
A 1939 tandem 2-seat low-wing trainer. Two prototypes of wooden construction were finally completed in 1948.
Engines: 2 x 220 hp Renault 6Q10/11
Wingspan: 13.5m

A 1939 tandem 2-seat low-wing trainer. Two prototypes of wooden construction were finally completed in 1948.
Engines: 2 x 220 hp Renault 6Q10/11
Wingspan: 13.5m

A piloted, three-eighths scale model of PBM flying boat; single-seat test aircraft built to generate aerodynamic data to design and build full-scale Martin PBM flying boat.
The construction was fabric-covered spruce plywood and aluminum.
In 1987, a dedicated and enthusiastic team of volunteers, many of whom were former Martin employees, began an exhaustive restoration of the 162A. After more than 10,000 man-hours of labor, the 162 was ready for display while on loan to the Museum of Industry in Baltimore, not far from where the “Tadpole Clipper” had been built and flown. Portions of the rear fuselage under-surface were left uncovered to illustrate some of the modifications made in the 162A’s hull during the course of its testing.
Wingspan: 43ft 5 5/8in / 13.25m
Length: 28ft 6 1/8in / 8.69m
Height: 12ft 1/8in / 3.66m
Weight: 2819.7 lb / 1279 kg

The beginning of the Korean conflict on 25 June 1950 and the shortcomings of the Douglas B-26 / A-26, accounted for the urgent procurement of a light tactical bomber.
The new bomber had to be capable of operating from unimproved airfields, at night and in every kind of weather, with conventional or atomic weapons. High altitude reconnaissance was another must. For such purposes, the B-45 was too heavy; the Navy AJ-1, too slow; and the Martin experimental B-51’s range too short.
As a result of the outbreak in Korea, the Air Force reached a final decision. The desire for a night intruder was so strong that it took just a few days to set in motion the informal production endorsement of February 1951. Because of its experience with the XB-51, the Glenn L. Martin Company was recognized as the most qualified contractor to assume the domestic production of the British aircraft and to deal with the likely engineering difficulties involved in manufacturing a high-performance tactical bomber.
The new bomber became the Martin B-57, a by-product of the English Electric Canberra, the first British-built jet bomber, initially flown in 1949. Adaptation of a foreign-made aircraft to American mass production methods, as well as the use of different materials and tools, could present many difficulties. Another problem, perhaps more critical, centered on the Wright J65 turbojets, due to replace the Canberra’s two Rolls Royce Avon turbojet engines. The J65 was the U.S. version of the Sapphire, a British hand-tooled production currently scheduled for manufacturing by the U.S. Curtiss-Wright Corporation. The Air Force was fully aware of these potential pitfalls, but had no better option. It had an immediate requirement for a light jet bomber, with a 40,000-foot service ceiling, a 1,000-nautical mile range, and a maximum speed of 550 knots.
Testing of two imported Canberras revealed design faults that could affect the safety, utility, and maintenance of the future B-57. Then, one of the British planes crashed; Martin’s subcontractors could not meet their commitments; and the J65 prototype engines consistently failed to satisfy USAF requirements. In June 1952, further test flights had to be postponed for a year because of continuing engine and cockpit troubles. As a result, the Korea-bound B-57 did not fly before 20 July 1953, just 7 days before the conflict ended. Production of the crucial RB-57 was also delayed. The reconnaissance version entered service in mid-1954, after testing again confirmed that the more powerful J65 engines, added equipment, and other improvements had increased the aircraft’s weight, in turn reducing the speed, distance, and altitude of both the B-57 and the RB-57.
The program was reduced, but there was no talk of cancellation. In 1955, the B/RB-57s justified their costs when they served overseas pending the B/RB-66 deliveries which, as predicted, had fallen behind schedule. The first Martin B‑57A (the name Canberra was retained, though Night Intruder was also used) flew on 20 July 1953. In 1956, much-needed RB-57Ds joined the Strategic Air Command, and various configurations of this model satisfied important special purposes.

The main model (202 built) was the B 57B with a redesigned forward fuselage with a crew of only two seated in tandem under a giant rear hinged canopy. This attack version introduced a heavier bombload in a rotary door weapon bay, plus eight pylons under the outer wings and forward firing guns. The B 57B equipped two wings in Tactical Air Command and a wing of PACAF (Pacific Air Forces) but had mainly been passed to Air National Guard units by the early 1960s. Vietnam requirements then demanded aircraft in this class and all available B 57Bs (many had been re built into other models) were rushed to South Vietnam and used very success¬fully in the attack role and in particular as FAC (Forward Air Control) aircraft.

Delivered too late for combat in Korea, the RB-57 in May 1963 and the B-57 in February 1965 began to demonstrate under fire in Southeast Asia the basic qualities justifying the Canberra’s original selection.
RB-57 Reconnaissance Canberra Article
The original B-57A differed little externally from the English Canberra B2. The RB-57A was similar, with reconnaissance equipment.
The B-57B, with eight 0.50 in or four 20mm guns in the wings, bombs in an internal bomb bay, and underwing racks, served with the Chinese Nationalist and Pakistani air forces.
Variants include the RB-57D(A) and (B) with cameras, the RB-57D(C) and (D) electronics reconnaissance aircraft with radomes at the nose and tail and under the fuselage, and the RB-57(C) with wingtip radomes.
In 1970, other reactivated and newly equipped B-57s, known as Tropic Moon III B-57Gs, were deployed to Southeast Asia, where they made valuable contributions until April 1972. A total of 16 B 57Bs was rebuilt as B-57G (Tropic Moon) all weather and night attack aircraft with APQ 139 radar, a FLIR (forward looking infra-red), low light TV and laser ranger. The most capable aircraft of its day, the B 57G remained a mere study programme despite brilliant combat results.

