Tuesday, 30 April 2019

Antonov An-178 Specs, Cargo Payload, Engine, and Price

Antonov An-178 Specs, Cargo Payload, Engine, and Price – The Antonov An-178 is a medium-short haul transport aircraft currently being developed by Antonov, a company based in Ukraine. The first An-178 prototype was launched in Kyiv on April 16, 2015. The aircraft will be available in civil and military configurations, and will replace old aircraft such as the Antonov An-12, Antonov An-26 and Antonov An-32.

Construction on the second An-178 aircraft began in March 2015 while the aircraft's first flight was expected to take place at the end of 2015. An-178 is expected to face potential competition from Alenia C-27J Spartan, EADS CASA C-295, Lockheed Martin C-130J, Embraer KC-390 and Ilyushin Il-214.

Antonov An-178

Antonov An-178 Specs

The An-178 is based on An-158 aircraft produced by Antonov. The fuselage is built with aluminum alloy and composite materials. A semi-monocoque aircraft with a round cross section integrating wings, wing wings, and T-tail that is being swept away. This includes a retractable landing gear with two main bogie wheels and one nose wheel.

The AN-178 base platform can be developed into a number of civil and military variants. The fuselage and onboard equipment are combined with the AN-148 and AN-158 aircraft.

The aircraft can carry 99 soldiers, 80 paratroopers or evacuate 70 sick and injured people. This can be used in various missions including troop logistical support, parachute drooping cargo on platforms or small troop divisions, carrying injured personnel, and light vehicle transportation. This can also be used to transport and send equipment and machinery.

The aircraft has a wider and full-pressure cargo compartment, which can carry up to 18 tons of cargo over 1,000 km. It has a cargo capacity above 10t and can reach a range of more than 4,000 km. It can accommodate high capacity 1C containers with a lateral size of 2.44m х 2.44m, and IATA maritime and container containers.

Antonov An-178 specs

Antonov An-178 Engine

The An-178 transport aircraft is powered by two D-436-148FM turbofan engines developed by Ivchenko-Progress. Each machine produces takeoff thrust of 7.880kgf. D-436-148FM has a dry weight of 1,450kg and an inlet diameter of 1,390mm.

Antonov An-178 cockpit

Antonov An-178 Cockpit and Avionics

This aircraft is equipped with digital avionics, and a glass cockpit. It can fly in intensive air traffic, under VFR and IFR weather conditions both day and night. It can take off and land on non-paved runways and gravel-covered surfaces.

The flight deck integrates a dual duplex fly-by-wire system with two control channels including the FCS-A and FCS-B sections. This also includes flight simulators for training flight crews.

The flight control surface of the aircraft is an aileron, four control spoilers, six lift-dump / speed-brake, steering and elevator spoilers, and an emergency mechanical cable backup system.

Antonov An-178 Price and Orders

The price of the latest 178 aircraft is around US $ 40 - 70 Million. In March 2015, Maximus Air signed an MoU with Antonov to order an undisclosed number of An-178 twinjet civil variants. Maximus will be the customer for the launch of the An-178 aircraft.

Monday, 29 April 2019

Antonov An-148 Specs, Cabin, Engine, and Price

Antonov An-148 Specs, Cabin, Engine, and Price – The Antonov An-148 is a twin-engine commercial aircraft designed by Antonov Aeronautical Scientific and Technical Complex from Ukraine. This aircraft is produced by SE Kyiv Aviation Plant Aviant and Voronezh Aircraft Building Stock Company (VASO), part of United Aircraft Corporation (UAC). The main models in the An-148 class are An-148-100, whose variations include An-148-100A, An-148-100B and An-148-100.

An-148-100 is a passenger aircraft with a wide range of up to 4,400 km with up to 85 seats. All variants have similar airframes. An-148-100A is a short-haul passenger plane (2,000 km-3,000 km) with up to 85 seats. An-148-100B is a passenger aircraft with an extended range of 3,600 km with up to 85 seats.

Other variants of this class include the stretched version of the An-158 or An-148-200 fuselage, the An-168 business variant and the An-178 cargo variant. The An-168 can accommodate 8 to 40 passengers and has a higher range (up to 7,000 km). An-178 has a higher 25t load capacity.

An-148 made its first flight on December 17, 2004 and certification testing was completed in December 2006. The first An-148 series aircraft produced by VASO JSC completed its inaugural flight on July 28, 2009. The first international commercial flight from An-148 was made from Odessa to Moscow on December 13, 2009.

Antonov An-148

Antonov An-148 Specs

An-148 combines a high wing monoplane design. It has the highest weight efficiency in its class due to the use of titanium alloys in structural components. This aircraft is equipped with bulletproof doors and anti-thief devices. Additional space is provided for the storage of weapons and ammunition.

Two turbofan jet engines are installed in pods under the wing. This arrangement protects the engine and wing structure against damage from foreign matter (FOD). Advanced aircraft systems and wing configurations allow aircraft to use all types of aerodromes including airfields that are not well equipped.

The tricycle type landing gear consists of a nose landing gear, right and left main landing gear. The main landing gear pulls back into the well on the fuselage.

Antonov An-148 Engine

The An-148 is powered by two high D-436-148 bypass turbo fans developed by Ivchenko-Progress. Each engine provides a maximum takeoff boost of 6.830Kgf. Automatic control and monitoring systems optimize engine performance.

An-148 has a cruising speed of 800 km / h-870km / hour. The maximum load range is 3,500 km. The aircraft can fly at a maximum flight height of 12,200 m. The maximum take-off weight is 41.55t and the maximum payload capacity is 9t. The aircraft can operate at temperatures on land ranging from -55 ° C to + 45 ° C.

Antonov An-148 Cabin and Interior

The layout of the passenger cabin is designed to combine different seating configurations including economic, business and VIP arrangements. Passenger capacity can vary from 10 to 85 based on configuration. Cabin layout includes service areas, individual and public areas. The passenger compartment has a modern seat and information entertainment system.

Shelves near the head that can be closed are available for handbags. The 4.2m³ space allocated for these shelves is the largest in regional aircraft classes and short distances.

The luggage compartment and cargo measuring 14.6 m³ are provided under the passenger compartment floor and on the tail. The noise level in the cabin is very poor and meets all international flight standards.

