From att-mt!ihlpl.att.com!jfb Mon Mar  1 12:15:46 1993
Path: cbnewsd!cbnewsc!att!linac!uwm.edu!cs.utexas.edu!sdd.hp.com!ncr-sd!ncrcae!ncrhub2!ciss!law7!military
From: jfb@ihlpl.att.com
Newsgroups: sci.military
Subject: Number Fifty-Two in the Series--Bell XP-52
Keywords: Never built
Message-ID: <C37zyB.2r2@law7.DaytonOH.NCR.COM>
Date: 1 Mar 93 17:15:46 GMT
Sender: military@law7.DaytonOH.NCR.COM (Sci.Military Login)
Organization: AT&T Bell Laboratories -  Naperville, Illinois
Lines: 58
Approved: military@law7.daytonoh.ncr.com


>From jfb@ihlpl.att.com


The Bell XP-52 was an unorthodox fighter project that arose out of a 
USAAC competition held in the winter of 1939 for a fighter that would 
be much more effective than any extant--with a top speed, rate of 
climb, maneuverability, armament, and pilot visibility, all of which 
would be far superior to those of any existing fighter.  In addition, 
the fighter was required to have a low initial cost and had to be easy 
and inexpensive to maintain.  A tall order, indeed! 

The USAAC issued its requirements to the industry in the form of 
Request for Data R-40C.  No less than 50 responses came in.  Among 
these was the Model 16, which the Bell company had developed some 
months earlier.  Bell was famous for submitting unconventional 
designs, and the Model 16 was no exception.  It had a round, 
barrel-shaped fuselage with the pilot seated in the nose and a 1250 hp 
Continental XIV-1430-5 liquid-cooled twelve-cylinder inverted vee 
engine mounted behind the pilot and driving a pair of contrarotating 
coaxial propellers operating in pusher fashion.  The wing was mounted 
in mid-fuselage position, and was swept back at an angle of about 20 
degrees.  Twin booms were mounted about one-third of the way along the 
wings outboard of the fuselage.  The horizontal tailplane at the rear 
connected the two booms.  A tricycle landing gear was to be fitted, 
with the nosewheel retracting into the fuselage and the mainwheels 
retracting into the booms.  

One unusual feature of the XP-52 was the presence of an air inlet for 
the engine radiators mounted in the extreme nose, a feature which was 
to be seen later in jet-powered fighters.  Two 20-mm cannon were to be 
mounted in the lower fuselage, and three 0.50-in machine guns were to 
be mounted in the front of each of the twin booms.  

By the end of 1940, the Army purchasing commission had chosen six of 
the submissions for further development.  Among them was the Bell 
Model 16.  A single prototype was ordered under the designation XP-52.  
However this order was canceled on November 25, 1941, before anything 
could be built.  It was replaced by an order for another Bell design, 
based on the XP-52 but equipped with a more-powerful Pratt & Whitney 
R-2800-52 air-cooled radial engine.  This aircraft was assigned the 
designation XP-59 by the US Army.  

Estimated performance of the XP-52 included a maximum speed of 425 mph 
at 19,500 feet.  It was expected that an altitude of 20,000 feet could 
be attained in 6.3 minutes and that the service ceiling would be 
40,000 feet.  Maximum range was to be 960 miles.  Weights were 
estimated to be 6840 lbs empty and 8750 lbs gross.  Dimensions were 
wingspan 35 feet, length 34 feet, height 9 feet 3 inches, and wing 
area 233 square feet.  

Source: 

  The American Fighter, Enzo Angelucci and Peter Bowers, Orion, 1987.  

Joe Baugher       AT&T Bell Laboratories    2000 North Naperville Road 
		  Naperville, Illinois 60566-7033.   (708) 713-4548



