The Sikorsky S-73 was a proposed heavy lift helicopter that Sikorsky Aircraft designed to meet the United States Army requirement of 1970 for a Heavy Lift Helicopter able to carry 45,000 pounds, more than twice the capacity of Sikorsky most powerful helicopter then flying. It was an enlarged version of the CH-54 and S-64 with a simplified single main rotor driven by three General Electric TF34-58 turboshaft engines of 21,000 horsepower combined, and a crew of five working from a forward cockpit with push buttons in place of the usual cyclic stick and collective lever. A rear cabin would have held 12 combat troops. Sikorsky submitted the design in February 1971, and in May the Army chose the Boeing Vertol XCH-62, ending the S-73 programme.
Facts
Engine Class StatusDesign only (never built) 1 Maximum Mass (kg) Connections
Exemplifies
Source Sikorsky S-73 (Wikipedia)
Of Make
Source Sikorsky S-73 (Wikipedia)
Sources
1. Sikorsky S-73 (Wikipedia)
Lead, design submission
Sikorsky submitted their design in February 1971
Lead, builder
The Sikorsky S-73 was a proposed aircraft design
Lead, engine class
powered by three General Electric TF34-58 turboshaft engines
Specifications
Empty weight: 59,000 lb (26,762 kg)
Specifications, maximum take-off weight
Max takeoff weight: 118,000 lb (53,524 kg)
Lead, origin
the United States Army requirement in 1970 for a Heavy Lift Helicopter
Of Make: Sikorsky Aircraft, Lead, maker
an enlarged version of the successful CH-54/S-64
In Group: Military Transport and Utility Helicopters, Lead, type of aircraft
Heavy Lift Helicopter (HLH) capable of carrying 45,000 lb
Exemplifies: Helicopter Transport, Lead, rotorcraft
Heavy Lift Helicopter (HLH) capable of carrying 45,000 lb
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