Antonov An-148 cockpit

Antonov An-148 Cockpit and Avionics

An-148 has a partial glass cockpit that can accommodate four crew members. The cockpit is equipped with five 6in × 8in multifunctional LCDs developed by Aviapribor and fly-by-wire flight controls.

Modern avionics suites include navigation and radio communication equipment, multifunction indicators and fly-by-wire systems that are compatible with VFR and IFR weather conditions, day and night. The onboard video surveillance system allows the crew to monitor passenger compartments and service areas.

Antonov An-148 Price and Orders

The price of the latest An-148 aircraft is around US $ 20 - 30 Million. Antonov built two An-148 prototypes in 2004 and 2005. The first prototype was being operated by Aerosvit Airlines and the second was stretched in 2009 to create An-158 (An-148-200). First orders were received from Ilyushin Finance (IFC) in April 2005. Seven planes were produced at Aviant, while VASO sent three aircraft to the aggregate of Kyiv.

Russian airlines, Ukraine and Kazakhstan expressed interest in buying around 100 An-148 aircraft. The KrasAir, Polyot, SCAT and Berkut airlines have signed a contract to purchase An-148 aircraft.

In June 2009, Atlant-Soyuz Airlines signed a memorandum of understanding for 30 An-148 jets. In November 2010, the Russian Emergency Ministry ordered two An-148-100 jets to be produced by the VACO UAC plant. Deliveries are planned for 2012 and 2013.

In March 2010, UAC signed a contract with three unscheduled domestic airlines based in India for 18 An-148 aircraft.

Sunday, 28 April 2019

Antonov An-140 Specs, Cabin, Engine, and Price

Antonov An-140 Specs, Cabin, Engine, and Price – The Antonov An-140 is a twin-engine passenger / cargo aircraft designed and developed by the Antonov Aeronautical Scientific and Technical Complex of Ukraine to operate on regional air routes. It was built to replace the An-24 aircraft which has been operating for 40 years. A total of 25 An-140s were operated worldwide in August 2010. An-140 has six variants which include An-140-100, An-140A, An-140T, An-140TK, An-140VIP Executive and An-142.

An-140-100 is a military version that was built in 2003 to replace the old An-24, An-26 and Yak-40. This variant runs maritime patrols, medical, aerial photography, geological exploration, transportation, and fisheries exploration missions. This extended aircraft feature, maximum take-off weight is higher and longer range.

The An-140A is an advanced version of the An-140, powered by the Pratt & Whitney PW127A turboprop engine. An-140T is a shipping model powered by TV3-117-SBM3 engines. Used by the Russian Navy, this variant is equipped with a large cargo door on the rear of the aircraft. An-140VIP carries 30 passengers.

Antonov An-140

Antonov An-140 Specs

An-140 development began in 1993 at the Kharkov Aircraft Production Plant in Ukraine. Production was also assigned to its partner AVIACOR Aviation Plant JS (Samara, Russian Federation). Three An-140 prototypes were built, the first came from the Kiev Factory in June 1997. The prototype took off for its inaugural flight in September 1997 and began operations in October 1999. The second prototype was introduced in 1998.

The An-140 has a conventional design and operates both day and night even under the worst climate conditions. The AI9-3B auxiliary unit integrated in the tail of the fuselage allows planes to take off and land from semi-prepared airfields, unpaved airfields, snow-covered ice fields and short runways.

The An-140 has a passenger entrance with a built-in ladder on the back of the aircraft. This aircraft is equipped with a goods door on the right front to load or lower the cargo. It also houses mating connectors, wing navigation red lights, air holes, clamp roads and warning horns provided by Goodrich Corporation.

The aircraft is equipped with a ventilation system, multichannel entertainment system, noise absorbing panels, cargo hold, cargo loading system, and a strong tricycle landing gear consisting of low pressure tires.

Antonov An-140 Engine

The An-140 is powered by two TV3-117VMA-SBM1 turboprop engines driven by two six-bladed AV-140 composite propellers. Each machine can produce 1,838kW of output power. The machine was produced by Ivchenko Progress Zaporozhye, Klimov Scientific Industrial Company and Motor Sich. The engine is 2.9m long, 0.98m wide and 1.2m high. The dry weight is 570kg.

An-140 can rise at the level of 6.8m / s. The maximum speed and cruising of each aircraft are 575 km / h and 460km / h. The maximum distance is 1,380 km and the ferry range is 3,680 km. The service ceiling is 7,600 m. The aircraft takeoff distance is 1,750 m and the landing distance is 1,360 m. The aircraft can operate at ambient temperatures ranging from -550C and + 450C from an airfield located 2,500m above sea level.

Antonov An-140 cabin interior

Antonov An-140 Cabin and Interior

An-140 has a large cabin with plenty of space for passengers. The cabin holds 52 passengers in a four-seat configuration parallel. It is divided into three zones which include an exclusive lounge with four seats, a business class equipped with 22 seats and an economy class with 26 seats.

The aircraft also offers luggage and cargo compartments with a volume of 9.1 m below the passenger cabin and at the rear of the aircraft. It can accommodate 1.84 tons of goods, which is 1.3 to 1.5 times greater than the capacity of conventional aircraft from the same category. Pallets can be placed on the front of the passenger cabin.

Antonov An-140 cockpit

Antonov An-140 Cockpit and Avionics

Flight decks accommodate two crew members: pilots and co-pilots. It is equipped with a voice recorder, weather radar, distance measuring equipment, automatic flight control systems, magnetic compass, CO-72M transponder, CH-3301 global navigation system, ground proximity warning system, emergency rescue radio station, emergency rescue radio station, transmitter emergency and environmental system settings.

Antonov An-140 Prices and Orders

The price of the latest An-140 aircraft is around US $ 9 - 11 Million. Orders received for An-140 from various customers include: Antonov Airlines (three), Ilyich-Avia (two), Motor Sich (three), Air Libya Tibesti (five), Yakutia Airlines (eight), Russian Ministry of Defense (seven) ), Safiran Airlines (two), Iran Air Tours (eight) and Aeroflot (25). The Russian Air Force ordered seven An-140s from Ukraine in May 2011, reports M & C.

