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gptkbp:instance_of
|
gptkb:mythological_figure
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Horten_brothers
|
|
gptkbp:aircraft_operated
|
research and development
Hermann Horten
cantilever wing
5.5 kg/m²
experimental glider
|
|
gptkbp:aspect_ratio
|
10:1
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:controls
|
stick and rudder
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:date
|
1930s
|
|
gptkbp:design
|
efficiency
Reimar Horten
|
|
gptkbp:developer
|
gptkb:Horten_brothers
|
|
gptkbp:engine
|
50 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
swept wings
|
|
gptkbp:first_flight
|
gptkb:government_agency
1941
stable and controllable
|
|
gptkbp:flaps
|
gptkb:none
|
|
gptkbp:floors
|
trimmable
|
|
gptkbp:historical_significance
|
early flying wing design
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Horten Ho 2
|
|
gptkbp:influenced_by
|
Horten Ho 1
|
|
gptkbp:inspiration
|
flying wing concept
|
|
gptkbp:landing_gear
|
fixed landing gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:material
|
gptkb:museum
monocoque
high aspect ratio
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
150 m
70 km/h
200 m
|
|
gptkbp:nationality
|
gptkb:government_agency
|
|
gptkbp:notable_ships
|
fixed rudder
|
|
gptkbp:number_built
|
2
|
|
gptkbp:production_years
|
1941
|
|
gptkbp:range
|
300 km
|
|
gptkbp:role
|
training glider
|
|
gptkbp:roll_rate
|
3°/s
|
|
gptkbp:service_ceiling
|
4000 m
|
|
gptkbp:setting
|
tailless
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:successor
|
Horten Ho 3
|
|
gptkbp:surface
|
elevator and ailerons
|
|
gptkbp:tail_type
|
gptkb:none
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:used_in
|
gptkb:World_War_II
|
|
gptkbp:weight
|
200 kg
400 kg
|
|
gptkbp:wingspan
|
15.5 m
|