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Bell X-14 Vectored-Thrust VTOL Research Aircraft Family

The Bell X-14 was a single-aircraft U.S. VTOL research family that demonstrated practical vectored jet thrust for vertical lift, hover, transition, and conventional flight. NASA and Air Force testing from 1957 to 1981 used the X-14 as a long-lived V/STOL handling and control laboratory, and its data influenced later designs including the Hawker P.1127 and Harrier.

Bell X-14 Vectored-Thrust VTOL Research Aircraft Family
NASA/Art Melliar, ARC-1974-AC74-4562-15 · 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-14X-14AX-14BBell Model 68Bell Model 8
Family Name
Bell X-14
Full Name
Bell X-14 Vectored-Thrust VTOL Research Aircraft Family
Roles
researchexperimentaltechnology_demonstrator
Status
retired
Type
aircraft

Details

Aircraft Specs
Configuration
powered_lift
Operating Modes
land
Takeoff Landing Capabilities
vtol
Description
The Bell X-14 was a single-aircraft U.S. VTOL research family that demonstrated practical vectored jet thrust for vertical lift, hover, transition, and conventional flight. NASA and Air Force testing from 1957 to 1981 used the X-14 as a long-lived V/STOL handling and control laboratory, and its data influenced later designs including the Hawker P.1127 and Harrier.
First Flight Year
1,957
Manufacturer
Propulsion Configurations
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Original X-14 configuration; two side-by-side Viper ASV.8 turbojets, approximately 1,900 lbf / 8.45 kN each according to NASA material.
    Name
    Bell X-14 original two-engine Viper ASV.8 installation
    Notes
    The original Bell X-14 fit used two Armstrong Siddeley Viper ASV.8 turbojets. Cascade thrust diverters redirected exhaust for vertical lift, while compressor bleed air fed reaction controls. The physical engine complement is retained in the count-2 entry.
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Later X-14A re-engining; two General Electric J-85 turbojets. Exact J85 variant is not asserted.
    Name
    Bell X-14A two-engine J85 installation
    Notes
    NASA records that the aircraft was later fitted with General Electric J-85 turbojet engines to increase thrust margins and was then redesignated X-14A. The bounded source does not identify a J85 mark, so the existing General Electric J85 family identity is used.

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Creation Time
August 13, 2026 at 22:47:38 UTC
Updated Time
September 8, 2026 at 10:03:23 UTC
Bell X-14 Vectored-Thrust VTOL Research Aircraft Family - AeroVia