Saturday, 27 April 2019

Sukhoi Su-34 Fighter Bomber Specs, Engine, Cockpit and Price

Sukhoi Su-34 Fighter Bomber Specs, Engine, Cockpit and Price – Sukhoi Su-34 is a combat bomber aircraft developed by the Sukhoi Design Joint Stock Company, Moscow and the Novosibirsk Aircraft Production Association in Novosibirsk, Russia. The Su-34 replaces the Tu-23M and Su-24 aircraft. This is one of a number of Russian aircraft based and developed from the Su-27 Flanker, including the Su-30, Su-33 and Su-35.

Sukhoi Su-34 by NATO named Fullback is a double-seat fighter aircraft with a configuration side by side and projected as a maritime fighter. Su-34 has a cruising power without re-fueling reaching 4,000 km and with 3 times re-fuelling capable of exploring up to 14,000 km, it is suitable for fighter and maritime patrol aircraft that require a fairly wide roaming power. This aircraft can attack targets in various weather conditions, day or night.

Sukhoi Su-34 Fullback Fighter Bomber

Sukhoi Su-34 Specs

The Su-34 design maintains the basic layout and construction of the Su-27 fuselage, as well as the same wing-high configuration and conventional onboard equipment.

The Su-34 has a changing contour from the nose to accommodate a phased array radar, multi-mode, step by step with terrain and field avoidance mode. It has a two-seat cockpit and not a single seat and the internal fuel tank capacity has increased with the result of increased takeoff weight. Changes have been made to the middle tail boom for rear-facing radar.

Sukhoi Su-34 specs

Sukhoi Su-34 Weapons

Sukhoi Su-34 is armed with 30mm GSh-301 weapons and 180 rounds of ammunition. The gun has a maximum firing rate of 1,500 revolutions per minute and the muzzle velocity is 860 m / s. This was provided by the Instrument Design Bureau, Tula.

This aircraft has ten hardpoints for weapons and is capable of carrying various missiles, including air to air, air to surface, anti-ship missiles and anti-radiation, guided and directed bombs, and rockets. This aircraft is equipped with a target pointer.

The R-73, Nato codename AA-11 Archer, a short-range air-to-air missile supplied by the State Technical Design Bureau of Vympel, Moscow. The R-73 is an all-aspect missile capable of pulling targets in tail-chase or head-on mode. The missile has cooled infrared homing.

The R-73 attacks the target in the target designation angle of ± 45 ° and with angular speeds of up to 60 ° per second. Missiles can intercept targets at an altitude of between 0.02 km and 20 km, and target G-loads up to 12g, with a target speed of up to 2,500 km / hr.

Also known as RR-77 or as NATO AA-12, the RVV-A long-range air-to-air missile is manufactured by Vympel. Missiles can intercept targets at speeds of up to 3,600 km / h and altitudes from 0.02 km to 25 km. The minimum range in the rear hemisphere is 300 m and the maximum vertical separation between the parent plane and the target is 10 km.

RR-77 has an inertial guide with radio updates in the middle of the road and active terminal guides. The new version of the R-77 with a longer range (R-77), with solid fuel ram-jet propulsion, is being tested by Vympel.

The Su-34 carries a series of precision and non-guided guided bombs and rockets, including the KAB-500 laser guided bomb developed by the State's Research and Production Company, Moscow.

Sukhoi Su-34 engine

Sukhoi Su-34 Engine

The first production of Sukhoi Su-34 was powered by two Saturn N-31F NPO turbofan engines. Then the aircraft can be equipped with the Salyut AL-31F-M2 / 3 MMPP engine or the Saturn 117 NPO. They are mounted under the wing and equipped with geometric air intakes which remain all tasks. The rotor protection installed in the air intakes provides protection against ingestion of foreign matter.

Internally, the aircraft can carry 12,100 kg of fuel in two fuel tanks on the wing and four on the plane. Three external 3000l fuel tanks can also be installed.

The aircraft can reach 1,900 km / h (Mach 1.6) at altitude and 1,300 km / h (Mach 1) at sea level, and has a flight range of 4,000 km.

Sukhoi Su-34 cockpit

Sukhoi Su-34 Cockpit and Avionics

The cockpit has two zero / zero K-36DM ejection seats side by side for pilots and co-pilots. The seats are provided by the Zvesda Research and Production Enterprise Joint Stock Company, Moscow. The multifunction screen in the cockpit shows flight parameters, aircraft unit operational status, and tactical data.

The Su-34 is equipped with an electro-optical fire control system, supplied by the Urals Optical and Mechanical Plant (YOM3), and the FLIR Geophysics pod, with infrared looking forward. Leninetz from St. Petersburg supplies a phased phased array array system and TsNIRTI suite of electronic countermeasures.

The Russian Air Force ordered 32 Su-34 aircraft in 2008, with additional requirements for 92 aircraft in 2012. The first two production aircraft were sent to the Russian Air Force in December 2006. The Su-34 export appointment was a Su-32.

Sukhoi Su-34 Price and Orders

The price of the latest Su-34 fighter bomber aircraft is around US $ 36 Million. Full production began in January 2008. In the same month, the Russian Air Force stated that 70 aircraft would be secured by 2015. Under a state contract with the Russian Ministry of Defense, Sukhoi will send Su-34 bombers to the Russian Air Force and military units until 2020.

Sukhoi Su-35 Fighter Specs, Engine, Cockpit, and Price

Sukhoi Su-35 Fighter Specs, Engine, Cockpit, and Price – Sukhoi Su-35 is a sophisticated multirole air superiority fighter aircraft developed from the Su-27. This aircraft has high maneuverability (+ 9g) with high angle attack, and is equipped with a high-capable weapon system that contributes to the extraordinary air combat capabilities of the new aircraft. The maximum level speed is 2,390 km / h or Mach 2.25. The latest version of the Sukhoi Su-35, Su-35BM (bolshaya modernizatsiya - great modernization).

Sukhoi Su-35 was developed to rival the F-15 Eagle and F-16 Fighting Falcon. This aircraft was developed, tested and introduced into serial production by the Sukhoi Design Bureau, based in Moscow, and produced by KNAPPO from Komsomolsk-on-Amur. The two companies are part of the Sukhoi Aviation Joint Stock Company.

