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gptkbp:instance_of
|
gptkb:light_aircraft
|
|
gptkbp:air_traffic_control
|
advanced avionics
digital fly-by-wire
|
|
gptkbp:aircraft_configuration
|
twin-engine configuration
tiltrotor
|
|
gptkbp:aircraft_operated
|
gptkb:vertical_lift_aircraft
multirole aircraft
medium-lift
|
|
gptkbp:aircraft_type
|
gptkb:vertical_lift_aircraft
multirole aircraft
|
|
gptkbp:armament
|
optional machine guns
none (configurable)
|
|
gptkbp:avionics
|
advanced avionics
|
|
gptkbp:awards
|
Joint Multi-Role Technology Demonstrator
|
|
gptkbp:cargo_capacity
|
up to 10,000 pounds
|
|
gptkbp:cargo_types
|
rear ramp
|
|
gptkbp:combat_radius
|
500 nautical miles
800 nautical miles
|
|
gptkbp:competitors
|
gptkb:V-22_Osprey
|
|
gptkbp:contract_award
|
gptkb:2014
|
|
gptkbp:crew
|
gptkb:4
2
|
|
gptkbp:cruise_speed
|
280 knots
|
|
gptkbp:design
|
multiple prototypes
Bell and Boeing
Bell and Lockheed Martin
|
|
gptkbp:design_feature
|
fly-by-wire controls
|
|
gptkbp:design_philosophy
|
modular design
|
|
gptkbp:design_purpose
|
enhanced survivability
speed and range
replace UH-60 Black Hawk
|
|
gptkbp:development
|
2016 to 2025
|
|
gptkbp:development_cost
|
$1 billion
estimated $1 billion
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:environmental_concerns
|
yes
|
|
gptkbp:environmental_impact
|
reduced emissions
|
|
gptkbp:first_flight
|
ongoing
December 2017
December 18, 2017
|
|
gptkbp:flight_style
|
expanded
expanded compared to predecessors
|
|
gptkbp:fuel_capacity
|
1,200 gallons
|
|
gptkbp:fuel_economy
|
improved over predecessors
|
|
gptkbp:fuselage_material
|
composite materials
|
|
gptkbp:has_programs
|
gptkb:Future_Vertical_Lift
Joint Multi-Role Technology Demonstrator
|
|
gptkbp:height
|
20 feet
11.5 feet
|
|
gptkbp:hover_capability
|
gptkb:true
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
V-280 Valor
|
|
gptkbp:is_tested_for
|
ongoing
scheduled for 2025
|
|
gptkbp:key_feature
|
speed and range
|
|
gptkbp:landing_distance
|
1,500 feet
|
|
gptkbp:length
|
58 feet
30.2 feet
|
|
gptkbp:logistics
|
advanced logistics
integrated support solutions
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
|
gptkbp:max_speed
|
300 knots
|
|
gptkbp:max_takeoff_weight
|
30,000 pounds
|
|
gptkbp:military_branch
|
gptkb:U._S._Army_Aviation
|
|
gptkbp:notable_pilots
|
gptkb:Bell_test_pilots
|
|
gptkbp:operational_range
|
1,000 nautical miles
|
|
gptkbp:operational_use
|
high
multi-mission
under evaluation
|
|
gptkbp:participating_nations
|
high
|
|
gptkbp:passenger_capacity
|
gptkb:14
|
|
gptkbp:primary_user
|
gptkb:United_States_Army
|
|
gptkbp:propulsion
|
two engines
|
|
gptkbp:range
|
2,100 nautical miles
|
|
gptkbp:related_aircraft
|
V-22 Osprey family
|
|
gptkbp:release_date
|
gptkb:2016
|
|
gptkbp:role
|
gptkb:military_logistics
potentially in special operations
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
10,000 feet
|
|
gptkbp:service_entry
|
2020s
|
|
gptkbp:speed
|
280 knots
|
|
gptkbp:stealth_features
|
limited
limited radar cross-section
|
|
gptkbp:takeoff_distance
|
1,500 feet
|
|
gptkbp:target_market
|
gptkb:United_States_Army
|
|
gptkbp:tiltrotor_mechanism
|
gptkb:true
|
|
gptkbp:training_programs
|
integrated training
developed alongside aircraft
|
|
gptkbp:upgrades
|
possible
planned
|
|
gptkbp:variant
|
possible
|
|
gptkbp:vertical_takeoff
|
gptkb:true
|
|
gptkbp:weight
|
30,000 pounds
|
|
gptkbp:wingspan
|
38 feet
38.5 feet
|
|
gptkbp:bfsParent
|
gptkb:Advanced_Tiltrotor_Program
gptkb:Bell_Textron
gptkb:Joint_Service_Vertical_Takeoff/_Landing_Experimental_Program
|
|
gptkbp:bfsLayer
|
5
|