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II-28 (Beagle) Russian Twin-Engine Light Bomber

II-28

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Basic Information
Name
II-28 (Beagle) Russian Twin-Engine Light Bomber
Designation
II-28
Alternate Designation
Equipment Type
Manufacturer
Ilyushin
Date of Introduction
1950
Description

The Ilyushin Il-28 (Russian: Илью́шин Ил-28; NATO reporting name: Beagle) is a jet bomber of the immediate postwar period that was originally manufactured for the Soviet Air Forces. It was the Soviet Union's first such aircraft to enter large-scale production. It was also licence-built in China as the Harbin H-5. Total production in the USSR was 6,316 aircraft, and over 319 H-5s were built. Only 187 examples of the HJ-5 training variant were manufactured. In the 1990s hundreds remained in service with various air forces over 50 years after the Il-28 first appeared. The only H-5s in service currently are approximately 80 aircraft which operate with the Korean People's Air Force. The Il-28 has the USAF/DoD reporting name "Type 27" and NATO reporting name "Beagle", while the Il-28U trainer variant has the USAF/DoD reporting name "Type 30" and NATO reporting name Mascot. After a number of attempts at a four-engined bomber (the Lyulka TR-1 powered Ilyushin Il-22 and the unbuilt Rolls-Royce Derwent powered Ilyushin Il-24), the Ilyushin Design Bureau began development of a new jet-powered tactical bomber in late 1947. Western Intelligence focused on the four-engine developments while the twin-engine Ilyushin Il-28 was created to meet a requirement for a bomber to carry a 3,000 kilograms (6,600 lb) bombload at 800 kilometres per hour (500 mph). The new design took advantage of the sale of a number of Rolls-Royce Nene jet engines by Great Britain to the Soviet Union, which allowed Soviet engineers to quickly produce an unlicensed copy of the Nene, the RD-45, with Ilyushin designing the new bomber around two RD-45s. The Il-28 was smaller than the previous designs and carried a crew of only three (pilot, navigator and gunner). It was also smaller than the competing design from the Tupolev design bureau, the three-engined (i.e. two Nenes and a Rolls-Royce Derwent) Tupolev Tu-73, which had been started long before the Ilyushin project, and flew before the design of the Il-28 was approved. The Il-28 design was conventional in layout, with high, unswept wings and a swept horizontal tail and fin. The engines were carried in bulky nacelles slung directly under the wings. The nosewheel retracted rearwards, while the main wheels retracted forwards into the engine nacelles. The crew of three were accommodated in separate, pressurised compartments. The navigator, who also acted as bombardier, was accommodated in the glazed nose compartment and was provided with an OPB-5 bombsight based on the American Norden bombsight of the Second World War, while the pilot sat under a sideways opening bubble canopy with an armoured windscreen. The gunner sat in a separate compartment at the rear of the fuselage, operating a power driven turret armed with two Nudelman-Suranov NS-23 23 mm cannons with 250 rounds each. In service, the turret was sometimes removed as a weight saving measure. While the pilot and navigator sat on ejector seats, the gunner had to parachute out of a hatch in the floor in the event of an emergency. Two more fixed, forward-firing 23 mm cannon with 100 rounds each were mounted under the nose and fired by the pilot, while a bomb bay was located in the fuselage, capable of holding four 100 kg (220 lb) bombs in individual containers, or single large bombs of up to 3,000 kg (6,600 lb) slung from a beam in the bomb bay. One unusual design feature of the Il-28 was that the wings and tail were split horizontally through the centre of the wing, while the fuselage was split vertically at the centreline, allowing the separate parts to be built individually and fitted out with systems before being bolted together to complete assembly of the aircraft. This slightly increased the weight of the aircraft structure, but eased manufacture and proved to be more economical. The first prototype, powered by two imported Nenes, made its maiden flight on 8 July 1948, with Vladimir Kokkinaki at the controls. Testing was successful, with the Il-28 demonstrating good handling and reaching a speed of 833 km/h (518 mph). It was followed on 30 December 1948 by the second prototype, with Soviet built RD-45 engines replacing the Nenes. After the completion of state tests in early 1949 the aircraft was ordered into large scale production on 14 May 1949, with the Klimov VK-1, an improved version of the RD-45 to be used in order to improve the aircraft's performance. The first pre-production aircraft with VK-1 engines flew on 8 August 1949, and featured reshaped engine nacelles to reduce drag, while the radome for the navigation radar was moved from the rear fuselage to just aft of the nosewheel. Full production in three factories started in September 1949, with service deliveries starting in early 1950, allowing 25 Il-28s to be displayed at the Moscow May Day parade of 1950 (as ordered by Joseph Stalin when it was ordered into production in 1949). The Il-28 soon became the standard tactical bomber in the Soviet forces and was widely exported.

