gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_configuration
|
single-engine.
|
gptkbp:aircraft_national_origin
|
Czechoslovakia.
|
gptkbp:aircraft_operated
|
1970.
1,500 kg.
300 km/h.
8.2 m.
trainer.
|
gptkbp:aircraft_retired
|
1990s.
|
gptkbp:aircraft_role
|
training.
|
gptkbp:aircraft_type
|
Astazou IV.
jet.
|
gptkbp:armament
|
gptkb:none
none.
|
gptkbp:ceiling
|
10,000 m
|
gptkbp:climb_rate
|
10 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder.
|
gptkbp:country_of_origin
|
gptkb:Czechoslovakia
|
gptkbp:crew
|
2
|
gptkbp:design
|
gptkb:Aero_Vodochody
|
gptkbp:design_features
|
low-wing monoplane.
|
gptkbp:engine
|
turbofan.
|
gptkbp:engine_type
|
turbofan
M601
|
gptkbp:first_flight
|
gptkb:1970
1970-06-01
1990-12-31
|
gptkbp:fuel_capacity
|
400 L
400 L.
|
https://www.w3.org/2000/01/rdf-schema#label
|
Astazou V
|
gptkbp:introduced
|
gptkb:1970
|
gptkbp:landing_distance
|
600 m
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.2 m
|
gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
gptkbp:max_speed
|
300 km/h
|
gptkbp:max_takeoff_weight
|
2,000 kg
2,000 kg.
|
gptkbp:number_built
|
50
50.
|
gptkbp:number_of_engines
|
gptkb:1
1.
|
gptkbp:passenger_capacity
|
2
|
gptkbp:primary_user
|
gptkb:Czechoslovak_Air_Force
|
gptkbp:production_location
|
Czech Republic.
|
gptkbp:production_years
|
1970-1980
|
gptkbp:range
|
1,200 km
|
gptkbp:related_aircraft
|
Aero L-39 Albatros.
|
gptkbp:retired
|
1990s
|
gptkbp:role
|
gptkb:trainer_aircraft
gptkb:light_aircraft
|
gptkbp:roll_rate
|
4°/s
|
gptkbp:service_ceiling
|
10,000 m
10,000 m.
|
gptkbp:service_history
|
used for training and aerobatics.
|
gptkbp:stall_speed
|
90 km/h
|
gptkbp:successor
|
gptkb:Aero_L-39_Albatros
|
gptkbp:takeoff_distance
|
500 m
|
gptkbp:type
|
gptkb:military_aircraft
|
gptkbp:variant
|
gptkb:Astazou_IV
|
gptkbp:weight
|
1,500 kg
|
gptkbp:wing_area
|
12 m²
12 m².
|
gptkbp:wingspan
|
9.5 m
9.5 m.
|
gptkbp:bfsParent
|
gptkb:Turbomeca_Astazou
|
gptkbp:bfsLayer
|
7
|