Northrop X-21

E20316

The Northrop X-21 was an experimental U.S. jet aircraft of the 1960s designed to test laminar-flow control technology for improved aerodynamic efficiency.

AI illustration

How this image was made

AI-generated illustration of Northrop X-21

This AI-generated illustration was produced by black-forest-labs/FLUX.2-dev (1024x1024) from a prompt written by openai/gpt-oss-120b from the entity's label + description.

Prompt

Generate an image of the Northrop X-21 (The Northrop X-21 was an experimental U.S. jet aircraft of the 1960s designed to test laminar-flow control technology for improved aerodynamic efficiency.)

All labels observed (2)

Label Occurrences
Northrop X-21 canonical 2
X-21 1

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf experimental aircraft ⓘ
jet aircraft ⓘ
research aircraft ⓘ
aircraftCategory fixed-wing aircraft ⓘ
aircraftConfiguration twin-engine jet ⓘ
aircraftType subsonic aircraft ⓘ
airframeOrigin Douglas DC-3 derivative ⓘ
airIntakeLocation underwing engine nacelles ⓘ
countryOfOrigin United States ⓘ
crew 2 ⓘ
designation X-21 ⓘ
linked to: Northrop X-21
designedFor improved aerodynamic efficiency ⓘ
laminar-flow control technology testing ⓘ
engineConfiguration underwing pods ⓘ
engineType turbofan ⓘ
era 1960s ⓘ
firstFlightDate 1963 ⓘ
fullName Northrop X-21 ⓘ
landingGearType tricycle landing gear ⓘ
manufacturer Northrop Corporation ⓘ
linked to: Northrop Grumman
notableFeature extensive wing suction system ⓘ
highly instrumented research aircraft ⓘ
numberBuilt 2 ⓘ
operatorType military research organization ⓘ
powerplantCount 2 ⓘ
primaryRole aerodynamic research ⓘ
laminar-flow control testbed ⓘ
programGoal demonstrate practical laminar-flow control on a transport-type wing ⓘ
programOutcome technology demonstrator ⓘ
programSponsor NASA ⓘ
United States Air Force ⓘ
programType X-plane program ⓘ
propulsionType jet ⓘ
registrationType military experimental designation ⓘ
researchDomain aerodynamics ⓘ
boundary-layer control ⓘ
researchFocus drag reduction ⓘ
fuel efficiency improvement ⓘ
high-Reynolds-number laminar flow ⓘ
researchUser NASA ⓘ
status retired ⓘ
tailConfiguration conventional tail ⓘ
testEnvironment flight testing ⓘ
usedBy United States Air Force ⓘ
wingFeature boundary-layer suction ⓘ
laminar-flow control system ⓘ
perforated wing surface ⓘ
wingPosition low-wing configuration ⓘ

How these facts were elicited

Referenced by (3)

Full triples — surface form annotated when it differs from this entity's canonical label.

Northrop X-21 → designation → X-21 ⓘ
linked to: Northrop X-21
Northrop X-21 → fullName → Northrop X-21 ⓘ