Douglas RB-66B Destroyer
Twin-engine high-wing photo-reconnaissance medium jet bomber

Archive Photos 1

Douglas RB-66B Destroyer (AF 543-0475, c/n 44356) on display (c.1999) at the National Museum of the United States Air Force, Wright Patterson AFB, Dayton, Ohio (Photos by John Shupek)

Overview 2

The Douglas B-66 Destroyer was a light bomber that was designed and produced by the American aviation manufacturer Douglas Aircraft Company.

The B-66 was developed for the United States Air Force (USAF) and is heavily based upon the United States Navy’s A-3 Skywarrior, a heavy carrier-based attack aircraft. Originally, officials intended for the aircraft to be a simple development of the earlier A-3, taking advantage of being strictly land-based to dispense with unnecessary naval features. However, due to the USAF producing extensive and substantially divergent requirements, it became necessary to make considerable alterations to the design, leading to a substantial proportion of the B-66 being original rather than derived from the A-3. The B-66 retained the three-man crew arrangement of the US Navy’s A-3; differences included the incorporation of ejection seats, which the A-3 had lacked.

Performing its maiden flight on 28 June 1954, the aircraft was introduced to USAF service during 1956. The standard model, designated B-66, was a bomber model that was procured to replace the aging Douglas A-26 Invader; in parallel, a dedicated photo reconnaissance model, designated RB-66, was also produced alongside. Later on, further variants of the type were developed, leading to the aircraft’s use in signals intelligence, electronic countermeasures and weather reconnaissance roles. Aircraft would commonly be forward deployed to bases in Europe, where they could more easily approach the airspace of the Soviet Union. Multiple variants would be deployed around Cuba during the Cuban Missile Crisis. They would also see use during the American intervention in the Vietnam War, typically operating as support aircraft for other assets that were active over the skies of North Vietnam. The last examples of the type were withdrawn during 1975.

Background 2

Early on in the United States Navy’s A-3 Skywarrior’s development, several officials within the United States Air Force (USAF) had been skeptical of the design, some regarding its relatively low take-off weight of 68,000 lb as being impossible to achieve. In one instance, USAF general Hoyt Vandenberg ridiculed the proposed A-3 as making irresponsible claims. This hostile climate may be a result of the A-3 being intended to be operated from the planned United States-class supercarriers, to which numerous high-ranking officials within the USAF were frequently critical of and were campaigning for the latter’s cancellation, which eventually happened.

However, as the flight test program only validated its performance, it was recognized that the A-3 was capable of carrying out the same mission profile of the USAF’s much larger Boeing B-47 Stratojet over an unrefueled combat radius of almost 1,000 miles. Coupled with the development costs having already been paid by the Navy, the cost and performance of a land-based A-3 derivative was quite promising, especially in light of the USAF’s pressing needs from the Korean War. Accordingly, during the early 1950s, the service openly expressed interest in procuring its own version of the A-3 to perform land-based missions for the USAF.


USAF officials had originally intended the conversion to be a relatively straightforward matter of removing the carrier-specific features and fitting USAF avionics, but otherwise adhering as closely as possible to the original A-3 design. For this reason, no prototypes were ordered when the USAF issued its contract to Douglas in June 1952, instead having opted for five pre-production RB-66A models to be supplied, the aerial reconnaissance mission being considered to be a high priority for the type. However, this contract would be amended, involving multiple new variants that were added and swapped about. Likewise, the list of modifications sought quickly expanded; to meet the changing requirements, the supposedly easy conversion would become what was essentially an entirely new aircraft.

A percentage of the changes made were a result of the USAF’s requirement for the B-66 to perform low-level operations, the complete opposite of the US Navy’s A-3, which had been developed and operated as a high-altitude nuclear strike bomber. However, aviation authors Bill Gunston and Peter Gilchrist attribute many of the design changes to have been made merely to be different, being driven by an intense rivalry between the two services; they conclude that an objective assessment might conclude that 98 per cent of the changes introduced in the RB-66A were unnecessary. Both the fuselage and wing were entirely redesigned from scratch, rather than simply de-navalized. The A-3 was powered by a pair of Pratt & Whitney J57 turbojet engines, whereas the B-66 used two Allison J71 engines; Gunston and Gilchrist note that this engine swap "offered no apparent advantage", generating less thrust and being more fuel-hungry than the original J57 unit, which was also already in USAF use.

