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gptkbp:instance_of
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gptkb:rocket
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Heinkel_He_178
|
|
gptkbp:aircraft_operated
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gptkb:Ernst_Udet
gptkb:aircraft
gptkb:Heinkel_He_178
gptkb:item
research and development
low-wing monoplane
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|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:date
|
1930s
|
|
gptkbp:design
|
gptkb:Hermann_Pohlmann
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:features
|
streamlined fuselage
|
|
gptkbp:first_flight
|
gptkb:1944
1939
|
|
gptkbp:fuel_type
|
liquid oxygen and gasoline
|
|
gptkbp:historical_significance
|
pioneering rocket flight
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Heinkel He 176
|
|
gptkbp:influenced_by
|
V-2 rocket technology
early jet technology
|
|
gptkbp:inspiration
|
future rocket aircraft designs
|
|
gptkbp:is_tested_for
|
gptkb:Peenemünde
German rocket aircraft program
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced space exploration technology.
|
|
gptkbp:length
|
8.0 m
|
|
gptkbp:manufacturer
|
Heinkel
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
600 km/h
|
|
gptkbp:max_takeoff_weight
|
2,500 kg
|
|
gptkbp:members
|
3°/s
|
|
gptkbp:notable_feature
|
first aircraft to fly using a liquid-fueled rocket engine.
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_history
|
limited
|
|
gptkbp:origin
|
gptkb:government_agency
|
|
gptkbp:propulsion
|
gptkb:rocket
1,500 kgf
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:strikeouts
|
4°/s
|
|
gptkbp:surface
|
elevators, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
experimental rocket aircraft
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wingspan
|
8.5 m
|