Martin B-57

Bombers with Pakistan Air Force


  • Role: Tactical bomber
  • Manufacturer: Martin
  • First flight: 20 July 1953
  • Introduction: 1954
  • Retired: 1983 (USAF); 1985 (Pakistan)
  • Status: Retired (3 still used by NASA)

Primary users    

  • United States Air Force
  • Pakistan Air Force
  • Republic of China Air Force
  • Number built: 403
  • Unit cost: US$1.26 million (B-57B)
  • Developed from: English Electric Canberra
  • Variants: Martin RB-57D Canberra
  • Developed into: Martin/General Dynamics RB-57F Canberra

The Martin B-57 Canberra is an American-built, twinjet tactical bomber and reconnaissance aircraft that entered service with the United States Air Force (USAF) in 1953. The B-57 is a license-built version of the British English Electric Canberra manufactured by the Glenn L. Martin Company. Initial Martin-build models were highly similar to their British-built counterparts; Martin later modified the design to incorporate larger quantities of US-sourced components and produced the aircraft in several different variants.

The B-57 Canberra holds the distinction of being the first jet bomber in U.S. service to drop bombs during combat. The Canberra was used extensively during the Vietnam War in a bombing capacity; dedicated versions of the type were also produced and served as high-altitude aerial reconnaissance platforms (the Martin RB-57D Canberra), and as electronic warfare aircraft. The B-57 Canberra was also sold to export customers abroad, further combat use was seen by the Pakistani Air Force during the Second Kashmir War and the Indo-Pakistani War of 1971.

In 1983, the USAF opted to retire the type; the B-57 Canberra’s retirement marked the ending of the era of the tactical bomber that had its beginning with the British World War I De Havilland DH-4 bomber. The three remaining flight worthy WB-57Fs are technically assigned to the NASA Johnson Space Center, next to Ellington Field in Houston, as high-altitude scientific research aircraft,[2] but are also used for testing and communications in the U.S. and Afghanistan.

Development, Origins

At the outbreak of the Korean War in 1950, the USAF found itself in dire need of an all-weather interdiction aircraft. The existing inventory of piston-engined Douglas B-26 Invaders had been dispatched in this capacity at the very start of the conflict; however, within only a few months within the theatre, the B-26 had suffered a very high rate of attrition and successes with the type were typically limited. In response to these needs, the USAF requested the British government to provide a private demonstration of the English Electric Canberra, a newly developed jet-powered bomber. On 17 August 1950, the Canberra demonstration was performed at RAF Burtonwood, Warrington, Cheshire, England; during the following month, a team of US test pilots and engineers visited English Electric’s Warton factory to perform a series of flight tests and a detailed technical assessment of the aircraft.

On 16 September 1950, the USAF formally issued a request for a jet-powered bomber; the sought aircraft had to possess a top speed of 630 mph (1,020 km/h), ceiling of 40,000 feet (12,190 m), and range of 1,150 miles (1,850 km). Full all-weather capability and a secondary reconnaissance role also had to be included in the design. The American contenders included the Martin XB-51, the North American B-45 Tornado and AJ Savage. To expedite the process, only projects based on existing aircraft were considered and, unusually, the service considered foreign aircraft. These included the Canadian Avro Canada CF-100 and the British English Electric Canberra, which had not yet officially entered service with the Royal Air Force (RAF). Aviation authors Bill Gunston and Peter Gilchrist commented that “It seems likely that this first batch of trials convinced the Americans that the Canberra was ideal for the job, but in order to satisfy the US Senate a competitive evaluation of all likely contenders had to be arranged”.

