December 24 / Antonov An-124 Ruslan first flight

Antonov An-124 Ruslan

Antonov Airlines An-124 at Belfast International Airport

The Antonov An-124 Ruslan (NATO reporting name: Condor) is a large, strategic airlift, four-engined aircraft that was designed in the 1980s by the Antonov design bureau in the Ukrainian SSR, then part of the Soviet Union (USSR). The An-124 is the world's 2nd heaviest gross weight production cargo airplane and heaviest operating cargo aircraft, behind the destroyed one-off Antonov An-225 Mriya (a greatly enlarged design based on the An-124) and the Boeing 747-8. The An-124 remains the largest military transport aircraft in service. The lead designer of the An-124 (and the An-225) was Viktor Tolmachev.

During development, it was known as Izdeliye 400 (Product #400) in-house, and An-40 in the West. First flown in 1982, civil certification was issued on 30 December 1992. In July 2013, 26 An-124s were in commercial service with 10 on order.

In August 2014, it was reported that plans to resume joint production of the Antonov An-124 had been shelved due to the ongoing political tensions between Russia and Ukraine. The sole remaining production facility is Russia's Aviastar-SP in Ulyanovsk. The various operators of the An-124 are in discussions with respect to the continuing airworthiness certification of the individual An-124 planes. The original designer of the An-124 is responsible for managing the certification process for its own products, but the Russia-Ukraine conflicts are making this process difficult to manage. In 2019, there were 26 An-124s in commercial service.

Ruslan first flew on the 24th of December 1982

Development

During the 1970s, the Military Transport Aviation Command arm of the Soviet Air Forces had a shortfall in strategic heavy airlift capacity. Its largest planes consisted of about 50 Antonov An-22 turboprops, which were used heavily for tactical roles. A declassified 1975 CIA analysis concluded that the USSR did "...not match the US in the ability to provide long-range heavy lift support.

The An-124 was manufactured in parallel by two plants: the company Aviastar-SP (ex. Ulyanovsk Aviation Industrial Complex) in Ulyanovsk, Russia and by the Kyiv Aviation Plant AVIANT, in Ukraine. Design work started in 1971 and construction of facilities began in 1973. Manufacturing of the first airframe began in 1979. Ultimately this project brought together over 100 factories contracted to produce systems and parts.

The type's maiden flight took place in December 1982; the first exposure of the An-124 to the West occurred in 1985 when it appeared at the Paris Air Show.

In the early 2000s, Volga-Dnepr upgraded its freighters with engine improvements to meet Chapter 4 noise regulations, structural improvements to increase service life, and avionics and systems changes for four person operations down from six or seven.

Russia and Ukraine agreed to resume production in the third quarter of 2008. In May 2008, a new variant—the An-124-150—was announced; it featured several improvements, including a maximum lift capacity of 150 tonnes. However, in May 2009, Antonov's partner, the Russian United Aircraft Corporation announced it did not plan production of An-124s in the period 2009–2012. In late 2009, Russian President Dmitry Medvedev ordered the production of the aircraft to resume. At the time Russia was expected to procure 20 new aircraft. In August 2014, Jane's reported that Russian Deputy Minister of Industry and Trade Yuri Slusar announced that Antonov An-124 production was stopped due to ongoing political tensions between Russia and Ukraine.

As of late 2017, An-124s were upgraded by the Aviastar-SP plant in Ulyanovsk, Russia. After Russia–Ukraine relations soured, Antonov had to source new suppliers and pushes to westernize the An-124. In 2018, GE Aviation was studying re-engining it with CF6s for CargoLogicAir, a Volga-Dnepr subsidiary. This would likely provide a range increase, and Volga-Dnepr Group operates 12 aircraft, implying 50-60 engines with a spares program.

In January 2019, Antonov revealed its plans to restart the An-124 production without support from Russia.

Aviadvigatel indicates a further development of its PD-14 for an upgraded version of the Russian-manufactured An-124, titled PD-35, with 50% more power than the present Ukrainian Progress D-18T engines.

