The Sikorsky S-75 was a proof-of-concept all-composite helicopter built under the United States Army Advanced Composite Airframe Program, whose goal was a lighter and cheaper airframe than the metal ones then in use, in support of the Light Helicopter Experimental program. Contracts went to Sikorsky and Bell in February 1981. The S-75 joined an entirely new composite airframe, mostly Kevlar and graphite, to the twin turboshaft engines, transmission and rotors of the civil S-76A, and carried two pilots and up to six passengers. It first flew on 27 July 1984, passed a 50-hour Army evaluation that beat the weight and cost targets, and was put into long-term storage after testing ended in April 1985.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Sikorsky S-75 (Wikipedia)
Of Make
Source Sikorsky S-75 (Wikipedia)
Sources
1. Sikorsky S-75 (Wikipedia)
Design and development, first flight
The S-75 flew for the first time on 27 July 1984.
Lead
The Sikorsky S-75 was a proof-of-concept all-composite helicopter.
Design and development
mated an entirely new composite airframe with the twin turboshaft engines
Specifications
Empty weight: 6,421 lb (2,913 kg)
Specifications, maximum take-off weight
Max takeoff weight: 8,470 lb (3,842 kg)
Specifications, maximum speed
Maximum speed: 160 kn (180 mph, 300 km/h)
Lead, builder
Sikorsky Aircraft used all-composite materials to replace metal
Lead, origin
Advanced Composite Airframe Program
Of Make: Sikorsky Aircraft, Lead, maker
Sikorsky Aircraft used all-composite materials to replace metal
In Group: Military Transport and Utility Helicopters, Lead, type of aircraft
The aircraft was flown by two pilots, and could carry up to six passengers in the 100-cubic-foot (2.8 m3) rear cabin.
Exemplifies: Helicopter Transport, Lead, rotorcraft
The aircraft was flown by two pilots, and could carry up to six passengers in the 100-cubic-foot (2.8 m3) rear cabin.
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