Sikorsky S-30

From Wikipedia, the free encyclopedia
S-30
Role Light transport
National origin United States
Manufacturer Sikorsky Manufacturing Corporation
Designer Igor Sikorsky

The Sikorsky S-30 was a proposed aircraft design by Igor Sikorsky to be built by the Sikorsky Manufacturing Corporation at Roosevelt, New York in 1925. The twin engine biplane was to have been used on mail routes or configured as a commercial passenger airliner. No examples of the S-30 were ever manufactured.[1][2]

Specifications

Data from Aerofiles[3]

General characteristics

Performance

  • Cruise speed: 100 mph (161 km/h; 87 kn)
  • Range: 500 mi (434 nmi; 805 km)

References

  1. ^ "S-30". all-aero.com. Retrieved 14 May 2017. 
  2. ^ "The American Fixed Wing Era". www.sikorskyarchives.com. Sikorsky Archives. Retrieved 14 May 2017. 
  3. ^ "S-30". aerofiles.com. 2014. Retrieved 14 May 2017. 
Retrieved from "https://en.wikipedia.org/w/index.php?title=Sikorsky_S-30&oldid=781171234"
This content was retrieved from Wikipedia : http://en.wikipedia.org/wiki/Sikorsky_S-30
This page is based on the copyrighted Wikipedia article "Sikorsky S-30"; it is used under the Creative Commons Attribution-ShareAlike 3.0 Unported License (CC-BY-SA). You may redistribute it, verbatim or modified, providing that you comply with the terms of the CC-BY-SA