The Su-35 flight test began on February 18, 2008. During a high-speed land test in April 2009, the third prototype of the Su-35 program crashed at Komsomolsk-on-Armur. The accident damaged the new NIIP Irbis-E radar set installed on the Su-35.

Sukhoi Su-35 Fighter

Sukhoi Su-35 Specs

Compared to the design of the Su-27 where it came from, the front body diameter of the Su-35 has been increased to accommodate 900mm diameter antennas larger than the Irbis-E radar.

High strength, low weight composite materials have been used for non-structural objects such as radomas, nose wheels, front doors and flaps. Some aircraft body structures are made of carbon fiber and aluminum lithium alloys.

Sukhoi Su-35 Weapons

This aircraft has 12 hardpoints to carry weapons and external stores. Each wing has four sticks - one on the wingtip and three stations under the wing. There are two hard points on the underside of the fuselage in the center line and one under each engine.

Air-to-air missile aircraft can include Vympel R-27 (designation of AA AA-10 Alamo), radar guided mid-range radar Vympel R-77 (AA-12 Enhancer) and infrared infrared-guided Vympel short range R-73E (Archer AA-11).

Air-to-surface missiles include Molniya Kh-29 (AS-14 Kedge) tactical missiles, Kh-31P (AS-17 Krypton) anti-radiation missiles and Kh-58UShE (AS-11 Kilter) long range anti-missile radiation.

Su-35 anti-ship missiles include the Kh-31A, the Kh-59MK long range (AS-18 Kazoo), long-range Kalibr, and the heavy YPO Mashinostroenia long-range missile.

Sukhoi Su-35 can be armed with a number of guided bombs, including TV-guided KAB-500Kr bombs, KAB-500S-E satellite guided bombs, LGB-250 laser guided bombs, bombs guided by TV Kab-1500Kr and KAB laser guide bombs. -1500LG.

The aircraft can also be armed with 80mm, 122mm, 266mm and 420mm rockets. Gryazev-Shipunov 30mm GSh-30-1 weapon is installed in the right wing root with 150 rounds of ammunition.

This suite of aircraft electronic warfare includes a radar warning system, radar jammer, cooperative radar interference system, missile approach warner, laser warner and chaff and flare dispensers.

Sukhoi Su-35 engine

Sukhoi Su-35 Engine

Sukhoi Su-35 is powered by two Sturn / UFA AL-31F 117S turbofan engines with thrust vectoring nozzle controls, each supplying thrust of 86.3kN or 142.2kN with afterburn. The machine was developed jointly by Sukhoi, Saturn and UMPO.

The total fuel capacity is 14,350l. To increase coverage and higher durability compared to previous models, the Su-35 incorporates additional tailin and root fin tanks. The fuel tank is made of aluminum lithium construction and is located on the wing, fuselage and at the end of the twin tail-tip. The unreferred range of internal fuel is 1,580 km.

For refueling in flight, the aircraft is equipped with a refueling probe on the side of the nose. Two external fuel tanks, the PTB-2000 type, provide an additional 4,000 l of fuel. Ferry range with two external tanks is 4,500 km.

This aircraft can fly with a maximum speed of 2,390 km / hour. The normal range and ferries of each aircraft are 3,600 km and 4,200 km. The maximum height is 18,000 m. The Su-35 weighs around 18,400 kg and the maximum takeoff weight is 34,500 kg.

Sukhoi Su-35 cockpit

Sukhoi Su-35 Cockpit and Avionics

Sukhoi Su-35 cockpit is equipped with two high resolution 230mm x 305mm MFI-35 liquid crystal screens with a multifunctional control panel and IKSh-1M main screen with a wide viewing area of ​​20 ° x 30 °. The cockpit has a central control column and is equipped with a zero-zero Zvesda K-36D-3.5E ejection seat that allows the pilot to launch zero speed and zero altitude.

This aircraft has a quadruplex, digital fly-by-wire control developed by Avionika Moscow Research and Production Complex JSC (MNPK Avionika).

The pilot has two VHF / UHF encrypted radio communication systems and a jammed military data connection system between squadron planes and between aircraft and ground control. The navigation system is based on a digital map display with a strapdown inertial navigation system and a global positioning system.

Su-35 Radar consists of a multimode X-band phased series, Irbis-E, supplied by the Tikhomirov Research Institute for Research-Scientific Design (NIIP), based in Zhukovsky. Irbis-E is a high-performance radar designed for Su-35 aircraft.

The 900mm phase phased array antenna is mounted on a hydraulic actuator for mechanical steering. Electronic steering provides azimuth and 60 ° altitude coverage. With mechanical and electronic scanning the coverage is 120 °.

The radar can detect low and clandestine observable aircraft, unmanned aerial vehicles and missiles with a radar cross section of 0.01 m² at distances of up to 90 km. Radar mode includes air to air, air to land, air to sea, mapping, Doppler rays, and synthetic radar aperture modes. It can detect and track up to 30 airborne targets with a 3m² radar section section (RCS) at a distance of 400 km using track-while-scan mode.

The search control and infrared fire tracking system, OLS-35 IRST, includes infrared sensors, laser scouts, target designers and television cameras. The accuracy of the laser rangefinder is the CEM 5m (probability of circular error), up to a maximum range of 20 km against targets in the air and 30km against targets on land. OLS-35 is a high-performance system with ± 90 ° azimuth and height coverage + 60 ° / -15 °.

The system acquisition range against non-afterburning targets is 50 km forward and 90 km backward. The Su-35 can also be equipped with targeting UOMZ Sapsan and laser designation pods.

Sukhoi Su-35 Price and Orders

The price of the latest Su-35 fighter aircraft is around US $ 45 - 65 million. The first Su-35 aircraft was handed over to the State Flight Test Center (GLITS) to 929 for flight testing in August 2011. The Russian Ministry of Defense received six Su-35 production aircraft from Sukhoi in December 2012.

The Russian Air Force ordered 48 Sukhoi Su-35 jets in August 2009 with deliveries scheduled to run until 2015. Sukhoi began producing components needed for aircraft assembly in November 2009. The information management system is integrated with the onboard subsystem and new phased arrays. radar systems with detection of long-range air targets have been installed on the aircraft, which are currently undergoing preliminary testing.