Air & Air Defense Specifications
Crew 3
Engine Turbojet (5952 hp)
Max Speed 900.0 km/h
Range 3550.0 km
Variants
Il-28 Basic three-seat bomber version, powered by two VK-1 engines.
Il-28U Unarmed training version fitted with new nose housing cockpit for instructor, while the trainee sat in the normal cockpit. First flown 18 March 1950.
Il-28R Three-seat tactical photo reconnaissance version, with extra fuel in bomb bay and tip-tanks, and with one forward firing cannon removed. Fitted with revised undercarriage to deal with heavier weights. First flew 19 April 1950.
Il-28RTR ELINT version of Il-28R
Il-28REB Electronic warfare, electronic jamming version, fitted with wingtip electronic pods, that were in the former wing tanks.
Il-28T Torpedo bomber version for the Soviet Naval Aviation able to accommodate two small or one large torpedo (including RAT-52 rocket propelled torpedoes) in a lengthened weapons bay.
Il-28N Nuclear bomber for the Soviet Air Force with modified bomb-bay and revised avionics. (N - Nositel - carrier, also known as Il-28A - Atomnyy - atomic).
Il-28P Unarmed civil conversion for Aeroflot, used as jet conversion trainer and to carry high priority cargo (i.e. newspaper matrices to allow simultaneous printing of Pravda and Izvestia in Moscow, Sverdlovsk and Novosibirsk). Also designated Ilyushin Il-20.
Il-28S Proposed swept-wing version with more powerful Klimov VK-5 engines. Unbuilt.
Il-28RM Modified Il-28R with VK-5 engine. One prototype built plus two similarly converted bombers (which carried no special designation) but no production.
Il-28TM Il-28T with VK-5. One converted, no production.
Il-28PL High-speed anti-submarine conversion of Il-28 bomber or Il-28T torpedo bomber. Capable of carrying dropping sonobuoys or acoustic homing torpedoes on direction of other anti-submarine assets.
Il-28Sh Ground attack (Shturmovik) conversion of Il-28 with 12 underwing pylons for rocket pods. Small number converted which saw limited service.
Il-28ZA Atmospheric sampling version.
Il-28M Target drone conversion of Il-28. Also known as M-28.
System
Alternate Designation(s) II-28; NATO: Beagle
Primary Function / Type Light Bomber Aircraft
Manufacturer Ilyushin
Crew 3 (pilot, navigator/bombardier, radio operator/gunner)
Number of Engines 2
Number of Hard Points 4
Dimensions
Length 17.65 m
Height 6.68 m
Width (Wing Span) 21.45 m
Wing Area 60.87 m sq
Weight, Empty 12,890 kg
Weight, Maximum Takeoff 21,200 kg
Weight, Maximum Weapons Load 3,000 kg
Weight, Normal Weapons Load 1,000 kg
Automotive
Engine Name 2 x Klimov VK-1A (Rolls Royce Nene) turbojet
Number of Engines 2
Engine Type Turbojet
Engine Power 5,952 lb (2,700 kg) static thrust each
Fuel Capacity 7,908 liters
Maximum Speed 900 km/h
Cruising Speed 769 km/h
Ceiling 12,500 m
Rate of Climb 900 m/min
Maximum Range 3,550 km
Radius 1,100 km
Main Gun System
System
Name Nudelman-Rikhter NR-23
Type Autocannon
Caliber 23mm
Quantity 4 x 23-mm NR-23 cannon (2 fixed in nose and two in tail position)
Length 1,980 mm
Barrel Length 1,450 mm
Width 165 mm
Height 136 mm
Weight 39 kg
Barrels 1
Action Short recoil
Rate of Fire 800–850 rpm
Muzzle Velocity 690 m/s
Ammunition
Type Rifle
Caliber 23mm
Cartridge INA
Basic Load INA
Bombing System
Weapons Bay Maximum Capacity 3,000 kg) of bombs or torpedoes in internal weapons bay
Fire Control / Avionics
Fire Control System Type INA
Fire Control Radar INA
Laser Desingator INA
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
I
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
17.65 m
Width
21.45 m
Height
6.68 m
Weight
21200 kg
Operators (1)
North Korea
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