Douglas X-3 Stiletto

E18817

The Douglas X-3 Stiletto was a slender, jet-powered experimental research aircraft of the early 1950s designed to investigate sustained supersonic flight and advanced aerodynamic concepts for future high-speed aircraft.

AI illustration

How this image was made

AI-generated illustration of Douglas X-3 Stiletto

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 Douglas X-3 Stiletto (The Douglas X-3 Stiletto was a slender, jet-powered experimental research aircraft of the early 1950s designed to investigate sustained supersonic flight and advanced aerodynamic concepts for future high-speed aircraft.)

All labels observed (1)

Label Occurrences
Douglas X-3 Stiletto canonical 2

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf experimental aircraft ⓘ
jet-powered aircraft ⓘ
research aircraft ⓘ
supersonic aircraft ⓘ
aircraftCategory X-plane ⓘ
airframeMaterial primarily metal construction ⓘ
configuration mid-wing monoplane ⓘ
single-seat ⓘ
twin-engine ⓘ
countryOfOrigin United States ⓘ
crew 1 ⓘ
designedFor advanced aerodynamic concepts research ⓘ
future high-speed aircraft development ⓘ
sustained supersonic flight investigation ⓘ
displayLocation National Museum of the United States Air Force ⓘ
displayLocationCity Dayton, Ohio ⓘ
linked to: Dayton
era early 1950s ⓘ
firstFlight 1952-10-20 ⓘ
fuselageType slender fuselage ⓘ
intendedRole aerodynamic research ⓘ
supersonic research ⓘ
landingGear tricycle landing gear ⓘ
manufacturer Douglas Aircraft Company ⓘ
maximumSpeed about Mach 1.2 in a dive ⓘ
subsonic in level flight ⓘ
noseGearFeature long nose gear strut ⓘ
noseType very long pointed nose ⓘ
notableFor data on slender-fuselage high-speed design ⓘ
investigation of inertial roll coupling ⓘ
numberBuilt 1 ⓘ
operator National Advisory Committee for Aeronautics ⓘ
linked to: NACA

United States Air Force ⓘ
powerplant 2 × Westinghouse J34 turbojet engines ⓘ
primaryUser USAF ⓘ
programOutcome did not achieve planned sustained Mach 2 performance ⓘ
programSponsor NACA ⓘ
United States Air Force ⓘ
programType experimental research program ⓘ
reasonForPerformanceLimitation underpowered engines ⓘ
registrationOrSerial USAF serial 49-2892 ⓘ
researchFocus stability and control at transonic and supersonic speeds ⓘ
structural loads at high speed ⓘ
status retired ⓘ
successorInfluenceOn later supersonic fighter designs ⓘ
slender-fuselage high-speed aircraft concepts ⓘ
tailType conventional tail ⓘ
usedBy NACA High-Speed Flight Station ⓘ
wingPlacement low-to-mid wing ⓘ
wingType small straight wings ⓘ

How these facts were elicited

Referenced by (2)

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