As part of the USAF evaluation’s process, all five aircraft were submitted to a series of fly-offs to determine their performance. On 21 February 1951, a British Canberra B.2 (WD932), flown by Roland Beamont, made the transatlantic journey, arriving in the United States to participate in the competition; by making this journey, the Canberra thus became the first jet aircraft to perform a non-stop unrefueled flight across the Atlantic Ocean, travelling from Warton, England, to Gander, Newfoundland and Labrador, Canada, in the record time of 4 hours 37 minutes. On 26 February 1951, the flyoff took placed at Andrews Field, Prince George’s County, Maryland; each aircraft was tasked with performing a set sequence of maneuvers within a ten-minute window, directly demonstrating its agility and performance against its rivals. According to Gunston and Gilchrist, the Canberra proved to be significantly superior to any of the competing aircraft, and that its selection was beyond doubt by the end of the competition.

Production arrangements

That the Canberra was a foreign aircraft meant that its superiority in terms of performance did not guarantee political support, in spite of the urgent need, particularly in light of there being several rival indigenous aircraft designs; there were also doubts about production availability with English Electric being able to mesh with USAF demands, as well as questions over continued spares support. In March 1951, many of these questions were answered when, in part due to its production lines being sustained at full capacity to meet orders from the Royal Air Force in addition to those emerging from other export customers, English Electric entered into discussions with Glenn L. Martin Company, under which it was proposed that Martin would receive a license to domestically build the Canberra in the United States. According to Gunston and Gilchrist, the Americanization of the Canberra program proved effective at dismissing many of the political opponents that had opposed the project.



The British-built Canberra B.2 that was used as a pattern and prototype for the B-57

On 23 March 1951, the USAF issued a contract to Martin, requesting the manufacturing of an initial quantity of 250 Canberras, which had received the USAF designation B-57A (Martin internally designated the type as the Model 272). On 3 April 1951, English Electric and Martin both signed a formal licensing agreement to cover the Canberra’s production.

During August 1951, a second British-built Canberra (WD940) was flown to the US to act as a pattern aircraft for Martin, as well as to perform assorted trials and to support performance validation of airframe changes. On 21 December 1951, one of the British pattern aircraft (WD932) was lost in accident; although this was subsequently discovered to be caused by incorrect fuel scheduling having led to the tail-heavy aircraft exceeding its design limits during a maneuver, the crash jeopardized the entire program and invigorated the anti-Canberra political opposition. The crash did lead to some design changes in the face of political pressure, but these were not implemented on the first 75 aircraft to be produced.

Due to the great urgency placed on delivering the B-57A Canberra, the initial phase of manufacturing performed by Martin used a minimum-change formula to expedite production, thus the first B-57As to be produced were largely identical to the Canberra B.2. As such, more than 30 changes that had been requested by the Wright Air Development Center (WADC) were rejected on program schedule or cost grounds.[6] One noticeable exception was the adoption of more powerful Armstrong Siddeley Sapphire engines capable of producing 7,200 lbf (32 kN) of thrust, which were license-built in the United States as the Wright J65. The Sapphire-based J65 powerplant had been selected in place of the British-built Canberra’s Rolls-Royce Avons as the USAF had placed an emphasis on operations within hot climates and intended to fly at a slightly higher maximum gross weight than the RAF’s operating practices.

Several other minor differences were also present between early US-built and UK-built Canberras; these changes included the canopy and fuselage windows being slightly revised, the crew being reduced from three to two, the adoption of wingtip fuel tanks, engine nacelles were modified with additional cooling scoops, and the conventional “clamshell” bomb bay doors were replaced with a low-drag rotating door originally designed for the XB-51. As a result of these changes, the bomb bay of the US-built aircraft was slightly smaller than its UK-built counterparts in order to allow the American aircraft to carry more fuel; however, the overall external shape of the Canberra remained unchanged.

In early July 1953, the first US-built production aircraft (52-1418) rolled out; it conducted its maiden flight on 20 July 1953. One month later, this initial production aircraft was accepted by the USAF, by which point a cessation of hostilities had come into effect in Korea. This was one of only eight B-57A Canberras to be manufactured; the remaining 67 aircraft from this first batch, deemed no longer to be required as bombers, were converted on the assembly line to serve as medium-altitude reconnaissance aircraft while retaining all the basic Canberra features, and were accordingly re-designated as the RB-57A Canberra.

