secretariat General of Defence/National Armaments Directorate of the Italian Ministry of Defence signed an agreement in June 2013 to jointly develop the M-345 HET.
By 2020, the M-345 variant will replace the ageing fleet of MB-339 aircraft currently in service with the Italian Air Force.
The Italian Air Force placed a €300m ($338.5m) order for 13 additional aircraft in June 2019. The first aircraft delivery is expected to take place in 2020.
“The new aircraft will meet various training requirements of the armed forces across the world.”
M-345 is a light, tandem twin-seat shoulder wing aircraft. The strengthened airframe offers fatigue life of 15,000 flight hours. It integrates a retractable tricycle landing gear and a single turbofan engine.
Improved features of the M-345 include integrated pressure refuelling and a two-level maintenance concept, which minimises operating costs. Together with the trainer jet’s on-board oxygen generating system (OBOGS), operators can reduce the manpower required for ground maintenance, and turnaround times to conduct more sorties a day.
The M-345 has an overall length of 9.85m, a wingspan of 8.47m, and a height of 3.74m. The aircraft has an empty weight of 3,300kg, a maximum take-off weight of 4,500kg, and a wing area of 12.6m². The external load carrying capability makes the M-345 suitable for secondary missions.

M-345 cockpit and avionics

M-345’s advanced glass cockpit can accommodate two crew members in tandem configuration.
The fully digital glass cockpit is equipped with hands on throttle-and-stick (HOTAS) controls and three 5in x 7in LCD multi-function displays (MFDs) for instructors and student pilots.
“Together with the trainer jet’s on-board oxygen generating system (OBOGS), operators can decrease the manpower required for ground maintenance, as well as turnaround times to conduct more sorties per day.”
The forward cockpit is fitted with a head up display (HUD), while the rear cockpit is installed with a HUD repeater.
Cockpit features include night vision goggles (NVGs) compatibility, along with an integrated global positioning system (GPS) or inertial navigation system (INS), digital moving map, and two mission computers.
The trainer jet is also equipped with an embedded tactical simulation suite that was successfully integrated on the MB-339 and M-346 advanced trainers produced by Alenia Aermacchi. The aircraft also integrates a stores management system (SMS).
Similarities between the M-345 and M-346 cockpits and the respective training syllabuses also ensure interoperability during joint training operations.

M-345 engine details

M-345 is powered by a turbofan engine developing a maximum thrust of 1,600kg (3,500lb) at take-off. Fuel is supplied by an internal tank with a storage capacity of 700kg.
The new M-345 HET is powered by Williams International’s FJ44-4M engine, which offers increased fuel efficiency.
The health and usage monitoring system (HUMS) aboard the aircraft provides information on the structure, engine, and other systems to monitor the operational status of each single component/system.

Performance of the M-345 trainer aircraft

M-345 trainer can fly at a cruise speed of 420KTAS. The certified service ceiling of the aircraft is 40,000ft.
The aircraft has a rate of climb of 5,400ft/min. It can reach a distance of 840nm, but the ferry range can be extended to 1,100nm by integrating two external tanks (10% reserve).
The aircraft has limit load factors of +7/-3.5g at 3,300kg take-off weight. The lengths of ground run required for take-off and landing of the aircraft are 460m and 450m, respectively.

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Il SIDAM 25 è un semovente antiaereo di concezione italiana, ma basato sullo scafo del trasporto truppe corazzato M113



Il SIDAM 25 è un semovente antiaereo di concezione italiana, ma basato sullo scafo del trasporto truppe corazzato M113 (con leggere modifiche), per cui si potrebbe considerare l'interpretazione del concetto dell'M163 VADS, solo con diversa torretta.
Entrato in fase di sviluppo attorno alla metà degli anni ottanta, arrivò in un tempo molto ridotto anche in produzione, nel 1989 presso la Otobreda, e poteva disporre di una portata utile di 2500 metri aprendo il fuoco contro bersagli a bassa quota con discreta precisione.




Nella nuova e più grande torretta, l'unico elemento interamente nuovo del progetto, invece che un singolo cannone a canne rotanti come nel caso dell'M163, sono ospitati ben 4 cannoni a canna singola da 25 mm svizzeri Oerlikon KBA: si può considerare una sorta di incrocio tra l'M163 VADS e lo ZSU-23-4 Shilka. La torretta può ruotare di 360° e sparare ad un alzo compreso tra -5° e +87°.
Il SIDAM ha un telemetro laser con la portata di 10.000 m circa invece che un radar come nei mezzi più vecchi, oltre ad una termocamera per la visione notturna e il calcolatore digitale. Non possiede una autonoma capacità ognitempo di sorveglianza e scoperta di obiettivi aerei per la mancanza di un radar, il che se non altro impedisce che l'aereo preso di mira sia messo in preallarme da sensori. Il Sidam poteva in pratica operare solo di giorno e preferibilmente con buon tempo.

Ha in dotazione munizioni per 15 secondi di fuoco continuato, su 4 contenitori per un totale di 600 colpi in funzione antiaerea. 