Thursday, 25 April 2019

Sukhoi Su-57 (T-50) PAK-FA Specs, Engine, Cockpit, and Price

Sukhoi Su-57 (T-50) PAK-FA Specs, Engine, Cockpit, and Price – Su-57 PAK-FA is a multirole stealth fighter aircraft developed by Sukhoi from Russia. This will be used to meet the requirements of the Russian and Indian Air Force. The first prototype of the PAK-FA Su-57 aircraft had made its inaugural flight for 47 minutes on 29 January 2010 at Komsomol'sk-na-Amur Airport, and was introduced in 2013. This is a fighter aircraft developed by Sukhoi since the collapse of the Soviet Union .

The PAK-FA Su-57 will replace the previous MIG-29 Fulcrum and Su-30 MKI Flanker aircraft. It will compete with the F-22 Raptor and the F-35 Lightning II US. The development of the PAK-FA Su-57 aircraft began in March 2007. Manufacturing work was carried out at Komsomol'sk-on-Amur by the Novosibirsk Chkalov Aviation Production Association (NAPO Chkalov).

The final assembly of the body in front of the aircraft was carried out at Komsomol'sk-on-Amur in 2009. The first flight test was delayed due to technical problems. The first prototype of the aircraft was developed in February 2009. Then, in January 2010, the aircraft successfully completed the initial path.

Sukhoi Su-57 PAK-FA

Sukhoi Su-57 PAK-FA Specs

The Sukhoi Su-57 is designed to perform supersonic at speeds of more than 2,000 km / h along with refueling on maintenance flights. This will show short takeoff and landing capabilities, and can achieve greater agility, low radar visibility and low heat signatures. The plane does not have a steering wheel. The design of the tail fin is similar to that of the V-tail incorporated in Northrop YF-23.

Horizontal stabilizers and vertical wing leading devices are used for signature control. The exterior of the aircraft is designed using stealth or low-observable (LO) technology.

The Su-57 PAK-FA aircraft radar has been designed based on the Su-35BM system. Tikhomirov NIIP the instrument design bureau has sent radar, Irbis N035 on the plane. The Su-57 prototype is also equipped with an active antenna system and three X-band radars (front and side view), Ku-band ventral radar equipped with friends or enemies (IFF), actively contacted electronic radar arrays (AESA) and subsystems electronic warfare.

Sukhoi Su-57 specs

Sukhoi Su-57 PAK-FA Weapons

Armament incorporated in the Sukhoi Su-57 PAK-FA aircraft uses two 30mm Gsh-30-1 internal cannon and R-77 missile fiber. This aircraft has four hard points (four sides in each wing) where the missile is installed.

Gsh-301 is a 30 mm single barrel sent by Izhmash JSC, Russia. The cannon can fire 1,500 to 1,800 rounds per minute and weigh around 64kg.

The R-77 missile is a medium-to-air range missile provided by Vympel, Russia. The weight of the missile is around 175kg. Two large anti-ship bombs weighing 1,500kg each and two missiles developed by the Novator Bureau were installed on the aircraft.

Sukhoi Su-57 engine

Sukhoi Su-57 PAK-FA Engine and Speed

The aircraft is powered by two turbofan Saturn-Lyulka 117S engines (upgraded AL-31). Each machine can produce a maximum thrust of 150kN after the burner. 117S is an improved model of the AL-31F engine.

The Saturn-Lyulka 117 is equipped with modern high and low pressure turbines, a new digital control system, vector push nozzles and a fan with a diameter of 932mm. The age and average time between the engine overhaul (MTBO) is 4,000 hours and 1,000 hours.

The Su-57 can go up at speeds of 350m / s. The maximum speed and cruising of each aircraft are 2.600 km / h and 1,800 km / hr. The range of aircraft varies between 4,000 km and 5,500 km, and the service ceiling is 20,000 m. The maximum durability of the Su-57 is three hours. This aircraft weighs around 18,500 kg and has a maximum takeoff weight of 37,000 kg. This aircraft can reach the target within 400 km.

Sukhoi Su-57 cockpit

Sukhoi Su-57 PAK-FA Cockpit

The sophisticated aircraft has a one-seat cockpit equipped with electronic systems including an automatic flight control system (AFCS) and other additional equipment.

Sukhoi Su-57 PAK-FA Price and Orders

The price of a new Su-57 PAK-FA stealth fighter aircraft is around US $ 50 Million. Request for proposals (RFP) were issued by the Russian Air Force in 1998 to be approved and developed by the Sukhoi Su-57 prototype. The Russian Air Force selected the Sukhoi Design Bureau in 2002 to develop a full-size double-engined fighter aircraft.

About 150 to 200 aircraft orders from the Russian Air Force (RAF) and 200 from the Indian Air Force (IAF) are expected. Production will begin in 2015 after five to six flight tests. About three trials were completed in February 2010.

Wednesday, 24 April 2019

Sukhoi Su-30SM Fighter Jet Specs, Engine, Cockpit, and Price

Sukhoi Su-30SM Fighter Jet Specs, Engine, Cockpit, and Price – Su-30SM is a multirole fighter aircraft developed by the Sukhoi Design Bureau for the Russian Air Force. This is a sophisticated derivative of the family of Su-30MK fighters. Su-30SM fighter planes are designed according to the requirements of the Russian Air Force. It is being produced by IRKUT, a company based in Russia. The first Su-30SM fighter aircraft designed for the Russian Ministry of Defense (MoD) made its maiden flight in September 2012.

Su-30MK fighters operate with the Algerian Air Force, Indian Air Force (IAF), Indonesian Air Force, People's Liberation Army Air Force, Malaysian Air Force, Ugandan Air Force, Uganda Air Force, Venezuelan Air Force and Vietnam People's Air Force.

Multirole Su-30SM can be used in airstrikes, land missions and sea missions. This can do electronic countermeasures and early warning tasks. The aircraft also acts as a command-and-control platform in the fleet of fighter aircraft carrying out joint missions.

Sukhoi Su-30SM Fighter Jet

Sukhoi Su-30SM Specs

Su-30SM fuselage is made of titanium and high strength aluminum alloy. This is based on the Su-30MKI aircraft which was developed jointly by the IRKUT and Sukhoi Design Bureau, for the IAF.

The head of the aircraft has a cockpit, radar parts and avionics bay. High maneuverability is achieved through integral aerodynamic forms combined with thrust vectoring features.