Further development


B57B Canberras of the 345th Bombardment Wing in flight, 1957


 In place of the curtailed B-57A, a more refined bomber variant, the B-57B, was developed. Having a more lengthy development time, this model incorporated the structural and system changes that had been recommended by WADC, which resulted in the aircraft being more adaptable than its B-57A predecessor. Of the external changes, the most significant was the adoption of a fighter-style canopy accompanied by a flat-panel windshield and a tandem seating arrangement, providing for greater transparency and an improved view for both the pilot and navigator, as well as allowing for a gunsight to be equipped, the corresponding glazed bombing nose of the B-57A was deleted along with the starboard crew entrance to the cockpit.

The B-57B introduced several other major changes. In terms of armaments, a total of four hardpoints attached to the outer wing panels were installed on this variant, capable of mounting external bombs and rockets; the B-57B was also furnished with a gun armament for strafing attacks, the first 90 aircraft to be produced were equipped with a total of eight 0.50 cal (12.7 mm) Browning machine guns installed within the wings, on later aircraft these were substituted for by an arrangement of four 20 mm M39 cannon.[10] A new rotary bomb door was adopted on the B-57B, which had originally been designed for the XB-51, replacing the hinged doors, this proved to be faster to open/close as well to reduce buffeting, which in turn improved accuracy and allowed for faster attack speeds. The redesigned bomb bay also enabled faster turnaround times on the ground.

In addition, hydraulically-operated triangular air brakes were installed on the rear fuselage, which worked in addition with the existing ‘finger’-type brakes installed in the wings; the new brakes gave the pilots a greater level of controllability, improving the accuracy of low-level bombing runs. The B-57B was equipped with an APW-11 Bombing Air Radar Guidance System for target approach guidance, as well as a APS-54 radar warning receiver. The engines were also furnished with a new cartridge starting system, eliminating the reliance on ground start carts.

The substantial design changes between the B-57A and B-57B models resulted in delays to the overall program, as well as incurring substantial costs on the fixed-price contract. Gunston and Gilchrist stated of the consequences to the program: “This was clearly not the manufacturer’s fault, but the money effectively ran out after 177 of the planned 250-aircraft order had been completed”. In 1954, in response to the sound performance offered by the B-57B, the USAF elected to place a large second order; this order included a further 100 B-57B bombers, 38 B-57C trainers, and 20 RB-57D high-altitude reconnaissance aircraft. In 1955, a final batch of 68 B-57E target tugs were ordered.

In 1969, in response to demands for a capable night interdiction aircraft for combat operations in the Vietnam theatre, a total of 16 B-57B Canberras were substantially rebuilt during a lengthy upgrade program. These aircraft received an entirely new nose section containing an AN/ANQ-139 forward-looking radar, a low-light television system, and an AN/AAS-26 forward-looking infrared detector. A laser rangefinder/designator was also installed, and the wing pylons modified to accommodate laser-guided Paveway bombs, while all the guns were removed to save weight. During the production run from 1953 to 1957, a total of 403 B-57s were built.

Operational history


EB-57A parked at Scott AFB, 1969.



B-57B, 71st Bombardment Squadron, Laon-Couvron Air Base, circa 1957



B-57E with nose graft from Bomarc, for testing of the missile


The B-57A was not considered combat-ready by the USAF and the aircraft were used solely for testing and development. One of the aircraft was given to the National Oceanic and Atmospheric Administration (NOAA) which fitted it with a new nose radome and used it to track hurricanes. The aircraft was placed into limited production. Particularly contentious were the cockpit arrangement and the lack of guns, the Canberra having been designed as a high-speed, high altitude bomber rather than for close air support. The definitive B-57B, which introduced numerous improvements, made its first flight on 18 June 1954. The aircraft initially suffered from the same engine malfunctions as the RB-57As and several were lost in high-speed low-level operations due to a faulty tailplane actuator which caused the aircraft to dive into the ground. The USAF came to consider the B-57B as being inadequate for the night intruder role and thus Martin put all aircraft through an extensive avionics upgrade in response. Regardless, by the end of 1957, the USAF tactical squadrons were being re-equipped with supersonic North American F-100 Super Sabres. The complete retirement was delayed, however, by the start of the Vietnam War.

