Northrop N-52 Flying Wing
USAF designation: YRB-49A, RB-49A-CF (cancelled)
Engines: 6 x 5,600 lb. Alison J35-A-19 (or -15?)
First flight: May 4, 1950 (by Fred C. Bretcher,
Dale Johnson)
Like the canceled B-49, the RB-49A grew
out of the unconventional XB-35, under
development by Northrop since 1941. In April 1948, the Air Staff and high ranking
officers of the Air Materiel Command, after comparing reconnaissance versions
of the Northrop B-35,
Boeing B-47 and B-50, and Republic F-12, concluded that perhaps the
eventual RB-49A could "realistically" perform
a portion of the strategic reconnaissance mission. Undoubtedly, this optimistic
appraisal stemmed from the testing already accomplished on the Northrop aircraft,
as well as from the aircraft's range, speed, altitude, and growth potential
with combinations of turbojet and turboprop engines. Therefore, 3 versions
of an ever improving RB-49A were planned — an initial aircraft with eight TB-190A
(General Electric J47) turbojets, an interim model powered by six Westinghouse
J40 engines (when they became available), and an ultimate configuration, which
would achieve greater range and economy with two Turbodyne T37 turboprops and
two TG-190A engines. The ultimate model was not an immediate possibility, since
the T37 engines would not be available until October 1951 or later.
However, the aircraft's basic development did not take shape until March 1948
when the contractor, after canvassing possible uses for the "flying wing;'
submitted to the Air Force proposals for a photographic reconnaissance version
of the aircraft. Briefly referred to as the FB-49A, then the RB-49A,
the proposed aircraft would be essentially a YB-49, stripped of items required
only for
bombardment
missions and incorporating necessary photographic apparatus. The formal nomenclature
of the prototype became YRB-49A, a six-engined
reconnaissance bomber with two engines in underwing nacelles to increase the
volume available
for fuel, which was the last chance for the flying wing design.
It was initially planned for five YB-35s
and 4 YB-35As
to be converted to six-jet configuration, fitted with cameras and redesignated RB-35B (later
to be redesignated YRB-49A). Believing that the planned RB-49A configuration
truly had merits, and still eager to salvage its costly investment in the
unfortunate XB-35 program, the
Air Force promptly decided to endorse the YRB-49A development. Following notice
of the decision in May 1948, Northrop received a letter contract on 12 June
for preliminary engineering work looking toward an eventual production contract
for 30 reconnaissance aircraft, at a cost of $86,800,420, this total to include
aircraft, engineering data, and flight testing.
Signed on 12 August 1948, Contract W33-038-ac-21721 covered the production
of 30 RB-49As and a static test shell. One of the aircraft was to be built
by Northrop, the remaining 29 by Consolidated Vultee, at the latter's government
leased plant in Fort Worth, Texas. The agreement had been preceded by difficult
negotiations, the two contractors being unwilling from the start to accept
the Air Force's contention that the nation would benefit from a pooling of
Northrop's
engineering skill and Consolidated's experience in quantity production of large
aircraft.
Support of the RB-49A production program was
short lived. Less than 2 months after the contract's signature, several Air
Materiel Command officials
concluded
that the program's initial eight jet version would only be "satisfactory
as an interim installation." In late September, the Air Force also began
to encounter difficulties in pinning down the 2 contractors' future delivery
dates for the 30 RB-49As. Just as disturbing was the continuing
indecision over which prototype Northrop would use to develop the YRB-49A.
At first,
the remaining YB-49 was chosen. Then, various versions of the 13 YB-35s ordered
in 1942 were reviewed, before settling on modification of the third B-35
prototype, a
YB-35A featuring specific reconfiguration changes dictated early in 1945.