Oltre a questi, porta a bordo 40 colpi APDS (Armour Piercing Discarding Sabot) proiettili perforanti da usare contro i bersagli terrestri equivalenti come VTT o blindati leggeri. Sebbene i quattro 25 mm rappresentino una concentrazione di fuoco micidiale con la loro cadenza di 2400 colpi al minuto, la capacità dei contenitori è limitata e le operazioni di caricamento richiedono diversi minuti. Lo spazio interno è insufficiente e il mezzo non è anfibio come i veicoli da cui è derivato.
Avendo una capacità di ricerca indipendente limitata, in situazioni operative il SIDAM viene asservito ad un radar di scoperta utilizzato a livello di batteria, cosa non sempre pratica in una battaglia di movimento. Estremamente arduo è comprendere come esso non abbia seguito la via dei veicoli leggeri di scuola francese, come i M3 VDA, ovvero con soli 2 cannoni ma anche spazio per un radar di ricerca e controllo del tiro (ovvero, "meno denti e più occhi"). Nella configurazione scelta il SIDAM è decisamente un mezzo squilibrato nelle sue caratteristiche.
Il motore è un sei cilindri diesel Detroit 6V-53T, da 266 cavalli, in grado di spingere il mezzo a 69 km/h, e di permettergli di scavalcare ostacoli verticali fino a 61 centimetri, fossati fino a 168 cm e inclinazioni fino al 60%.

Malgrado i suoi limiti sono stati costruiti ben 275 SIDAM, ricavati da M113 già esistenti, con motore diesel degli ultimi lotti; la spesa complessiva è stata di 800 miliardi di lire del 1992. 

Il progetto iniziale prevedeva addirittura l'acquisizione di 350 esemplari, praticamente uno per ogni plotone di 4 carri, ridotti solo in seguito alla contrazione degli organici dell'esercito. A titolo di paragone, l'esercito tedesco con 3500 carri aveva 420 semoventi Gepard e 140 Roland, quello francese 1300 carri e 60 semoventi, l'Olanda possedeva 900 carri e 95 Gepard. La dimensione del progetto e i tagli dei costi verosimilmente ostacolarono il progetto OTOMATIC. Date le limitate caratteristiche il semovente è stato ritirato dai servizi operativi e messo in riserva.

ENGLISH

The SIDAM 25 is a self-propelled anti-aircraft anti-aircraft of Italian design, but based on the hull of the US M113 armoured troop transport (with slight modifications), so the interpretation of the M163 VADS concept could be considered, only with a different turret.
It entered the development phase around the mid-eighties, arrived in a very short time also in production, in 1989 at the Otobreda, and could have a useful range of 2500 meters opening fire against targets at low altitude with fair accuracy.
In the new and bigger turret, the only entirely new element of the project, instead of a single rotating barrel cannon as in the case of the M163, are housed as many as 4 Swiss Oerlikon KBA 25 mm single barrel guns: it can be considered a sort of cross between the M163 VADS and the ZSU-23-4 Shilka. The turret can rotate 360° and fire at a lift between -5° and +87°.
The SIDAM has a laser rangefinder with a range of about 10,000 m instead of a radar as in older vehicles, as well as a night vision camera and digital calculator. It does not have any autonomous surveillance and detection capability due to the lack of a radar, which at least prevents the targeted aircraft from being alarmed by sensors. sidam could in practice only operate during the day and preferably in good weather.
It is equipped with ammunition for 15 seconds of continuous fire, on 4 containers for a total of 600 rounds in anti-aircraft operation. In addition to these, it carries 40 APDS (Armour Piercing Discarding Sabot) armor-piercing projectiles to be used against equivalent land targets such as VTT or light armor. Although the four 25mm represent a deadly concentration of fire at a rate of 2400 rounds per minute, the container capacity is limited and loading operations take several minutes. The interior space is insufficient and the vehicle is not as amphibious as the vehicles from which it is derived.
Having a limited independent search capacity, in operational situations the SIDAM is subjugated to a detection radar used at battery level, which is not always practical in a battle of movement. It is extremely difficult to understand how it has not followed the path of the light vehicles of the French school, such as the M3 VDA, i.e. with only 2 cannons but also space for a search and fire control radar (i.e. "less teeth and more eyes"). In the chosen configuration the SIDAM is definitely an unbalanced vehicle in its characteristics.
The engine is a six-cylinder Detroit 6V-53T diesel engine, with 266 hp, able to push the vehicle at 69 km/h, and allow it to overcome vertical obstacles up to 61 cm, ditches up to 168 cm and inclinations up to 60%.
In spite of its limitations, 275 SIDAM were built, made from existing M113s, with diesel engine of the last lots; the total cost was 800 billion lire in 1992. The initial project even foresaw the acquisition of 350 units, practically one for each platoon of 4 wagons, reduced only after the reduction of the army personnel. By way of comparison, the German army with 3500 wagons had 420 self-propelled Gepard and 140 Roland, the French army had 1300 wagons and 60 self-propelled, the Netherlands had 900 wagons and 95 Gepards. The size of the project and the cost cuts were likely to hamper the OTOMATIC project. Due to its limited characteristics, the self-propelled wagon was withdrawn from operational services and placed in reserve.

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