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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Letov_Š-328
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|
gptkbp:aircraft_operated
|
wood and fabric
military trainer
Letov Š-28
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
5.0
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:date
|
1930s
|
|
gptkbp:design
|
Miloš Štros
|
|
gptkbp:engine
|
Avia R-14
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
high-wing configuration
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historical_significance
|
used in WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Letov Š-20
|
|
gptkbp:influences
|
Czech aviation design
|
|
gptkbp:is_used_by
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
Letov
|
|
gptkbp:material
|
gptkb:NACA_2412
wood and fabric
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
80 km/h
1,200 kg
|
|
gptkbp:nickname
|
Š-20
|
|
gptkbp:number_built
|
50
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:powers
|
400 hp
|
|
gptkbp:predecessor
|
gptkb:Letov_Š-16
|
|
gptkbp:primary_user
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:production_location
|
gptkb:Monarch
|
|
gptkbp:production_years
|
1939-1945
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirement_year
|
1950s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
3.5 s per 360°
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:services
|
gptkb:1940
|
|
gptkbp:setting
|
two-seat
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
Letov Š-28
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
Letov Š-20 A
Letov Š-20 B
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
10.5 m
|