|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Ilyushin_Il-78
|
|
gptkbp:aircraft_operated
|
gptkb:Il-76_family
gptkb:Ilyushin_Il-76
gptkb:starship
high-wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized systems
|
|
gptkbp:crew
|
gptkb:3
gptkb:Russian_Air_Force_Academy
|
|
gptkbp:date
|
gptkb:1980s
|
|
gptkbp:deployment
|
strategic airlift missions
|
|
gptkbp:design
|
gptkb:Ilyushin_Design_Bureau
gptkb:battle
multirole aircraft
|
|
gptkbp:engine
|
25,000 lbf per engine
|
|
gptkbp:engine_type
|
D-30 KP
|
|
gptkbp:exported_to
|
several countries
|
|
gptkbp:first_flight
|
gptkb:1987
|
|
gptkbp:fuel_capacity
|
90,000 liters
|
|
gptkbp:fuel_type
|
probe and drogue
|
|
gptkbp:has_programs
|
Aerial refueling programs
|
|
gptkbp:height
|
15.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ilyushin Il-78 M2
|
|
gptkbp:introduced
|
gptkb:1990
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
46.5 m
|
|
gptkbp:manufacturer
|
gptkb:Ilyushin
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
850 km/h
|
|
gptkbp:max_takeoff_weight
|
200,000 kg
|
|
gptkbp:military_branch
|
gptkb:Il-78_M2
|
|
gptkbp:military_technology
|
gptkb:none
|
|
gptkbp:modifications
|
Il-78 M, Il-78 M2
|
|
gptkbp:notable_features
|
in-flight refueling capability
|
|
gptkbp:number_built
|
over 30
|
|
gptkbp:operational_area
|
1990s
|
|
gptkbp:operational_history
|
used in various conflicts
|
|
gptkbp:operational_range
|
1,500 km with 100,000 kg payload
|
|
gptkbp:primary_user
|
gptkb:Russian_Air_Force
|
|
gptkbp:production_years
|
1987-present
|
|
gptkbp:range
|
5,000 km
|
|
gptkbp:role
|
aerial refueling
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Ilyushin_Il-78
|
|
gptkbp:wingspan
|
50.5 m
|