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Northrop YB-49


Flying Wing Bomber Prototype


United States | 1947



"The Northrop YB-49 jet bomber was an evolved form of the earlier piston-powered YB-35 flying wing design."

Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Northrop YB-49 Flying Wing Bomber Prototype.
8 x Allison / General Electric J35-A-5 turbojets developing 4,000 lb of thrust each.
Propulsion
493 mph
793 kph | 428 kts
Max Speed
45,932 ft
14,000 m | 9 miles
Service Ceiling
9,942 miles
16,000 km | 8,639 nm
Operational Range
3,758 ft/min
1,145 m/min
Rate-of-Climb
Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the Northrop YB-49 Flying Wing Bomber Prototype.
7
(MANNED)
Crew
52.5 ft
16.00 m
O/A Length
171.9 ft
(52.40 m)
O/A Width
20.3 ft
(6.20 m)
O/A Height
88,405 lb
(40,100 kg)
Empty Weight
194,007 lb
(88,000 kg)
MTOW
Armament
Available supported armament and special-mission equipment featured in the design of the Northrop YB-49 Flying Wing Bomber Prototype .
STANDARD:
4 x 0.50 caliber (12.7mm) Browning M3 heavy machine guns in tail "stinger" unit.

OPTIONAL:
Up to 32,000 lb of internal stores.
Variants
Notable series variants as part of the Northrop YB-49 family line.
YB-49 - Base Series Designation; three units completed with several others ending in various states of conversion/construction prior to project termination.
YRB-49A - Proposed long-range reconnaissance model; sole example scrapped in 1953.
RB-49A - Proposed designation for YRB-49A series in service.
B-49 - Proposed in-service designation for YB-49 model


Authored By: Staff Writer | Last Edited: 01/29/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.

The YB-49 strategic bomber prototype came about as an extension of the ultimately-cancelled XB-35/YB-35 project. The major difference between the two lines was the YB-49's switch to an all-turbojet-powered arrangement (the B-35 series relied on radial piston engines in a "pusher" configuration). Like the XB-35/YB-35 before it, the YB-49 also eventually suffered cancellation. Just two were completed with seven more remaining in various stages of conversion from the YB-35 standard at the end.

The pre-production quality YB-35 served as the basis for two YB-49 prototypes and was part of the shift of the USAAF to jet-powered forms late in World War 2 (1939-1945). The installation of eight Allison J35 turbojets (4,000lb thrust each) provided an instant increase in performance - particularly in maximum speed and altitude while reducing the operating ranges by as much as 50% when compared to the piston-powered form. The general arrowhead design was retained and the nine-person crew was now reduced to seven.

The prototype YB-49 made its maiden flight on October 21st, 1947 and showcased a promising future in testing. All gains were lost when the second airframe crashed, killing all of its crew, on June 5th, 1948 - the wing mainplanes had become detached from the fuselage section during flight, making recovery impossible. In February of 1949, a YB-49 completed a flight from Muroc AFB to Andrews AFB covering four hours and twenty-five minutes. On its return trip, half of the engines suffered issues and were shutdown.

With the termination of the YB-35 project in 1949, the YB-49 continued on. However, another crash in March of 1950 only added to the project's woes. A nosewheel collapse being blamed for the resulting accident, fire spreading from the fully-fueled aircraft. By this time YB-35 line was already under conversion to turbojet form. On the whole, the YB-49 performed excellently despite its highly publicized issues.

Like the YB-35, the YB-49 was done in by technological challenges and politics at both the industry and governmental levels. Jack Northrop, founder of the Northrop aviation concern, would not see his dream of the flying wing realized until he received an early look at the in-development B-2 "Spirit" stealth bomber just prior to his death in 1981. The Spirit was officially introduced into service in 1997 and continues to fly today (2015).

As completed, the YB-49 featured a crew of seven and dimensions were made up of a 16 meter running length, a 52.4 meter wingspan and a 6.2 meter height. Empty weight was 40,115 kilograms against a Maximum Take-Off Weight (MTOW) of 88,000 kilograms. Power was from 8 x Allison / General Electric J35-A-5 series turbojet engines developing 4,000 lb thrust each. Performance included a maximum speed of 495 mph, a range out to 9,980 miles (ferry), a combat radius of 1,615 miles, a service ceiling of 45,700 feet and a rate-of-climb nearing 3,760 feet-per-minute. Proposed armament was 4 x 0.50 caliber Browning M3 Heavy Machine Guns (HMGs) set in a tail "stinger" position (as in the proposed XB-35/YB-35). The internal bomb load was to be 32,000 lbs, far less than the 51,000 lb war load estimated for the B-35 design.

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Operators
Global customers who have evaluated and/or operated the Northrop YB-49. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 3 Units

Contractor(s): Northrop - USA
National flag of the United States

[ United States (cancelled) ]
1 / 1
Image of the Northrop YB-49
Image from the Public Domain.

Going Further...
The Northrop YB-49 Flying Wing Bomber Prototype appears in the following collections:
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