Su-30SM is equipped with a hydraulically retractable tricycle type landing gear. The main landing units are equipped with a single wheel. Each unit retreats through 90 ° to pull forward into the bay at root-wing.

The main landing gear has carbon disc brakes that function hydraulically which are equipped with an electric brake cooling fan and an anti-skid mechanism. A single nose wheel that can be pulled forward can be adjusted hydraulically. The cones on the stern of the fuselage integrate the brake parachute compartment.

Sukhoi Su-30SM engine

Sukhoi Su-30SM Engine

The Su-30SM is powered by two AL-31FP by-pass turbojet engines. The engine produces total thrust after burning 25,000 kgf. The power plant provides a horizontal flight speed of Mach 2.

The maximum unrefined flight range of the Su-30SM is 3,000 km. The aircraft is also equipped with a probe and flight refueling system.

Sukhoi Su-30SM Weapons System

Su-30SM is capable of carrying sophisticated weapons weighing up to 8t. The aircraft can be armed with machine guns, bombs, air-to-air missiles, and Onik (Yakhont) supersonic anti-ship and ground attack missiles. Developed by NPO Mashinostroyeniya, Oniks is the basis for the BrahMos supersonic missiles. Oniks has an operational range of 120 km to 300 km depending on altitude.

This aircraft can carry out air, land and sea level targets by using directed / not directed air-to-air and air-to-surface weapons. It can be equipped with anti-surface weapons such as rockets and rocket pods to carry out ground attack operations.

Sukhoi Su-30SM cockpit

Sukhoi Su-30SM Cockpit and Avionics

The glass cockpit accommodates two pilots in a tandem configuration. The crew is equipped with ejection seats. The cockpit combines a sophisticated avionics suit that integrates the head-up display and multifunctional liquid crystal display.

Su-30SM is equipped with identification of friends or opponents, a global positioning system and an inertial navigation system. Open architectural design enables the integration of modern avionics, including new radar systems, radios and recognition systems, and other support systems.

Sukhoi Su-30SM specs

Sukhoi Su-30SM Price and Orders

The price of a new Su-30SM fighter aircraft is around US $ 37.5 Million. The IRKUT and the Russian Ministry of Defense signed contracts for 30 Su-30SM multirole fighters in March 2012. The Ministry of Defense plans to replace the Su-24 fleet with Su-30SM fighter aircraft.

The Ministry of Defense placed orders for the second batch of 30 Su-30SM fighters in December 2012. The IRKUT sent the first two Su-30SM fighters to the Russian Air Force in November 2012.

The Russian Air Force received four Su-30SM aircraft in February 2016 and the Russian Knight, the Russian Air Force aerobatics demonstration team, received eight units that year. IRKUT sent four units to the Kursk Flight Regiment from the Western Military District (ZVO) in July 2017. The company currently produces 12 Su-30SM fighter planes for the Russian Air Force and two for the Russian Navy.

The company handed over the first batch of Su-30SM multirole fighter aircraft to the Kazakhstan Air Force in April 2015. The Kazakhstan Ministry of Defense signed a contract with IRKUT for another batch of Su-30SM aircraft in May 2018. Aircraft shipments are expected to be completed by 2020.

Tuesday, 23 April 2019

Embraer KC-390 Specs, Engine, Cockpit, and Price

Embraer KC-390 Specs, Engine, Cockpit, and Price – KC-390 is a new generation multi-mission aircraft that combines a very flexible platform with the lowest life cycle costs in the medium air transport market. The KC-390 is capable of transporting and launching cargo and troops as well as carrying out various missions: medical evacuation, search and rescue, humanitarian rescue and rescue, human air refueling (fighters and helicopters), air fire and aid.

Developed according to stringent requirements, the KC-390 is a multi-mission aircraft, with a sturdy design that can withstand operations from semi-finished and damaged runways, and in harsh environments, varying from hot and humid Amazon forests to the Antarctic continent cold freezing, and in hot, sandy desert conditions.

The KC-390 features will be in line with the new National Defense Strategy and meet the needs of the FAB. The new aircraft will replace the 22 Lockheed Martin C-130E / H and KC-130 which are currently part of the FAB.

Embraer KC-390

Embraer KC-390 Specs

The basic characteristics of the KC-390 design also increase the aircraft's ability to survive Key Points: High Speed ​​is similar to fast jet: Mach 0.8; Altitude Height: 36,000 feet; Inertization of the Fuel Tank: OBIGGS; Redundancy and separation for critical systems; Night Vision Compatibility; Tactical radar.

KC-390 can be equipped with a complete self-protection package (SPS) to increase the level of survival. Detection & Control with 360 ° coverage: Radar Warning Receiver (RWR) Laser Warning System (LWS) Missile Warning System (MAWS) Chaff & Flare Directional Infrared Counter Measures (DIRCM). Infrared / Optical Optics; Ballistic Protection (Armor 7.62 mm and 0.50 inches); Enhanced Vision System (EVS); HALO Oxygen Rack.

KC-390 is capable of operating from the maximum (worst) semi-ready runway specified by MIL-A-008866B and, for soft field operations, carries out 10 trajectories on the CBR 4 airfield (loose fine sand or soft clay). The KC-390 has excellent soil maneuverability, and can operate in airfields with limited space for parking or maneuvering and no land facilities.

Small, simple and semi-prepared airfields are important operational environments for military aircraft. The operational capacity of KC-390 on semi-ready and non-paved airfields is achieved with a very capable structure. The Critical Field Long landing gear is designed to operate and reduce damage to non-paved soft air fields. The KC-390 is also equipped with a dual chamber shock absorber system and a modern hydraulic system. The machine is mounted in a raised position to prevent debris from entering.

The twin-turbofan-powered KC-390 can be filled with fuel in flight and can be used for refueling on aircraft or on land from other aircraft. The new Jet 20t is technically sophisticated and has fly-by-wire technology, which optimizes mission results to reduce pilot workload. This also helps improve security and the ability to operate on short and rural runways.

KC-390 uses computed air release point (CARP) technology that is integrated with fly-by-wire systems to provide greater accuracy during air decrease, thereby reducing crew workload.

