Sikorsky S-30 - Aeroplane - avia.wikisort.org

avia.wikisort.org - Aeroplane

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]

S-30
Role	Light transport
National origin	United States
Manufacturer	Sikorsky Manufacturing Corporation
Designer	Igor Sikorsky

Specifications

Data from Aerofiles[3]

General characteristics

Crew: Two
Capacity: 10 passengers or 1,800 pounds (820 kg)
Powerplant: 2 × Wright R-790 Whirlwind Air-cooled 9-cylinder radial engines, 200 hp (150 kW) each

Performance

Cruise speed: 100 mph (160 km/h, 87 kn)
Range: 500 mi (800 km, 430 nmi)

References

"S-30". all-aero.com. Retrieved 14 May 2017.
"The American Fixed Wing Era". www.sikorskyarchives.com. Sikorsky Archives. Retrieved 14 May 2017.
"S-30". aerofiles.com. 2014. Retrieved 14 May 2017.

v t e Sikorsky aircraft
Fixed-wing aircraft (company designations)	S-1 S-2 S-3 S-4 S-5 S-6 S-7 S-8 S-9 S-10 S-11 S-12 S-13 S-14 S-15 S-16 S-17 S-18 S-19 S-20 S-21 S-22 S-23 S-24 S-25 S-26 S-27 S-28 S-29-A S-30 S-31 S-32 S-33 S-34 S-35 S-36 S-37 S-38 S-39 S-40 S-41 S-42 S-43 VS-44 S-45
Fixed-wing aircraft (military designations)	C-6 C-28 JRS JR2S PS RS XBLR-3 XPBS XSS XV-2
Helicopters (company designations)	VS-300 (S-46) S-47 S-48 S-49 S-50 S-51 S-52 S-53 S-54 S-55 S-56 S-57 S-58 S-59 S-60 S-61 S-61L/N S-61R S-62 S-63 S-64 S-65 S-66 S-67 S-68 S-69 S-70 S-71 S-72 S-73 S-74 S-75 S-76 S-80 S-92 S-97 S-100 S-300 S-333 S-434
Helicopters (military designations)	SH-3 HH-3E/F R-4 H-5 H-6 H-18 H-19 H-34 CH-37 XH-39 HH-52A CH-53 CH-53E CH-53K MH-53 CH-54 UH-60 HH-60G HH-60J/MH-60T MH-60R/S SH-60B/F H-60J/K VH-60 RAH-66 VH-92 CH-124 CH-148 HLH
Experimental aircraft	Cypher/Cypher II Firefly Raider Raider X SB-1 X2 XBLR-3 XV-2

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