Antonov An-124 Ruslan at the Ostrava Airport in 2018

An-124 has been introduced in 1986

Russian replacement design

At MAKS Air Show in 2017, the Central Aerohydrodynamic Institute (TsAGI) announced its An-124-102 Slon (Elephant) design to replace the similar An-124-100. The design was detailed in January 2019 before wind tunnel testing was scheduled for August–September. It is intended to be produced at the Aviastar-SP factory in Ulyanovsk. It should transport 150 t (330,000 lb) over 3,800 nmi (7,000 km) (up from 1,675 nmi, 3,102 km), or 180 t (400,000 lb) over 2,650 nmi (4,910 km) at 460 kn (850 km/h). The Russian MoD wants a range of 4,100 nmi (7,600 km) with five Sprut-SDM-1 light tanks, their 100 crew and 300 armed soldiers.

The planned An-124-102 is larger at 82.3 m (270 ft) long from 69 m (227 ft), with a 87–88 m (286–290 ft) span versus 73.3 m (240.5 ft) and 24.0 m (78.7 ft) high compared with 21.0 m (68.9 ft). A new higher aspect ratio, composite wing and a 214–222 t (472,000–489,000 lb) airframe would allow a 490–500 t (1,080,000–1,100,000 lb) gross weight. It should be powered by Russian PD-35s developed for the CR929 widebody, producing 35 tf (77,000 lbf) up from 23 tf (51,000 lbf). Two fuselages are planned, one for Volga-Dnepr with a width of 5.3 m (17.4 ft) from the An-124's 4.4 m (14.4 ft), and one for the Russian MoD of 6.4 m (21 ft) wide to carry vehicles in two lines.

On 5 November 2019, the TsAGI released pictures of a 1.63 m (5 ft 4 in) long and 1.75 m (5 ft 9 in) wide model, ahead of wind tunnel testing. On 26 March 2020, TsAGI released new pictures of a wind tunnel model, announcing that the researchers of the Institute had completed the first cycle of aerodynamic testing; the results confirmed the characteristics laid down during preliminary studies.

An-124 Cruise speed is 865 km/h (537 mph, 467 kn) max

Design

The Antonov An-124 Ruslan is a large, strategic airlift, four-engined aircraft. Externally, it bears numerous similarities to the American Lockheed C-5 Galaxy, having a double fuselage to allow for a rear cargo door (on the lower fuselage) that can open in flight without affecting structural integrity. The An-124 is a slightly shorter fuselage, has a slightly greater wingspan, and is capable of carrying a 17 percent larger payload. Instead of the Galaxy's T-tail, the An-124 is furnished with a conventional empennage, similar in design to that of the Boeing 747. The An-124 is powered by four Lotarev D-18 turbofan engines, each capable of generating up to 238–250 kN of thrust. Pilots have stated that the An-124 is light on the controls and easy to handle for an aircraft of its size.

The landing gear of the An-124 is outfitted with an oleo strut suspension system for its 24 wheels. This suspension has been calibrated to allow for landing on rough terrain and is able to kneel, which allows for easier loading and unloading via the front cargo door. The aircraft is equipped with an onboard overhead crane, capable of lifting up to 30 tonnes of cargo, while items up to 120 tonnes can be winched on board. Up to 150 tonnes (150 long tons; 170 short tons) of cargo can be carried within a single An-124 configured for military purposes; it can also carry 88 passengers in an upper deck behind the wing centre section. The cargo compartment of the An-124 is 36×6.4×4.4 m (118×21×14 ft), ca. 20% larger than the main cargo compartment of the C-5 Galaxy, which is 36.91×5.79×4.09 m (121.1×19.0×13.4 ft). Due to limited pressurisation in the main cargo compartment (24.6 kPa, 3.57 psi), it has seldom been used to carry paratroopers. Due to the heat and blast effects of the aircraft's two TA18-200-124 auxiliary power units, some airports require pavement protection to be deployed

An-124 has a Max takeoff weight of 402,000 kg (886,258 lb)

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