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Douglas X-3 Stiletto High-Speed Research Aircraft Family

The Douglas X-3 Stiletto was a single-seat research aircraft intended to take off under its own power and sustain Mach 2 flight while testing low-aspect-ratio wings and extensive titanium construction. Its substitute Westinghouse J34 engines left it severely underpowered: it exceeded Mach 1 only in a dive. An initial hop on October 15, 1952 preceded the official first flight on October 20. During abrupt-roll tests on October 27, 1954, Joseph Walker encountered severe coupled pitch and yaw motions and recovered the aircraft. Those flights became important evidence for understanding inertial roll coupling in slender, high-speed aircraft. The X-3’s final flight was May 23, 1956; its research value lay in stability, structural loads, materials, and tire technology despite the unrealized Mach 2 objective.

Douglas X-3 Stiletto High-Speed Research Aircraft Family
NASA photo E-17348 · NASA content is generally not subject to U.S. copyright and may be used factually for educational or informational purposes with NASA acknowledged; no NASA endorsement is implied. Usage guidelines: https://www.nasa.gov/nasa-brand-center/images-and-media/ · Source
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Identity

Aliases
X-3StilettoDouglas XS-3Douglas Stiletto
Family Name
Douglas X-3 Stiletto
Full Name
Douglas X-3 Stiletto High-Speed Research Aircraft Family
Roles
researchexperimentaltechnology_demonstrator
Status
retired
Type
aircraft

Details

Aircraft Specs
Configuration
fixed_wing
Crew Capacity
1
Operating Modes
land
Takeoff Landing Capabilities
conventional
Description
The Douglas X-3 Stiletto was a single-seat research aircraft intended to take off under its own power and sustain Mach 2 flight while testing low-aspect-ratio wings and extensive titanium construction. Its substitute Westinghouse J34 engines left it severely underpowered: it exceeded Mach 1 only in a dive. An initial hop on October 15, 1952 preceded the official first flight on October 20. During abrupt-roll tests on October 27, 1954, Joseph Walker encountered severe coupled pitch and yaw motions and recovered the aircraft. Those flights became important evidence for understanding inertial roll coupling in slender, high-speed aircraft. The X-3’s final flight was May 23, 1956; its research value lay in stability, structural loads, materials, and tire technology despite the unrealized Mach 2 objective.
First Flight Year
1,952
Last Flight Year
1,956
Manufacturer

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Creation Time
August 13, 2026 at 21:07:34 UTC
Updated Time
October 29, 2026 at 15:19:52 UTC