Due to the engine change, this necessitated a complete redesign of the power systems as well, repositioning all hydraulic pumps and generators onto the engines themselves instead of being fed with bleed air from within the fuselage. The pressurized crew compartment was given a different structure, adopting a very deep glazed front position for the pilot. The landing gear was also redesigned, even implementing a completely different door geometry. An impactful difference was the decision to equip the B-66 with ejection seats, a feature which the A-3 had lacked entirely. Aviation authors Bill Gunston and Peter Gilchrist observe of the B-66 that: The history of the aviation is sprinkled with aircraft which, to save money, were intended to be merely a modified version of an existing type. In very few cases it actually happened like this … the B-66 is a classic example.

Into Flight

On 28 June 1954, the first of the RB-66A pre-production aircraft conducted its maiden flight, development being only slightly behind schedule despite the substantial redesign work involved. The test program conducted with the five pre-production aircraft heavily contributed to improvements introduced upon the subsequent production aircraft. On 4 January 1955, the first production B-66B aircraft, which featured an increased gross weight and numerous other refinements, performed its first flight. Deliveries of the B-66B commenced on 16 March 1956. However, the USAF decided to curtail the bomber variant’s procurement, cancelling a further 69 B-66Bs and largely relegating the model for use in various test programs.

Once in service, the aircraft’s design proved to be relatively versatile. The principal production model was the RB-66B, which incorporated the bomber version’s upgrades. Furthermore, it was either produced or retrofitted into a variety of other versions, including the EB-66, RB-66, and the WB-66. Likewise, many variants of the US Navy’s A-3 Skywarrior were also produced.

Operational History 2

p align="justify"> During 1956, deliveries to the USAF commenced. A total of 145 RB-66Bs would be produced. In service, the RB-66 would function as the primary night photo-reconnaissance aircraft of the USAF during this period; accordingly, many examples served with tactical reconnaissance squadrons based overseas, typically being stationed in the United Kingdom and West Germany. A total of 72 of the B-66B bomber version were built, 69 fewer aircraft than had been originally planned. A total of 13 B-66B aircraft later were modified into EB-66B electronic countermeasures (ECM) aircraft, which played a forward role in the Cold War between the United States and the Soviet Union, and were stationed at RAF Chelveston with the 42nd Tactical Reconnaissance Squadron, who performed the conversion during the early 1960s. They would rotate out of an alert pad in Spain during the time that the 42nd had them.

These aircraft, along with the RB-66Cs that the 42nd received, would subsequently see combat service during the Vietnam War. Unlike the US Navy’s A-3 Skywarrior, which performed bombing missions in the theater, the Destroyer was never once used to perform bombing missions in Vietnam.

The RB-66C was a specialized electronic reconnaissance and electronic countermeasures (ECM) aircraft; according to Gunston and Gilchrist, it was the first aircraft designed from the onset for electronic intelligence (ELINT) missions. It was operated by an expanded crew of seven, which included the additional electronics warfare specialists. A total of 36 of these aircraft were constructed; the additional crew members were housed in the space that was used to accommodate the camera/bomb bay of other variants, these aircraft were outfitted with distinctive wingtip pods that accommodated various receiver antennas, which were also present upon a belly-mounted blister. Several RB-66Cs were operated in the vicinity of Cuba during the Cuban Missile Crisis, they would also be deployed over Vietnam. During 1966, these planes were re-designated as EB-66C.