Reconnaissance and electronic warfare B-57s

While the USAF found the B-57A lacking, the photo reconnaissance RB-57A saw some operational use. First flying in October 1953, RB-57As fully equipped the 363rd Tactical Reconnaissance Wing at Shaw Air Force Base by July 1954. The aircraft were also deployed with USAF squadrons in Germany, France, and Japan. However, operational readiness was poor and the aircraft suffered from significant production delays because of engine problems. Wright had subcontracted production of J65 engines to Buick, which resulted in slow deliveries and a tendency for engine oil to enter the bleed air system, filling the cockpit with smoke. The problems were ameliorated when Wright took over engine production in 1954. RB-57As also suffered from a high accident rate caused in part by poor single-engine handling. This resulted in the entire fleet spending much of 1955 on the ground. By 1958, all RB-57A craft were replaced in active service by the Douglas RB-66B and McDonnell RF-101A. Air National Guard units extensively used the RB-57A for photographic surveys of the United States until 1971.

A number of modified RB-57As were used by the 7499th Support Group at Wiesbaden AB, West Germany in Operation “Heart Throb” reconnaissance missions over Europe. Ten aircraft were pulled off Martin’s production line and modifications were performed in August 1955 by the Wright Air Development Center and by Martin. All equipment not absolutely essential for the daytime photography role was eliminated. The bomb bay door was removed and the area was skinned over. The seat for the system operator/navigator was removed, and an optical viewfinder was installed in the nose so that the pilot could perform all the reconnaissance duties without the assistance of the navigator. The clear plexiglass nose cone was replaced by an opaque fiberglass cone, but with a small optical glass window cut for the viewfinder. The plane’s J65-BW-5s were replaced by higher-thrust J65-W-7s. The aircraft was referred to as RB-57A-1. The weight reduction program shaved 5665 pounds off the weight of the RB-57A, and the ceiling was increased by 5000 feet.

Two RB-57A-1s were used by the Republic of China Air Force for reconnaissance missions over China; one was shot down by a Chinese Mikoyan-Gurevich MiG-17 on 18 February 1958 and the pilot killed. In 1959, two RB-57Ds were delivered to replace the A-types; one of them was shot down over China by a SA-2 Guideline missile, marking the very first successful operational engagement of surface-to-air missiles. Two other RB-57As were used by the Federal Aviation Administration to plan high-altitude airways for the upcoming jet passenger aircraft.

Starting in 1959, Martin began to modify retired RB-57As with electronic countermeasures (ECM) equipment in the bomb bay. Redesignated EB-57A, these aircraft were deployed with Defense Systems Evaluation Squadrons which played the role of aggressors to train the friendly air defense units in the art of electronic warfare. Subsequent bomber variants were also modified to fulfill this role. Although initially conducted by active duty Air Force units, the EB-57 mission eventually migrated to selected units of the Air National Guard. The ANG’s EB-57s were replaced, in the 1980s, by the USAF’s more advanced General Dynamics/Grumman EF-111A Raven operated by the active-duty USAF.

Strategic Air Command employed 20 RB-57D aircraft from 1956 until 1964. Little is known about their use. The aircraft were retired due to structural fatigue and the advent of the U-2 and SR-71.

For many years two WB-57F Canberras (NASA 926 and NASA 928) were flown and maintained by NASA for high altitude atmospheric research. These same two aircraft have also been deployed alternately to Afghanistan for use as communications platforms that fly high over an area linking various communications devices on the battlefield and to other airborne assets, they were known as the Battlefield Airborne Communications Node system (BACN). In 2011 it was determined that a third aircraft was needed to satisfy mission requirements and an additional WB-57 was removed from the 309th AMARG after over 40 years at Davis-Monthan AFB and returned to flight status in August 2013 as NASA 927.

