|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Antonov_An-32
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:compression_ratio
|
12:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
gptkb:currency
air-cooled
|
|
gptkbp:design
|
robust and efficient
|
|
gptkbp:developer
|
1950s
|
|
gptkbp:diameter
|
1,100 mm
|
|
gptkbp:emissions_standard
|
environmentally friendly design
compliant with standards
|
|
gptkbp:engine
|
advanced aerodynamics
high efficiency
wing-mounted
proven track record
various upgrades available
5,000 hours
air-start
widely used in aviation history
|
|
gptkbp:engine_type
|
turboprop
high bypass turboprop engine
compatible with various aircraft types
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
1,200 kg
1,800 mm
1,100 mm
optimized for performance
0.5 kg/k W·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ivchenko AI-20 M
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
easy access
1,000 hours
|
|
gptkbp:manufacturer
|
Ivchenko
|
|
gptkbp:noise_level
|
low
designed for low noise
|
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:power_output
|
2,900 k W
|
|
gptkbp:powers
|
2.4 k W/kg
|
|
gptkbp:produced_by
|
over 10,000
|
|
gptkbp:production_years
|
1955-1980
|
|
gptkbp:propulsion
|
3.33
variable-pitch
4,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
8,000 m
|
|
gptkbp:setting
|
two-shaft
|
|
gptkbp:successor
|
AI-22
|
|
gptkbp:used_in
|
gptkb:Antonov_An-12
|
|
gptkbp:variant
|
AI-20 D
|
|
gptkbp:weight
|
1,200 kg
3,000 kg
|