Against this clouded background, a board representing numerous Air Staff offices
met in November to review the requirements for reconnaissance aircraft. All
3 versions of the future RB-49As came under fire. The 8 jet RB-49A, it appeared,
would not be available until January 1950 and would have an inadequate operating
radius; the 6 jet model, planned for 1951, would be much slower than the B-47;
finally, Northrop could not promise the ultimate turboprop turbojet version
until 1953, at which time that particular RB-49A would be in competition with
(and outclassed by) the B-52. The Air Staff Board, therefore, recommended elimination
of the RB-49A.
The RB-49A production program was irrevocably canceled in late December 1948,
as the new USAF Board of Senior Officers" supported the Air Staff Board's
recommendation, deciding also soon afterward to substitute the procurement
of additional B-36s for the deleted RB-49As. The RB-49 offered no real advantages
over the B-47 and the new B-52. Only one YB-35A (42-102376)
was modified with six jet engines as a YRB-49A. The RB-49
cancellation thefore became official in mid-January 1949, even before the single
YRB-49A flew, when the Air Materiel Command directed Northrop
to stop work on all phases of the reconnaissance version except for completion
and test of the one YRB-49A. Conversion of the third YB-35A was "shop
completed" by February 1950, shortly after the Northrop project was totally
cut back to the level of a low budget, state of the art research and development
endeavor.
The YRB-49A differed significantly from the third YB-35A by featuring
6 engines instead of 8. Four of the YRB-49's six J35s were internally mounted;
2 were outside
of the airframe. The removal of 2 engines and the relocation of an additional
2, allowed the YRB-49A to carry much more fuel, a configuration change designed
to extend the aircraft's range. Yet, despite the contractor's continuing
attempts to revive its program, the April delivery deadline set by the Air
Force was
not met. The YRB-49A's
first flight occurred on 4 May, a one month slippage due to the time consumed
in installing additional instrumentation. Like the YB-49, the reconnaissance
prototype's first flight was from Hawthorne to Edwards AFB, California.
The YB-49 and YRB-49A programs
continued into the late 1940s and early 1950s, but neither of these jet powered
flying wing programs was successful. The YRB-49A's test program was quickly
marred by a potentially fatal accident. On 10 August 1950, during its tenth
test flight, the reconnaissance prototype
was in a climb at approximately 35,000 feet, at a speed of about 225 miles
per hour, when the canopy failed and blew off, tearing away the pilot's oxygen
mask and injuring him slightly. Only because the alert flight engineer supplied
emergency oxygen was the pilot able to land the aircraft without further incident.
The test program was resumed after a replacement canopy was provided and various
aircraft modifications were made. No test flights were recorded after 20 September
1950, even though the aircraft was probably still test flown on and off. In
any case, on 6 May 1952, the Air Materiel Command indicated that there was "no
future flying time scheduled" for the YRB-49A.
And so the last of the "flying wings" was flown to Northrop's
Ontario International Airport facility, and it most likely remained in storage
for 18 months. The Air Force reclaimed and scrapped the aircraft in November
1953.
Population: 1 former YB-35A modified [42-102376]
Specs:
Length: 53.08 ft. (16.20 m)
Height: 20 ft. (6.09m) (or 15 ft.?)
Wingspan: 172 ft. (52.40 m)
Wingarea: 4,000.0 sq. ft. (371.5 sq. m)
Empty weight: 84,000 lb.
Loaded weight: 193,938 lbs (87,953 kg) (or 165,000 lb.?)
Maximum weight: 206,000 lb.
Amament : 188 lb. T-89 Flash bombs × 6
Bomb Load : 14,515 kg
Performance:
Range 3,155 miles (5080 km), 2,250 miles (basic mission)
Cruise speed: 419 mph (674 km/h, 364 kt) (or 340 mph?)
Maximum speed: 493 mph (793 km/h, 429 kt) (or 381 mph?)
Ceiling: 40,700 ft. (12,400 m), 45,500 ft. (basic mission)
Crew/passengers: 3

Main sources:
- Joe Baugher's B-49 page
- GlobalSecurity.org
- Northrop Slovak site
- Northrop Japanese site
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