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Il-78MK

Il-78MK

Tanker Aircrafts
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Basic Information
Name
Il-78MK
Designation
Il-78MK
Alternate Designation
Il-78, Il-78M, Il-78MK-90 (PS-90A-76 powered version), Midas
Equipment Type
Tanker Aircrafts
Manufacturer
Ilyushin Aviaton Complex
Date of Introduction
1987
Description

In 1987 the Soviet Union's Air Force introduced the first Il-78, NATO dubbed 'Midas', air-to-air refueling aircraft based on the Il-76MD military transport aircraft. The Il-78 features two internal fuel tanks that can removed reverting the tanker to the freighter role. The Il-78M is an improved version equipped with three permanent fuel tanks and aimed at refueling three aircraft using three hose drum units. Two hose drum units are located under each wing and the other one on the rear starboard fuselage. The Il-78MK was build on the Il-78M. The Il-78MK tanker can provide in-flight refueling of up to three different aircraft in adverse visibility conditions or at night. On the ground it is capable of refueling up to four aircraft. The Il-78MK can be re-configured to provide transport of cargoes, personnel and/or equipment. The Il-78MK is powered by four D-30KP turbofan engines. The IL-78MK-90 is a further version powered by more powerful PS-90A-76 turbofans, each rated at 35,000-lb, providing a maximum combined thrust of 140,000-lb at takeoff. The Il-78MK-90 adds two tons to the payload up to 50 tons and increases the cruise speed from 750 kph to 850 kph compared with the D-30KP powered Il-78MK. The landing run distance is shortened by 40 meters and can take off in 1,550 meters compared to 2,200 meters for the same aircraft powered by D-30KP engines.

Air & Air Defense Specifications
Crew 6
Max Speed 750.0 km/h
Wingspan 50.50 m
Overview (Deagel)
Group Tanker Aircrafts
Status Active
Also Known As Il-78, Il-78M, Il-78MK-90 (PS-90A-76 powered version), Midas
Origin Russia
Contractor Ilyushin Aviaton Complex
Initial Operational Capability (IOC) 1987
First Flight June 26, 1983
Total Production ?
Specifications (Deagel)
Crew 6
Number of Engines 4
Area — Wing Area 300 square meter
Dimensions — Fuselage Diameter 4.8 meter
Dimensions — Height 14.8 meter
Dimensions — Length 46.6 meter
Dimensions — Wingspan 50.5 meter
Mass — Max Takeoff Thrust 105,000 pound
Mass — Max Takeoff Weight 210 ton
Mass — Payload 48 ton
Performance — Landing Run Distance 1,000 meter
Performance — Take Off Run Distance 2,200 meter
Speed — Cruise Speed 750 kph
Speed — Flight Speed during Refueling 440 kph
Volume — Refueling Tanks Capacity 45,928 liter
Gear (Deagel)
Item 1 Turbofan Engines: D-30KP (4)
Item 2 Turbofan Engines: PS-90A-76 (4)
Variants
Variant 1 Il-76TF
Variant 2 Il-78MK
Variant 3 Il-76MF
Variant 4 Il-476
Variant 5 Il-76MD-M
Variant 6 Il-78M-90A
Details
Country of Origin Russia
Category Aerial Refueling Aircraft
Air > Aerial Refueling Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
46.6 m
Width
50.5 m
Height
14.8 m
Weight
210000 kg
Operators (7)
Russia
China
Ukraine
India
Pakistan
Soviet Union
Venezuela
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