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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
|
gptkb:Vladimir_Petlyakov
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Pe-2
low-wing
conventional configuration
influenced future designs
good maneuverability
initial and advanced training
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|
gptkbp:armament
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gptkb:none
|
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gptkbp:climb_rate
|
6 m/s
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|
gptkbp:cockpit
|
two-seat cockpit
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|
gptkbp:crew
|
2
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|
gptkbp:decommissioned
|
1950s
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gptkbp:design
|
gptkb:Vladimir_Petlyakov
multirole aircraft
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|
gptkbp:engine_type
|
twin-engine
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|
gptkbp:features
|
high performance
|
|
gptkbp:first_flight
|
gptkb:1940
|
|
gptkbp:fuel_capacity
|
800 L
|
|
gptkbp:height
|
3.8 m
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|
gptkbp:historical_significance
|
used during WWII
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Pe-2 T trainer aircraft
|
|
gptkbp:influenced_by
|
Pe-2 bomber design
|
|
gptkbp:is_used_by
|
gptkb:Soviet_Air_Force
|
|
gptkbp:landing_gear
|
retractable landing gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Petlyakov
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
4000 kg
|
|
gptkbp:notable_features
|
twin-engine design
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:operational_area
|
training and conversion
|
|
gptkbp:operational_history
|
served in various air forces
|
|
gptkbp:power_output
|
gptkb:M-105_engine
|
|
gptkbp:production_years
|
1940-1945
|
|
gptkbp:propulsion
|
two propellers
|
|
gptkbp:range
|
1000 km
|
|
gptkbp:role
|
gptkb:battle
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
8000 m
|
|
gptkbp:service_history
|
used in training pilots
|
|
gptkbp:speed
|
120 km/h
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:training
|
pilot training
advanced training
|
|
gptkbp:variant
|
gptkb:Pe-2
|
|
gptkbp:weight
|
2500 kg
|
|
gptkbp:wingspan
|
14.5 m
|