|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
|
gptkbp:aircraft_type
|
experimental prototype
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:ceiling
|
30,000 ft
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
flying wing
Northrop design team
|
|
gptkbp:design_date
|
1939
|
|
gptkbp:design_feature
|
low drag
|
|
gptkbp:design_influence
|
gptkb:Northrop_B-2_Spirit
|
|
gptkbp:design_philosophy
|
flying wing concept
|
|
gptkbp:disbandment_date
|
1943
|
|
gptkbp:engine_configuration
|
twin-engine
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:Muroc_Army_Air_Field
1941
limited due to war
|
|
gptkbp:flight_style
|
stable at high speeds
expanded during testing
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
12 ft 0 in
|
|
gptkbp:historical_significance
|
pioneered flying wing technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Northrop N-1 M
|
|
gptkbp:influenced_by
|
gptkb:Horten_Ho_229
|
|
gptkbp:inspiration
|
gptkb:stealth_technology
|
|
gptkbp:is_tested_for
|
1941-1943
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced future aircraft designs
|
|
gptkbp:length
|
40 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Corporation
|
|
gptkbp:max_speed
|
300 mph
|
|
gptkbp:max_takeoff_weight
|
20,000 lb
|
|
gptkbp:notable_pilots
|
gptkb:M._J._Mc_Gowan
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_use
|
gptkb:none
|
|
gptkbp:project
|
gptkb:Jack_Northrop
3 years
|
|
gptkbp:related_aircraft
|
gptkb:Northrop_YB-49
|
|
gptkbp:release_date
|
1941
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:significance
|
early flying wing design
|
|
gptkbp:status
|
retired
|
|
gptkbp:tail_type
|
gptkb:none
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:wing_area
|
1,200 sq ft
|
|
gptkbp:wingspan
|
66 ft 4 in
|
|
gptkbp:bfsParent
|
gptkb:John_K._Northrop
gptkb:Jack_Northrop
|
|
gptkbp:bfsLayer
|
5
|