Pratt & Whitney R-1340-S1H1-G Wasp

New Topic
Pratt & Whitney R-1340-S1H1-G Wasp

Arrangement of cylinders: radial devítiválec
Cooling: air
Cylinder bore: 146 mm
Stroke: 146 mm
Displacement: 22,0 liter (dm3)
The degree of compression: 6,0:1
Divorce: OHV (1 intake valve and 1 exhaust for each cylinder head)
Fuel: 87 octane
Carburetor: Stromberg
Supercharger: a mechanical supercharger
Length: 1 of 212.5 mm
The diameter of the engine: 1 305 mm
Weight: 421 kg
Performance:
600 hp at 2 250 r/min at the start
550 hp at 2 200 rpm/min at h= 2 440 m - maximum performance
400 hp at 2 000 rpm - continuous power

Source:
www.oldengine.org
author archive.
URL : https://www.valka.cz/Pratt-Whitney-R-1340-S1H1-G-Wasp-t66435#235179 Version : 0
Pre airplane CAC Wirraway vyrábala this engine in licencii austrálska the company the Commonwealth Aircraft Co.

Source:
Novotný, Josef: the Commonwealth Wirraway, Edition of the Triad, volume 4,.
URL : https://www.valka.cz/Pratt-Whitney-R-1340-S1H1-G-Wasp-t66435#468035 Version : 0
Discussion post Fact post
Attachments

Join us

We believe that there are people with different interests and experiences who could contribute their knowledge and ideas. If you love military history and have experience in historical research, writing articles, editing text, moderating, creating images, graphics or videos, or simply have a desire to contribute to our unique system, you can join us and help us create content that will be interesting and beneficial to other readers.

Find out more