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II-38 (May) Russian Anti-Submarine Warfare (ASW) Aircraft

II-38

Anti-Submarine Warfare (ASW) Aircraft
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Basic Information
Name
II-38 (May) Russian Anti-Submarine Warfare (ASW) Aircraft
Designation
II-38
Alternate Designation
Equipment Type
Anti-Submarine Warfare (ASW) Aircraft
Manufacturer
Ilyushin OKB, Moscow, Russia
Date of Introduction
1967
Description

II-38 (May) Russian Anti-Submarine Warfare (ASW) Aircraft is a maritime patrol aircraft and anti-submarine warfare aircraft designed in the Soviet Union. It was a development of the Ilyushin Il-18 turboprop transport. The Il-38 is an adaptation of the four-engined turboprop Ilyushin Il-18 for use as a maritime patrol aircraft for the Soviet Navy. It met a requirement to counter American ballistic missile submarines. The Communist Party Central Committee and the Council of Ministers issued a joint directive on 18 June 1960, calling for a prototype to be ready for trials by the second quarter of 1962. The fuselage, wing, tail unit, and engine nacelles were the same as the Il-18 and it had the same powerplant and flight deck. An aerodynamic prototype of the Il-38 first flew on 28 September 1961, with the first production aircraft following in September 1967. Production continued until 1972 when the longer-range and more versatile Tupolev Tu-142 derivative of the Tupolev Tu-95 strategic bomber entered service. The airframe is based on the Il-18, with the wings moved forward 3 m (9.84 ft). Unlike the Il-18, only the forward fuselage of the Il-38 is pressurized. The tail contains a MAD, while under the forward fuselage, a Berkut ("Golden Eagle") search radar (named "Wet Eye" by NATO) is housed in a bulged radome. There are two internal weapons bays, one forward of the wing, housing sonobuoys, and one behind the wing housing weapons. Some Western sources state that 58 were produced; the commander of the ASW squadron at Ostrov has stated that Soviet Naval Aviation received 35, of which about thirty remain in service with Russian Naval Aviation. Five were passed to India in 1977/8. In the mid-1990s it seems the Tu-204/Tu-214 airliner won a competition against the Beriev A-40/Be-42 amphibious plane to replace the Il-38 in Russian service, but a lack of funds crippled the project. More recently an A-40 variant seems to be under development to replace the Il-38. India received three ex-Soviet Naval Aviation Il-38s in 1977, with two more arriving in 1983. Indian modifications included fitting pylons to the fuselage side to carry the Sea Eagle anti-ship missile. The Il-38s of the Indian Navy have been sent back to Russia for upgrades. They will incorporate the new Sea Dragon avionic suite, incorporating a new radar, a Forward-looking infrared turret under the nose, and an electronic intelligence system housed in a box-like structure mounted on struts above the forward fuselage. Three upgraded aircraft, designated Il-38 SD, have been delivered to the Indian Navy.

Air & Air Defense Specifications
Crew 12
Engine Turboprop (4250 hp)
Max Speed 720.0 km/h
Range 7200.0 km
Endurance 13.00 hrs
Variants
Il-38 Production aircraft
Il-38M Modified with a receiver probe as part of a probe and drogue air refueling system. System not adopted.
Il-38MZ Tanker variant of the Il-38. Prototype only
Il-38N This is an upgraded variant that is fitted with the Novella sensor system; see main entry. Improved variant sometimes referred to as Il-38SD for Sea Dragon, which is a new search and tracking system. The Russian Navy version is equipped with the Novella P-38 system.
System
Alternate Designation(s) II-38; NATO: May
Type Anti-Submarine Warfare (ASW) Aircraft
Manufacturer Ilyushin OKB, Moscow, Russia
Crew 12 (pilot, co-pilot, flight engineer, radar operator, navigator, 3 systems operators,tactical coordinator, 3 observers)
Number of Engines 4 ea
Number of Hard Points Internal bomb bay
Cargo Capacity 9,000 kg
Dimensions
Length 39.60 m
Height 10.16 m
Width (Wing Span) 37.40 m
Wing Area 140 sq m
Empty Weight 36,000 kg
Maximum Takeoff Weight 63,500 kg
Automotive
Engine Name 4 x Ivchenko AI-20M
Engine Type Turboprop
Engine Power 4,250 shaft hp each
Internal Fuel Capacity 30,000 liters
Maximum Speed 720 km/h
Patrol Speed 400 km/h
Minimum Flying Speed 190 km/h
Range 7,200 km
Takeoff Run 1,300 m
Landing Run 850 m
Endurance 13 hours
Missile System
System
Name R-73 (AA-11 Archer)
Type Air-to-Air Missile
Length 2.93 m
Diameter 165 mm
Wingspan 510 mm
Weight 105 kg
Engine Solid-fuel rocket engine
Guidance System All-aspect infrared homing
Range 30 km
Maximum Speed Mach 2.5
Anti-Submarine Warfare (ASW) Aircraft
ASW Suite Magnetic Anomaly Detector (MAD) System
Sonobuoys The Il-38 can carry and drop a variety of sonobuoys. These include up to 144 small RGB-1 radio beacons, 10 RGB-2 passive sonobuoys and 3 RBG-3 or RGB-16 sonobuoys with active/passive sonar.
Torpedoes 450mm AT-1; 533mm AT-2; 400mm AT-3 Orlan (air launched UMGT-1); APR-1 Kondor rocket torpedo; APR-2 Yastreb rocket torpedo
Mines AMD-2
Depth Charges PLAB-50; PLAB-250-120; PL-250-120
Radar Systems
Surface / Search Radar 1 x Wet Eye surface search
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin Russia
Category Maritime Patrol
Air > Maritime Patrol
Filter Label
I
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
39.6 m
Width
37.4 m
Height
10.16 m
Weight
63500 kg
Operators (3)
Russia
Ukraine
India
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