Unarmed EB-66B, EB-66C and EB-66E aircraft flew numerous missions during the Vietnam War. They helped gather electronic intelligence about North Vietnamese defenses, and provided protection for bombing missions of the F-105s by jamming North Vietnamese radar systems. Early on, B-66s flew oval racetrack patterns over North Vietnam, but after one B-66 was shot down by a MiG, the vulnerable flights were ordered to fly just outside North Vietnamese air space.

On 10 March 1964, a 19th TRS RB-66C flying on a photo-reconnaissance mission from the Toul-Rosières Air Base in France, was shot down over East Germany by a Soviet MiG-21 after it had crossed over the border due to a compass malfunction. The crew ejected from the aircraft and, following a brief period of detention, were repatriated to the United States.

The final Douglas B-66 variant was the WB-66D weather reconnaissance aircraft; 36 were built.

By 1975, the last EB-66C/E aircraft had been withdrawn from USAF service. Most aircraft were scrapped in place, others were temporarily stored while awaiting eventual scrapping.

Variants 2

Operators 2

Douglas B-66 Specifications 3,4,5

Model ➜Douglas B-66BDouglas RB-66Douglas RB-66CNorthrop X-21
Manufacturer:Douglas Aircraft Company
Long Beach, CA
Northrop Aircraft Inc.
Hawthorne, CA
RB-66A and RB-66B:Pilot, navigator and gunner/camera operator.
B-66B:Pilot, navigator and gunner/bomb-aimer.
EB-66B and EB-66E:Pilot, navigator and electronic warfare officer.
RB/EB-66C:Pilot, navigator and 5 electronic warfare officers
WB-66D:Pilot, navigator, gunner and two equipment operator.
X-21:Pilot and four flight engineers.
Wing span:72 ft 6 in72 ft 6 in64 ft 7 in93 ft 6 in
Length:75 ft 2 in75 ft 2 in75 ft 2 in76 ft 3.5 in
Height:23 ft 7 in23 ft 7 in23 ft 7 in23 ft 7 in
Wing area:780 ft²780 ft²781 ft²1,250 ft²
Weights and Loadings
Empty weight:42,549 lb43,476 lb43,966 lb45, 828 lb
Loaded weight:57,800 lb59,550 lb64,085
Maximum weight:83,000 lb83,000 lb82,420 lb83,000 lb
Wing loading:74.1 psf73.6 psf82.1 psf
Power loading:2.8 lb/lb st2.9 lb/lb st3.1 lb/lb st
Maximum speed:631 mph at 6,000 ft631 mph at 6,000 ft640 mph at S/L560 mph
Cruising speed:528 mph525 mph532 mph
Rate of climb:5,000 fpm4,840 fpm5,000 fpm
Service ceiling:39,400 ft38,900 ft39,200 ft42,500 ft
Combat radius:900 miles925 miles1,440 miles
Maximum range:2,470 miles2,425 miles2,935 miles4,780 miles
Power Plant
Two Allison
J71-A-13 turbojets
10,200 lbf
Two General Electric
J79-GE-13 turbojets
9,400 lbf
Cannon:Two 20mm cannon in remotely-controlled tail turn (RB-66, B-66, WB-66).
Bomb load:15,00 lb in internal bomb bay.
Serial Numbers
RB-66B:53-409/481; 54-417/446; 54-506/547.
B-66B:53-482/507; 54-477/505; 54-548/551; 55-302/314.
RB-66B:54-447/476; 55-384/389.
X-21:55-408 and 55-410


  1. Shupek, John. The Skytamer Photo Archive, photos by John Shupek, copyright © 2001 Skytamer Images (
  2. Wikipedia, the free encyclopedia. Douglas B-66 Destroyer
  3. Francillon, René J. McDonald Douglas Aircraft Since 1920: volume I, London: Putnam Aeronautical Books, 1995, ISBN 0-85177-827-5, pg. 505.
  4. Swanborough, Gordon and Peter M. Bowers. United States Military Aircraft since 1908,, London: Putnam & Company Limited, 1971, ISBN 0-370-0009, pg. 269.
  5. Wikipedia, the free encyclopedia. Northrop X-21


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