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Tu-95LAL
Tu-95LAL
	The Tu-95LAL test aircraft. The bulge in the fuselage aft of the wing covers the reactor.
General information
Type	Experimental nuclear aircraft
Manufacturer	Tupolev
Number built	1
History
First flight	1961
Developed from	Tupolev Tu-95

The Tupolev Tu-95LAL experimental aircraft (Russian: Летающая Атомная Лаборатория, romanized: Letayushchaya Atomnaya Laboratoriya, lit. 'flying atomic laboratory') which flew from 1961 to 1965 was a modified Tupolev Tu-95 Soviet bomber aircraft, analogous to the United States' earlier Convair NB-36H.^[1] It was intended to see whether a nuclear reactor could be used to power an aircraft, primarily testing airborne operation of a reactor and shielding for components and crew. The reactor did not actually power the aircraft.^[1]

Design and development

During the Cold War the USSR had an experimental nuclear aircraft program. Without the need to refuel, a nuclear-powered aircraft would have greatly extended range compared to conventional designs.^[2]

On 12 August 1955 the Council of Ministers of the USSR issued a directive ordering bomber-related design bureaus to join forces in researching nuclear aircraft. The design bureaus of Andrei Tupolev and Vladimir Myasishchev became the chief design teams, while N. D. Kuznetsov and A. M. Lyulka were assigned to develop the engines. They chose to focus on the direct-cycle system from the start, testing ramjets, jet engines and even turboprops.^[2]

The Tupolev bureau, knowing the complexity of the task assigned to them, estimated that it would be two decades before the program could produce a working prototype. They assumed that the first operational nuclear-assisted airplane could take to the air in the late 1970s or early 1980s. In order to gain experience with operational problems, they proposed building a flying testbed as soon as possible, mounting a small reactor in a Tupolev Tu-95M to create the Tu-95LAL.^[2]^[3]

The VVRL-lOO reactor was fitted in the bomb bay of the aircraft, requiring aerodynamic fairings over the top and bottom. From 1961 to 1969, the Tu-95LAL completed over 40 research flights.^[1]^[4] Most of these were made with the reactor shut down.^[1] The main purpose of the flight phase was examining the effectiveness of the radiation shielding, which was one of the main concerns for the engineers.^[1] Liquid sodium, beryllium oxide, cadmium, paraffin wax and steel plates were used for protection. The shielding efficiency is disputed: most sources say that it was at least efficient enough to warrant further work,^[2]^[3]^[5] and indeed, the design of the follow-up prototype, the Tu-119, was started.^[5]

As in the US, development was curtailed on grounds of cost and environmental concerns.^[1] The emerging potential of intercontinental ballistic missiles made the expensive nuclear aircraft program superfluous, and it was scaled back.^[1]^[2]

Tu-119

The next stage in the development of a nuclear-powered bomber would have been the Tupolev Tu-119, a modified Tu-95, which would have been powered by both nuclear-fuelled and kerosene-fuelled turboprop engines: two Kuznetsov NK-14A nuclear-fuelled engines inboard, fed with heat from a fuselage-mounted reactor and two kerosene-fed Kuznetsov NK-12 turboprops outboard. The Tu-119 was never completed due to the nuclear-powered bomber project being cancelled on grounds of cost and the dire environmental impact of possible mishaps and accidents.^[2]

Specifications (Tu-95LAL)

Note: the specifications given are those of the Tu-95MS, which were identical to the Tu-95LAL.

Data from Combat Aircraft Since 1945^[6]

General characteristics

Length: 46.2 m (151 ft 7 in) ^[7]
Wingspan: 50.1 m (164 ft 4 in) ^[7]
Height: 12.12 m (39 ft 9 in)
Wing area: 310 m² (3,300 sq ft)
Gross weight: 145,000 kg (319,670 lb)
Landing weight: 110,000 kg (242,508 lb)
Powerplant: 4 × Kuznetsov NK-12M turboprop engines 15,000 PS (15,000 hp; 11,000 kW)
Propellers: 8-bladed contra-rotating constant-speed fully feathering propellers

Performance

Cruise speed: 750–800 km/h (470–500 mph, 400–430 kn)
Range: 4,700 km (2,900 mi, 2,500 nmi)
Endurance: >6.4 hours

References

Citations

^ ^a ^b ^c ^d ^e ^f ^g Trakimavičius, Lukas. "The Future Role of Nuclear Propulsion in the Military" (PDF). NATO Energy Security Centre of Excellence. Archived from the original (PDF) on 2021-10-18. Retrieved 2021-10-15.
^ ^a ^b ^c ^d ^e ^f Buttler & Gordon 2004, pp. 79–80
^ ^a ^b Colon 2009
^ From the television/DVD documentary, Planes That Never Flew: The Atomic Plane, Discovery Channel Europe and Alba Communications Ltd. 2003]
^ ^a ^b Ту-95ЛАЛ (заказ 247) tr. "Tu-95LAL (order 247)"; TestPilot.Ru
^ Stewart Wilson (2000). Combat Aircraft Since 1945. p. 137. ISBN 9781840371505.
^ ^a ^b Grant and Dailey 2007, p. 293.

Bibliography

Gordon, Yefim; Komissarov, Dmitriy and Sergey (2004). OKB Ilyushin: A History of the Design Bureau and its Aircraft. London: Ian Allan. ISBN 1-85780-187-3.
Colon, Raul (2009). Soviet Experimentation with Nuclear Powered Bombers. Hinckley: Midland Publishing. ISBN 978-1-85780-194-1. Archived from the original on 6 January 2012. Retrieved 3 January 2012.
Buttler, Tony; Gordon, Yefim (2004). "Chapter 6: Nuclear Power and Flying Wings". Soviet secret projects : Bombers since 1945. Hinckley: Midland Publishing. ISBN 1-85780-194-6. Archived from the original on 17 February 2012. Retrieved 8 January 2012.