Vietnam War

Patricia Lynn RB-57E at Da Nang, January 1964


Tropic Moon III B-57G with FLIR/LLLTV pod on the left nose

Although intended as a bomber and never before deployed by the USAF to a combat zone, the first B-57s to be deployed to South Vietnam were not operated in an offensive role. The need for additional reconnaissance assets, especially those capable of operating at night, led to the deployment of two RB-57E aircraft on 15 April 1963. Under project Patricia Lynn these aircraft provided infrared coverage using their Reconofax VI cameras. Later in August 1965, a single RB-57F would be deployed to Udon, RTAB in an attempt to gather information about North Vietnamese SAM sites, first under project Greek God and then under project Mad King. In December another RB-57F would be deployed for this purpose, under project Sky Wave. Neither project garnered useful results nor they were terminated in October 1965 and February 1966 respectively.

The deployment of actual combat capable B-57Bs from 8th and 13th Bomb Squadrons to Bien Hoa Air Base in August 1964 began with two aircraft lost and one damaged in collisions on arrival. An additional five aircraft were destroyed with another 15 damaged by a Viet Cong mortar attack in November of the same year. Low level sorties designated as training flights were conducted with the hope of it having a psychological effect. As a result, the first combat mission was only flown on 19 February 1965. The first excursion into North Vietnam took place on 2 March as part of Operation Rolling Thunder. The aircraft typically carried nine 500 lb (227 kg) bombs in the bomb bay and four 750 lb (340 kg) bombs under the wings. In April, Canberras began flying night intruder missions supported by USAF’s Fairchild C-123 Provider or Lockheed C-130 Hercules flare ships and USN’s EF-10B Skyknight electronic warfare aircraft.

U.S. B-57 Canberras were primarily used for dive bombing and strafing, with the early models mounting eight .50 caliber machine guns, four per wing. Later models mounted four 20mm cannons, two per wing, for strafing. These weapons combined with their bomb loads, and four hours of flight time made them excellent ground support aircraft, as well as exceptional truck killers along the Ho Chi Minh trail. Deployed along the notorious “trail” for much of their eight years in Vietnam, Canberras participated in truck hunting campaigns during operations Barrel Roll, Steel Tiger, and Tiger Hound, gaining reputations with their “Centurion Club” which consisted of Canberra crews which attained 100 truck kills.

On 16 May 1965, an armed B-57B exploded on the runway at Biên Hòa, setting off a chain reaction that destroyed 10 other Canberras, 11 Douglas A-1 Skyraiders, and one Vought F-8 Crusader. Due to combat attrition, in October 1966, B-57Bs were transferred to Phan Rang where they supported operations in the Iron Triangle along with Australian-built Canberra B.20s of No. 2 Squadron RAAF. The aircraft also continued to fly night interdiction missions against the Ho Chi Minh trail. Of the 94 B-57Bs deployed to Southeast Asia, 51 were lost in combat and seven other Canberras were lost to other causes. Only nine were still flying by 1969.

B-57s returned to Southeast Asia in the form of the Tropic Moon III B-57G, deployed to Thailand during the fall of 1970. Intended as a night intruder to help combat movement along the Ho Chi Minh trail, these aircraft were equipped with a variety of new sensors and other equipment, and were capable of dropping laser guided munitions. The relative kill rates per sortie during Operation Commando Hunt V between the B-57G and the AC-130A/E showed that the former was not as suited to the role of trucker hunter. An attempt to combine both led to one B-57G being modified to house a special bomb bay installation of one Emerson TAT-161 turret with a single M61 20mm cannon as a gunship under project Pave Gat. After delays in testing at Eglin AFB, Florida, due to competition for mission time from the Tropic Moon III B-57Gs, Pave Gat tests proved “that the B-57G could hit stationary or moving targets with its 20mm gun, day or night. Loaded with 4,000 rounds of ammunition, the Pave Gat B-57G could hit as many as 20 targets, three times as many as the bomb-carrying B-57G. The Pave Gat aircraft could avoid antiaircraft fire by firing from offset positions, while the bomb carrier had to pass directly over the target.” Deployment to SEA was resisted, however, by the Seventh and Thirteenth Air Forces and others as the decision had been made in August 1971 to return the B-57G squadron to the U.S. in early 1972, leaving insufficient evaluation time. Project Pave Gat was terminated 21 December 1971.The B-57G was removed from Thailand in May 1972. Plans remained for the continuation of the B-57G program but post-conflict spending cuts forced the abandonment of these plans.