The twin-engine twin-engined Embraer KC-390 also integrates technology solutions developed for the Embraer 190 commercial aircraft. It is expected to bring 84 military personnel and cargo cabins to be configured to carry injured or sick people, on medical evacuation missions (MEDEVAC). This will also be used for refueling, flight search and rescue missions.

Fuel Refueling

The KC-390 is capable of refueling fixed and rotary aircraft, operating at speeds from 120 KCAS to 300 KCAS and at altitudes from 2,000 feet to 32,000 feet. The KC-390 land refueling capability also serves ground forces with vehicles or moves forward. basic refueling.

Day and night air refueling capabilities with observer windows and night vision cameras. The KC-390 has an advanced fueling pod (912E) that meets the high performance criteria of the aircraft providing a lightweight and efficient solution. Each pod provides fuel transfers of up to 400 USgpm. Additional removable fuel tanks can be installed on the fuselage to expand aircraft fuel loading capacity or range performance.

Humanity Search and Rescue

During the Search & Rescue mission, every minute is important to save lives. The KC-390 turbo fan engine delivers unmatched speed compared to other aircraft in the medium lift segment. The KC-390 can be equipped with a complete set of equipment to support the Search & Rescue mission: Removable Electro-Optical / Infrared pod (EO / IR); Four position scouts; Lateral waste and / or crew seat; Removable internal fuel tank to expand the range or time at the station.

Medical Evacuation

KC-390 provides support for land operations or disaster relief missions that carry victims or injured victims. KC-390 can be configured to carry up to 74 liters (STANAG 2040) and 8 additional members, including medical personnel and necessary life support equipment. KC-390 can be configured to carry up to 74 liters.


When equipped with a roll-on-roll-off fire extinguishing system, KC-390 is an important air source for firefighters in fighting forest fires, dropping water or fire retardants. The KC-390 fly-by-wire provides exceptional maneuverability at low speeds and low altitudes to fly over fire areas, increasing mission efficiency.

Embraer KC-390 specs

Embraer KC-390 Cargo

KC-390 military aircraft have cargo space equipped with rear roads similar to Hercules, and are capable of carrying various types of cargo (weighing up to 26t), including armored vehicles. It is equipped with a sophisticated loading and unloading system to handle cargo.

Cargo floors, an integral part of the main structure of the KC-390, are designed with the power to carry wheeled vehicles weighing up to 26,000 kg (57,320 lb). Optimized tie-down ring grille with 10,000 lb and 25,000 lb in all directions ensures rapid configuration changes and exceptional cargo cargo flexibility. CHS displays all the accessories needed to facilitate loading, containment and disassembly, such as ring binders, roller trays, cargo guidelines, and anchoring systems. It is fully compatible with existing military air transport equipment, such as type V platforms, 463L pallets, A-22 CDS bundles, and supporting loaders on land.

The KC-390 air delivery system provides long-distance and automatic release of cargo at low and high altitudes. KC-390 is capable of: V-type LVAD platforms (single and multiple) up to 41,887 lb; CDS (Container Shipping System) air shipping up to 22 slippage boards; Low-altitude parachute extraction (LAPES) up to 22,046 lb.

Embraer KC-390 Engine

International Aero Engines (IAE) was chosen by Embraer in July 2011 to design, develop, supply, and install a V2500-E5 power plant on the KC-390 aircraft. IAE is a consortium consisting of Rolls-Royce, United Technologies Unit, Pratt & Whitney and Japanese Aero Engine Corp.

IAE sent the first three V2500-E5 powerplants for the new KC-390 Embraer aircraft in early 2014 and the remaining three in May of the same year. The Federal Aviation Administration (FAA) certification for the new engine model was given in August 2014.

KC-390 can fly to a maximum height of 10,973 m. The maximum speed is 987.8 km / hr. The normal range and ferries of the aircraft are 2,590 km and 6,130 km respectively. This aircraft weighs around 23,600 kg and the maximum takeoff weight is 74,400 kg.

Embraer KC-390 cockpit

Embraer KC-390 Cockpit and Avionics

The KC-390 pilot is facilitated by an integrated avionics system and fly-by-wire flight control. Avionics includes two head-up displays (HUD), self defense systems and night-vision goggles (NVG). And it is equipped with ballistic protection which increases its capacity to operate in hostile environments.

Rockwell Collins signed an agreement with EDS in May 2011 to supply Pro Line Fusion avionics for aircraft. The system will provide increased situational awareness and reduce pilot workload. Embraer gave a contract to BAE Systems on July 27, 2011 to supply and install flight control electronics on the KC-390 transport aircraft.

Goodrich Corporation will design, build and supply the main flight control system as part of the agreement signed with Embraer on July 27, 2011. The company will supply electro-hydrostatic actuators, electro-backup electrostatic actuators, electronic actuators and electrical controls.

Embraer KC-390 Price and Orders

The price of a new Embraer KC-390 aircraft is around US $ 55 Million. National Aviation Company Empresa Nacional de Aeronautica (ENAER) from Chile signed a contract with Embraer in August 2010 to jointly build a KC-390 aircraft for the Chilean Air Force (CAF). About six KC-390 aircraft will be purchased by CAF.

The Brazilian Air Force expressed its desire to acquire the KC-390 aircraft at the 47th Farnborough International Airshow held in England in July 2010 and signed a series production contract for the aircraft in May 2014.

The R $ 7.2 billion contract ($ 3.3 billion) will make the company supply 28 KC-395 aircraft for ten years. The contract also includes a logistical support package, including parts and maintenance. Embraer signed a letter of intent (LoI) with SkyTech for the purchase of up to six KC-390 multi-mission aircraft in February 2018.

Monday, 22 April 2019

Embraer EMB-314 Super Tucano Specs, Engine, Cockpit, and Price

Embraer EMB-314 Super Tucano Specs, Engine, Cockpit, and Price – EMB-314 Super Tucano is a turboprop-engined light combat aircraft manufactured by Embraer Defense System, Brazil. EMB-314 Super Tucano is an enhanced version of the EMB-312 Tucano training aircraft, improvements made from previous aircraft including avionics systems, weapons systems and data communication systems. The Super Tucano prototype first flew in 1992.

EMB-312 Tucano is a military aircraft with low operational costs, around USD 1,000 per hour flight. Minimum infrastructure and ground support are needed, rapid error identification and ease of correction & intensive use of the maintenance concept of on-condition.

