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The Sikorsky XHJS-1 (manufacturer designation S-53), was developed by Sikorsky Aircraft to meet a Naval requirement for a utility helicopter. The XHJS-1 was not ordered into production and only two prototypes were built.[1]

Sikorsky S-53 / XHJS-1
Role Helicopter
National origin United States
Manufacturer Sikorsky Aircraft
First flight 22 September 1947
Primary user United States Navy
Number built 2
Developed from Sikorsky S-51

Design and development


Powered by a 525 hp (391 kW) Continental R-975-34, the S-53 was a development of the S-51 designed for use on aircraft carriers. The tail rotor was raised above head-height to give more clearance and the landing gear was made stronger to enable operations from a moving deck. Other enhancements were a folding main rotor and the option for amphibious landing gear. Two prototypes were ordered by the United States Navy as the XHJS-1[1] and the first flew on 22 September 1947. The type was evaluated against the Piasecki XHJP-1. With the Piasecki design being ordered as the HUP-1 by the Navy, the S-53 was not developed further.


Variants


XHJS-1
Prototype naval utility helicopter, two built.[1]

Specifications (XHJS-1)


General characteristics


See also


Related development

Aircraft of comparable role, configuration, and era


References


Notes
  1. Andrade 1979, p. 194
Bibliography

На других языках


- [en] Sikorsky XHJS

[it] Sikorsky S-53

Il Sikorsky S-53, indicato anche come Sikorsky XHJS-1 da convenzioni US Navy, fu un elicottero utility monorotore tripala quadriposto, progettato dall'azienda aeronautica statunitense Sikorsky Aircraft Corporation nella seconda parte degli anni quaranta. Venne sviluppato in risposta a un requisito della U.S. Navy per un elicottero polivalente navale. Il progetto XHJS-1 non fu avviato in produzione e ne vennero costruiti solo tre prototipi[2].



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