Pratt & Whitney R-1860-17 engines

Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules

vikingBerserker

Lieutenant General
28,790
4,609
Apr 10, 2009
South Carolina
Does anybody have this book? I m trying to find out the HP for the R-1860-17 Twin Hornets. So far I have seen 525, 575, 600, 630, and 700 from various books and Air Corps documents.

1598223048323.png
 
I have the book and it is of little help. the section on the R-1860 is about 4 pages including tables. It does say that 446 were built compared to 2,944 of the Hornet "A"s which stayed in production much longer.
 
Does anybody have this book? I m trying to find out the HP for the R-1860-17 Twin Hornets. So far I have seen 525, 575, 600, 630, and 700 from various books and Air Corps documents.

View attachment 592576
Wiki is always a good place to start.
Just Google the name of the engine (in this case, I Googled "P&W Hornet R-1860").
Looks like it made 575 HP @ 1950 rpm, but at what altitude, I don't know.

Pratt & Whitney R-1860 Hornet B - Wikipedia
 
The Devil is in the details. The dash number is of critical importance whenever you are asking about US based engines. Each sub-type was optimised for a specific use, or environment. I just hate seeing (for example) "The R-2800 generated 2000 hp". No, it didn't, at least not ALL R-2800's. Some managed as much as 2800 hp, on a daily basis. Most, yes, came close, but at different altitudes. And different RPM settings.
Sorry. Rant over...
... for now...
 
The Devil is in the details. The dash number is of critical importance whenever you are asking about US based engines. Each sub-type was optimised for a specific use, or environment. I just hate seeing (for example) "The R-2800 generated 2000 hp". No, it didn't, at least not ALL R-2800's. Some managed as much as 2800 hp, on a daily basis. Most, yes, came close, but at different altitudes. And different RPM settings.
Sorry. Rant over...
... for now...
I hear ya, Chief, but at least its a place to start.
 

Users who are viewing this thread

Back