This aircraft is suitable for basic and advanced pilot training. The aircraft's main mission is border patrol and counter-insurgency operations. In addition, the right air to ground attack mode is combined with various weapon configurations to succeed in dynamic battle scenarios.

Embraer EMB-314 Super Tucano

EMB-314 Super Tucano Specs

Operational flexibility and extensive maneuverability across the spectrum of mission portfolios. The only Light Attack Aircraft designed from the start to meet the demands of air combat and hard airfield operations.

The EMB-314 Super Tucano is equipped with a fully integrated EO / IR system, exceptional visibility of seats and night operations with full capabilities with Night Vision Goggles (NVG). So it is very suitable for border patrols and armed reconnaissance. With incredible speed, altitude and range, it is highly maneuverable for aircraft tapping, exceptional visibility from both cockpits, and capable of operating day / night.

The EMB-314 Super Tucano is equipped with a complete system set for: Reconnaissance and appointment of targets. Supports the acquisition and attack of real-time targets.

EMB-314 Super Tucano specs

EMB-314 Super Tucano Engine

The EMB-314 Super Tucano is powered by a PT6A-68A turboprop engine, which develops 969kW. The power plant is equipped with automatic engine monitoring and control.

Its fuel capacity is 695l, which provides a range of more than 1,500 km and endurance of 6 hours 30 minutes. EMB-314 can fly at 24m / s. The maximum speed and cruising of each aircraft are 530km / h and 593km / h. The range and ceiling of the Super Tucano service are 4,820 km and 10,670 m respectively. The maximum durability is six hours and 30 minutes. The aircraft weighs 3,020kg and has a maximum takeoff weight of 5,200 kg.

EMB-314 Super Tucano Weapons

The aircraft is equipped with two central mission computers. Integrated weapons systems include software for aiming weapons, weapons management, mission planning and mission training. Onboard recordings are used for post mission analysis.

There are five hardpoints for carrying weapons, and this aircraft can withstand a maximum external load of 1,500kg. The aircraft is armed with two 12.7mm machine guns mounted on the wings with a firing rate of 1,100 revolutions per minute and is able to carry general-purpose bombs and air-to-air and air-to-ground missiles. The Brazilian AF aircraft is armed with near-infrared air-to-air missiles guided by the MAA-1 Piranha from Orbita.

The two-seat AT-29 is equipped with a forward-facing AN / AAQ-22 SAFIRE infrared turret at the bottom of the fuselage. The SAFIRE thermal imaging system provided by FLIR Systems is for targeting, navigation and target tracking. This system allows the aircraft to carry out night surveillance and attack missions.

In July 2012, Embraer and Boeing signed a cooperation agreement to increase the capacity to integrate new weapons at the A-29 Super Tucano to meet the requirements of the US Air Force LAS program.

EMB-314 Super Tucano cockpit

EMB-314 Super Tucano Cockpit and Avionics

EMB-314 Super Tucano focuses on ease of mission achievement. Pressurized cockpit with air conditioning, Anti-G system, OBOG, armored cockpit and engine compartment, HOTAS control (hands on throttle and stick), two mission and display processor, automatic flight (autopilot / system director) flight)), HUD - Screen Head-Up with Colored (CHVC) HUD Video Camera, backup control panel (UFCP) with CMFD, Designed for pilot safety and comfort for long-term flights.

The all-glass cockpit is fully compatible with night-vision glasses. The Brazilian AF ALX aircraft is equipped with an avionics system from Elbit Systems of Haifa, Israel, including a head-up display (HUD), a sophisticated mission computer, a navigation system, and two 6in x 8in multi-function liquid crystal displays.

A head-up screen with a 24 ° field of view and an advanced weapon delivery system integrated through the MIL-STD-1553B data bus. The pilot is equipped with direct throttle and stick (HOTAS) control.

The pilot is protected with Kevlar armor and is equipped with zero / zero ejection seats. The clamshell canopy, hinged on the front and rear and electrically activated, is equipped with a de-icing system and features a windshield that is able to withstand, at 300k, the impact of a 4lb bird. The Northrop Grumman onboard (OBOGS) oxygen generating system is installed.

The aircraft is equipped with a navigation system and advanced laser inertial attack, a global positioning system (GPS) and a traffic warning and collision avoidance system (TCAS).

EMB-314 Super Tucano Price and Orders

The price of a new EMB-314 Super Tucano is around US $ 18 million. EMB-314 Super Tucano is operated by more than 14 air forces around the world. Besides Brazil itself, the aircraft has also been used by the Colombian Air Force, Chile, the Dominican Republic and Ecuador. Embraer also plans to expand to several countries in Asia and the Middle East.

In April 2008, the Chilean Air Force selected the EMB-314 Super Tucano, with requirements for 12 aircraft. A contract for 12 aircraft was signed in August 2008. Embraer sent four of the first 12 aircraft to the Chilean Air Force on December 23, 2009. The Dominican Republic placed contracts for eight Super Tucano aircraft in late 2008.

The Ecuadorian Air Force (EAF) ordered 24 Super Tucano aircraft in March 2009 as part of a $ 270 million agreement signed with Embraer in 2008. A total of six Super Tucano were shipped in April 2010. EAF reduced orders from 24 to 18 in May 2010 to get 12 used Cheetah warplanes from Denel Dynamics.

Embraer signed a contract with the Indonesian Ministry of Defense in November 2010 to supply eight light attacks of the Super-Tucano A-29 and advance the trainer aircraft to replace the OV-10 Broncos fleet. It also supplies land support stations and integrated logistics packages. The contract was completed and entered into force on June 9, 2011. The first four aircraft were sent in August 2012.

The Indonesian Air Force placed an order for the second batch of eight A-29 Super Tucano aircraft and flight simulators in July 2012, while the Philippine Air Force (PAF) gave a contract to Embraer for six A-29 aircraft in November 2017. Deliveries to PAF began in 2019.

Embraer received a contract from the Nigerian Air Force for the delivery of 12 Super Tucano 12 A-29 attack aircraft in February 2019. Embraer will also provide ground training equipment, mission planning tools, a question and answer system mission, a land support system and additional equipment for the Nigeria Air Force .