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gptkbp:instance_of
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gptkb:helicopter
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gptkbp:armament
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gptkb:none
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|
gptkbp:cargo_capacity
|
1,000 kg
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|
gptkbp:ceiling
|
3,000 m
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|
gptkbp:certification
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gptkb:EASA
|
|
gptkbp:climb_rate
|
8.5 m/s
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|
gptkbp:combat_role
|
light utility
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gptkbp:crew
|
gptkb:1
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|
gptkbp:design
|
MBB engineers
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|
gptkbp:design_features
|
modular design
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gptkbp:diameter
|
twin-rotor
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gptkbp:engine_type
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gptkb:turbofan_engine
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|
gptkbp:first_flight
|
gptkb:1967
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|
gptkbp:fuel_capacity
|
500 L
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gptkbp:height
|
3.30 m
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gptkbp:historical_significance
|
first helicopter with a fully articulated rotor system.
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|
https://www.w3.org/2000/01/rdf-schema#label
|
MBB Bo 105 DB-21
|
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gptkbp:length
|
11.68 m
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|
gptkbp:manufacturer
|
gptkb:MBB
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|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
2,500 kg
|
|
gptkbp:military_technology
|
gptkb:emergency_services
|
|
gptkbp:modifications
|
various military configurations
|
|
gptkbp:notable_features
|
fenestron tail rotor
|
|
gptkbp:notable_operators
|
gptkb:Germany
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:operational_status
|
retired from service in many countries
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:power_source
|
2 x Allison 250-C20
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|
gptkbp:produces
|
1,500 units
|
|
gptkbp:production_years
|
1967-2001
|
|
gptkbp:range
|
600 km
|
|
gptkbp:related_aircraft
|
gptkb:Eurocopter_EC120
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_record
|
generally good
|
|
gptkbp:service_entry
|
gptkb:1970
|
|
gptkbp:service_history
|
used in various conflicts
|
|
gptkbp:successor
|
Eurocopter EC135
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gptkbp:used_by
|
gptkb:Germany
|
|
gptkbp:variant
|
gptkb:MBB_Bo_105
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wingspan
|
10.70 m
|
|
gptkbp:bfsParent
|
gptkb:MBB_Bo_105_DB
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gptkbp:bfsLayer
|
9
|