The Ling-Temco-Vought XC-142 was an experimental tiltwing transport built to test whether vertical and short takeoff aircraft could serve the American armed forces. It came out of the Tri-Service Assault Transport Program that the Army, Navy and Air Force agreed in 1961 under the Navy's Bureau of Naval Weapons. A team of Vought, Ryan and Hiller won the design contest, and a contract for five prototypes was signed in early 1962. It first flew conventionally on 29 September 1964, and on 11 January 1965 it completed its first transition, taking off vertically, changing to forward flight and landing vertically. Four General Electric T64 turboshaft engines on a common driveshaft drove four propellers, and the wing tilted to the vertical for hovering. Five aircraft flew 420 hours in 488 flights with 39 pilots, but driveshaft problems, a crash that killed three and the withdrawal of the services one by one ended the program, and only one aircraft survives.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineGeneral Electric T64 turboshaft 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source LTV XC-142 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source LTV XC-142 (Wikipedia)DevelopmentQuote, Development
Vought responded with a proposal combining engineering from their own design arm, as well as Ryan and Hiller, who had more extensive helicopter experience.
Originated In
Also in Geography Atlas: where this subject originated.
Source LTV XC-142 (Wikipedia)Development, country of originQuote, Development, country of origin
In 1959 the United States Army, Navy and Air Force began work on the development of a prototype V/STOL aircraft
Sources
1. LTV XC-142 (Wikipedia)
Lead
An XC-142A first flew conventionally on 29 September 1964
Lead, body style
The Ling-Temco-Vought (LTV) XC-142 is a tiltwing experimental aircraft designed to investigate the operational suitability of vertical/short takeoff and landing (V/STOL) transports.
Design, engine
The XC-142 was powered by four General Electric T64 turboshaft engines cross-linked on a common driveshaft
Operational history
The aircraft never proceeded beyond the prototype stage.
Operational history, units built
Five XC-142As were built during the 1960s.
Specifications (XC-142A), empty weight
Empty weight: 22,595 lb (10,249 kg)
Specifications (XC-142A), maximum takeoff weight
Max takeoff weight: 44,500 lb (20,185 kg) (STOL)
Specifications (XC-142A), speed
Maximum speed: 431 mph (694 km/h, 375 kn) at 20,000 ft (6,100 m)
Development
Vought responded with a proposal combining engineering from their own design arm, as well as Ryan and Hiller, who had more extensive helicopter experience.
Development, country of origin
In 1959 the United States Army, Navy and Air Force began work on the development of a prototype V/STOL aircraft
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