National Museum of the USAF   Right Corner Banner
Join the Air Force

Home > Fact Sheets > North American XB-45

NORTH AMERICAN XB-45

Posted 7/7/2009 Printable Fact Sheet
 
Photos
Previous ImageNext Image
North American XB-45
North American XB-45 (S/N 45-59479) in flight. (U.S. Air Force photo)
Download HiRes

The development of the XB-45 was initiated in August 1944 in response to a spring 1944 request by the Army Air Force for proposals using the newly developed General Electric J35 axial-flow turbojet engine. The AAF issued requirements for a 500 mph top speed, a 1,000-mile combat radius and service ceiling of at least 40,000 feet. North American submitted its preliminary design studies in December and got approval for full-scale development in March 1945. Besides the North American XB-45, the Consolidated XB-46, Boeing XB-47 and Martin XB-48 resulted from the Army request.

The XB-45 was powered by four J35s arranged in pairs in wing-mounted nacelles. The Army considered jet bombers to be so fast that only the tail of the aircraft needed to be defended. The XB-45 carried only two .50-cal. machine guns in the tail. The power-assisted turret guns were fired manually by a tail gunner. The rest of the four man crew consisted of a pilot, copilot-radio operator and bombardier-navigator. The normal bomb load of the XB-45 was 8,000 lbs., but it was capable of carrying one 22,000 lb. "Grand Slam" bomb.

Three XB-45 prototypes were built and the first flight was March 17, 1947. The XB-45 competed against the four-engine XB-46 and proved superior. An initial production contract for 97 aircraft, built as B-45A, made the aircraft the first production all-jet bomber to enter service with the USAF.


Type Number built/
converted
Remarks
XB-45 3 XB-45


TECHNICAL NOTES:
Armament: Two .50-cal. machine guns in the tail and 8,000 lbs. of bombs; note the aircraft could carry one 12,000-lb. "Tall Boy" or one 22,000-lb. "Grand Slam" bomb
Engines: Four Allison J35-A-11 turbojets of 4,000 lbs. thrust each
Maximum speed: 500 mph
Cruising speed: 419 mph
Range: 2,920 miles
Service ceiling: 38,500 ft.
Span: 89 ft. 6 in.
Length: 74 ft. 0 in.
Height: 25 ft. 2 in.
Weight: 66,820 lbs. (gross weight)
Crew: Four (pilot, copilot-radio operator, bombardier-navigator, tail gunner)
Serial numbers: 45-59479 to 45-59481

Click here to return to the Bomber Aircraft index.







 Inside the Museum

ima cornerSearch

ima cornerArchive - Online Aircraft Features

 


tabCategories
tabRelated Links
tabConnect

Museum Virtual TourMuseum Facebook PageMuseum Twitter PageMuseum Instagram
Museum Google Plus PageMuseum Pinterest PageMuseum YouTube ChannelMuseum Flickr Page
Museum PodcastsMuseum E-newsletter Sign-upMuseum RSS Feeds



Site Map      Contact Us     Questions     USA.gov     Security and Privacy notice     E-publishing  
Suicide Prevention    SAPR   IG   EEO   Accessibility/Section 508   No FEAR Act