 Operation Shed Light

For a short period South Vietnamese Air Force personnel operated four B-57B aircraft. The VNAF never officially took control of the aircraft, and, after accidents and other problems, including apparent claims by VNAF pilots that the B-57 was beyond their physical capabilities, the program was terminated in April 1966, and the aircraft were returned to their original USAF units.

A total of 58 B-57 Canberras were recorded as having been lost during the Vietnam War; of these, 26 were lost to ground fire, 5 were lost to mortar fire and ground attack, 4 were lost to mid-air collision, 10 were lost to airfield accidental bomb explosion, 7 were lost to operational causes, and 6 were lost due to unknown causes. These figures include two B-57E Canberras from the 1st Det 33rd Tactical Group.




PAF B-57s

The Pakistan Air Force was one of the main users of the B-57 and made use of it in two wars with India. In the Second Kashmir War of 1965, B-57s flew 167 sorties, dropping over 600 tons of bombs. Three B-57s were lost in action, along with one RB-57F electronic intelligence aircraft. However, only one of those three was lost as a result of enemy action. During the war, the bomber wing of the PAF was attacking the concentration of airfields in north India. In order to avoid enemy fighter-bombers, the B-57s operated from several different airbases, taking off and returning to different bases to avoid being attacked. The B-57 bombers would arrive over their targets in a stream at intervals of about 15 minutes, which led to achieving a major disruption of the overall IAF effort. PAF’s B-57 Squadron was the first to form a regular formation aerobatics team of four such aircraft. The unknown Pakistani flying ace, 8-Pass Charlie, was named by his adversaries for making eight passes in the moonlight, to bomb different targets with each of the B-57’s bombs.

During the Indo-Pakistani War of 1971, the PAF again made use of the B-57. On the very first night, 12 IAF runways were targeted and a total of 183 bombs were dropped rendering the Indian airfields useless for 6 hours to 6 days. As the war progressed, PAF B-57s carried out many night missions. There was a higher attrition rate than in 1965, with at least five B-57s being put out of service by the end of the war. They were retired from PAF service in 1985.




USAF B-57 dropping 750 lb (340 kg) bombs



WB-57F flies over the Gulf of Mexico near its base at NASA JSC.

