Statements (112)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:light_aircraft
|
| gptkbp:air_traffic_control |
advanced avionics
Automatic flight control system Troop transport and logistics |
| gptkbp:aircraft_configuration |
Aerodynamic efficiency
Tiltrotor with wings tiltrotor Advanced rotor system Tiltrotor with advanced systems |
| gptkbp:aircraft_mission_profile |
Combat and support missions
|
| gptkbp:aircraft_operated |
Stealth technology
Advanced avionics Utility aircraft medium-lift Integrated mission systems 88 feet 6 inches Enhanced maneuverability enhanced compared to predecessors military rotorcraft 14,000 lb empty Joint venture with Lockheed Martin Multi-role versatility Next-generation rotorcraft technology |
| gptkbp:aircraft_performance_metrics |
Speed and payload capacity
|
| gptkbp:aircraft_type |
multirole aircraft
Military rotorcraft |
| gptkbp:armament |
None (configurable)
|
| gptkbp:cargo_capacity |
10,000 lb
|
| gptkbp:combat_radius |
500 nautical miles
|
| gptkbp:configuration |
gptkb:convertible
|
| gptkbp:control_system |
Digital fly-by-wire
|
| gptkbp:country_of_origin |
gptkb:United_States
|
| gptkbp:crew |
gptkb:4
|
| gptkbp:cruise_speed |
250 knots
|
| gptkbp:customer_support |
gptkb:United_States_Army
|
| gptkbp:design |
Tiltrotor
completed multiple prototypes Bell and Lockheed Martin Bell Helicopter and Lockheed Martin |
| gptkbp:design_advantage |
vertical lift capability
|
| gptkbp:design_feature |
fly-by-wire control system
|
| gptkbp:design_features |
High speed and agility
Fly-by-wire controls |
| gptkbp:design_philosophy |
modular design
|
| gptkbp:design_purpose |
Speed and range improvement
speed and range improvement over existing helicopters |
| gptkbp:development |
gptkb:Lockheed_Martin
2013 to 2020 2013 to 2022 |
| gptkbp:development_cost |
$1 billion
$1.3 billion |
| gptkbp:diameter |
11.6 m
|
| gptkbp:elevation |
25,000 ft
|
| gptkbp:engine_type |
T64-GE-419
|
| gptkbp:first_flight |
Ongoing
ongoing December 18, 2017 Flight testing phase |
| gptkbp:flight_style |
expanded compared to traditional helicopters
|
| gptkbp:folding_rotor_blades |
gptkb:Yes
|
| gptkbp:future_prospects |
significant in military aviation.
|
| gptkbp:has_ability |
multi-mission
Vertical takeoff and landing |
| gptkbp:has_programs |
Joint Multi-Role Technology Demonstrator
|
| gptkbp:height |
6.5 m
22 feet 6 inches |
| https://www.w3.org/2000/01/rdf-schema#label |
Bell V-280 Valor
|
| gptkbp:inspiration |
gptkb:V-22_Osprey
|
| gptkbp:is_tested_for |
planned for 2023
|
| gptkbp:key_concept |
adaptive rotor system
|
| gptkbp:key_feature |
speed and agility
|
| gptkbp:length |
24.5 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:market_segment |
gptkb:military_aircraft
|
| gptkbp:max_speed |
300 knots
|
| gptkbp:max_takeoff_weight |
30,000 pounds
30,000 lb |
| gptkbp:military_branch |
gptkb:United_States_Army
|
| gptkbp:military_outcome |
ongoing
|
| gptkbp:notable_pilots |
gptkb:Bell_test_pilots
|
| gptkbp:operational_range |
1,000 nautical miles
800 nautical miles |
| gptkbp:operational_use |
high
|
| gptkbp:participating_nations |
high
|
| gptkbp:passenger_capacity |
gptkb:14
|
| gptkbp:payload_capacity |
10,000 pounds
|
| gptkbp:primary_mission |
gptkb:military_logistics
logistics support medical evacuation |
| gptkbp:primary_user |
gptkb:United_States_Army
|
| gptkbp:project |
gptkb:prototype
|
| gptkbp:propulsion |
Two engines
two Honeywell HTS900 turboshaft engines |
| gptkbp:range |
2,000 miles
2,100 nautical miles |
| gptkbp:release_date |
October 2016
|
| gptkbp:role |
gptkb:transport_aircraft
gptkb:Future_Vertical_Lift_program Military transport replacement for UH-60 Black Hawk |
| gptkbp:safety_features |
Redundant systems
redundant systems |
| gptkbp:service_entry |
gptkb:2022
|
| gptkbp:target_market |
future vertical lift programs
|
| gptkbp:upgrades |
possible
Potential armament integration |
| gptkbp:vertical_takeoff_and_landing |
gptkb:true
|
| gptkbp:wingspan |
20.1 m
84 feet 6 inches |
| gptkbp:bfsParent |
gptkb:Bell_Helicopter
|
| gptkbp:bfsLayer |
4
|