  • B-57A-First production version; eight built.
  • B-57B-Definitive production version, tandem cockpit, 8x 0.50 in (12.7 mm) machine guns or 4x 20 mm cannons, four underwing hardpoints; 202 built.
  • B-57C-Dual-control trainer, first flight: 30 December 1954; 38 built.
  • B-57E-Target tug, first flight: 16 May 1956; 68 built.
  • B-57G-B-57Bs modified as night intruders with FLIR, LLTV and laser designator in the nose, capable of using laser-guided bombs; 16 converted.
  • EB-57A-Electronic aggressor aircraft converted from RB-57As.
  • EB-57B-ECM aircraft converted from B-57Bs.
  • EB-57D-ECM aircraft converted from RB-57Ds.
  • EB-57E-Electronic aggressor aircraft converted from RB-57Es.
  • RB-57A-Photo reconnaissance version with cameras installed aft of the bomb bay; 67 built. RB-57A avionics included an AN/APS-11A transponder and AN/APA-90 Indicator Group for command guidance (LEFT, RIGHT, CLIMB, DESCEND, BOMB, etc.) and was tested[where?] for “MSQ-1 controlled pinpoint photography” in 1954 (“Night Photo Bombing” capacity was 21 M-120 Photoflash Bombs).
  • RB-57B- Photo-reconnaissance aircraft converted from B-57Bs.
  • Martin RB-57D Canberra- High-altitude strategic reconnaissance version, J57-P-9 engines, wingspan increased to 106 ft (32.31 m), first flight: 3 November 1955; 20 built.
  • B-57Es modified to all-weather reconnaissance aircraft, used in “Patricia Lynn” missions during the Vietnam War; six converted.
  • Martin RB-57F Canberra-High-altitude strategic reconnaissance version developed by General Dynamics. Pratt & Whitney TF33 turbofan engines, wingspan increased to 122 ft (37.5 m), first flight 23 June 1963; 21 built.
  • WB-57D-Air Weather Service RB-57Ds used for nuclear atmospheric sampling testing.
  • WB-57F-Air Weather Service RB-57Fs re-designation after June, 1968


  • Pakistan Air Force: No. 31 Bomber Wing; No. 7 Squadron Bandits; No. 8 Squadron Haiders
  • Republic of China Air Force
  • United States Air Force



B/C model, 3-view Data from Quest for Performance, Jet Bombers


Specifications (B-57B)


General characteristics

  • Crew: 2 (pilot, navigator)
  • Length: 65 ft, 6 in (20.0 m)
  • Wingspan: 64 ft 0 in (19.5 m)
  • Height: 14 ft 10 in (4.52 m)
  • Wing area: 960 ft² (89 m²)
  • Empty weight: 27,090 lb (12,285 kg)
  • Loaded weight: 40,345 lb (18,300 kg)
  • Max. takeoff weight: 53,720 lb (24,365 kg)
  • Powerplant: 2 × Wright J65-W-5 turbojets, 7,220 lbf (32.1 kN) each
  • *Zero-lift drag coefficient: 0.0119
  • Drag area: 11.45 ft² (1.06 m²)
  • Aspect ratio: 4.27


  • Maximum speed: Mach 0.79 (598 mph, 960 km/h) at 2,500 ft (760 m)
  • Cruise speed: 476 mph (414 knots, 765 km/h)
  • Stall speed: 124 mph (108 knots, 200 km/h)
  • Combat radius: 950 mi (825 nm, 1,530 km) with 5,250 lb (2,380 kg) of bombs
  • Ferry range: 2,720 mi (2,360 nm, 4,380 km)
  • Service ceiling: 45,100 ft (13,745 m)
  • Rate of climb: 6,180 ft/min (31.4 m/s)
  • Wing loading: 42 lb/ft²  (205 kg/m²)
  • Thrust/weight: 0.36
  • Lift-to-drag ratio: 15.0


  • Guns: 4× 20 mm (0.787 in) M39 cannon, 290 rounds/gun


  • 4,500 lb (2,000 kg) in bomb bay, including nuclear bombs
  • 2,800 lb (1,300 kg) on four external hardpoints, including unguided rockets


  • APW-11 Bombing Air Radar Guidance System
  • SHORAN bombing system
  • APS-54 Radar Warning Receiver

Related development

  • English Electric Canberra
  • Martin RB-57D Canberra
  • Martin/General Dynamics RB-57F Canberra

Aircraft of comparable role, configuration and era

  • Avro CF-100
  • Ilyushin Il-28
  • Martin XB-51
  • North American AJ Savage
  • North American B-45 Tornado

Courtesy of





2 thoughts on “Martin B-57

Leave a Reply

Fill in your details below or click an icon to log in: Logo

You are commenting using your account. Log Out /  Change )

Facebook photo

You are commenting using your Facebook account. Log Out /  Change )

Connecting to %s

This site uses Akismet to reduce spam. Learn how your comment data is processed.