The last new-built version was the B 57E multi role attack/bomber and target tug, all 68 of which were later modified for other tasks.

Finally, WB-57Fs, either modified RB-57Fs or former B-57Bs, were still flying high-altitude radiation sampling missions in 1973. Concurrently, EB-57Es, and related adaptations of the versatile B-57, continued to play significant roles, with no immediate phaseout in sight.

403 were built under licence by Martin (in six variants) as the B-57 and served with the US Air Force from August 1953 until 1982 in various marks and guises. At a later date a number of these were converted by General Dynamics to serve as ultra high-altitude strategic reconnaissance aircraft. These were provided with a wing span of 37.19m, two 80kN Pratt & Whitney TF33-P-11 turbofan engines (replacing the conventional power plant), plus two 14.68kN Pratt & Whitney J60-P-9 turbojets in underwing pods, and many equipment and avionics changes to fit them for their specialised role. The B-57 saw combat over Vietnam beside other Canberras from Australia.
The USAF bought 21 WB-57F aircraft, which were built by General Dynamics from existing B-57Bs and RB-57Ds. The airplanes’ ability to reach altitudes over 65,000 feet, carry payloads in excess of 4,000 lbs, and its triple spar wings made it a very capable high-altitude platform. Missions included everything from weather reconnaissance for Apollo space launches to sampling radiation in nuclear weapon test plumes.
In the late 1960s and early 1970s the Air Force decided to ground the WB-57F and depend exclusively on the U-2 for high-altitude support. The mission of monitoring nuclear test bans was better done by the WB-57F than the U-2, however. That mission was important enough that three aircraft were given to NASA to keep that capability alive, which were designated N925N, N926NA, and N928NA.
When N925N was retired and put on display at Pima Air & Space Museum in Tucson, Arizona, it that left NASA with two WB-57Fs. Another airframe joined the fleet in 2011 after been taken out of the 309th Aerospace Maintenance and Regeneration Group, (AMARG), better known as the “Bone Yard,” at Davis-Monthan Air Force Base, Arizona. The aircraft, designated N927NA, began as a B-57B, and then was one of 21 aircraft rebuilt as an RB-57F in 1964. As an RB-57F the aircraft had its wingspan increased to 122 feet and the original Wright J65 turbojets were replaced by Pratt & Whitney TF-33 turbofans, doubling both the wingspan and thrust.
N927 had been retired in June 1972 and remained on “celebrity row” at the Bone Yard until May 2011 when it was dismantled and trucked to Sierra Nevada Corporation at Centennial Airport, Colorado. After being refurbished to flying condition it was flown to Ellington AFB in August 2013.
The aircraft had been in storage for over 40 years and made its first flight in 41 years in the summer of 2013, setting a record for the longest an aircraft had sat in the Bone Yard before returning to flying status.

Based at Ellington Field near NASA’s Johnson Space Center in Houston, Texas, the WB-57F operates in NASA’s High Altitude Research Program. The aircraft provides unique, high-altitude (up to 70,000 feet MSL) airborne platforms to United States government agencies and other customers for scientific research, advanced technology development, and testing around the world.
Since 2000, the unique performance capabilities of the WB-57F aircraft and increasing costs associated with the ER-2 program have resulted in NASA allowing multiple customers to use the WB-57Fs for atmospheric and satellite sensor research. The DOD programs have gotten much broader, and N928 (and sometimes N926) have multiple customers asking us to help them develop satellite sensors.

Both aircraft were enjoying multiple customers. By June 2014, both aircraft were upgraded with global positioning satellite navigation systems, F-15 main landing gear and brakes, and the gross weight capability of both aircraft was certified from 63,000 pounds to 72,000 pounds. Ongoing upgrades to the aircraft include installation of the ACES II ejection seat system and installation of an improved, modern autopilot.
B-57B
Night intruder bomber
Engines: 2 x Wright J65-W-3 Sapphire turbojets, 7,500lb thrust
Wingspan: 64 ft
Length: 65 ft. 6 in
Loaded weight: 46,000 lb.
Max speed: over 600 m.p.h.
Ceiling: over 45,000 ft.
Max range: 3,000 miles.
Armament: 8x.50 in. machine-guns
Bombload: 6,000 lb; 8×5-in. rockets
Hardpoints: 4
Crew: 2
B 57B
Engines: two 3,275 kg (7,220 lb) thrust Wright J65 W 5 turbojets.
Maximum speed 937 km/h (582 mph) at 12190 m (40,000 ft).
Service ceiling 14630 m (48,000 ft).
Range 3700 km (2,300 miles).
Weights: empty 11793 kg (26,000 lb)
Maximum take off 24948 kg (55,000 lb)
Wing span 19.51 m (64 ft 0 in)
Length 19.96 m (65 ft 6 in)
Height: 4.75 m (15 ft 7 in)
Wing area: 89.18 m (960 sq ft).
Armament: eight 12.7 mm (0, 5 in) or four 20 mm guns; up to 2722 kg (6,000 lb), 16 underwing rockets or mixed rocket/ bomb/napalm loads.
RB-57D
Engines: 2 x Pratt & Whitney J57C, 11,000 lb
Wingspan: 106 ft
Length: 65 ft 6 in
Height: 14 ft 10 in
Max speed: 632 mph at 40,000 ft
Service ceiling: 60,000 ft
RB 57F
Engines: 2 x Pratt & Whitney TF33 P 11 turbofan, 18,000 lb (8,165 kg) st, and 2 x P&W J60 P 9 auxiliary turbojets, 3,300 lb (1,500 kg) st.
Wing span: 122 ft 5 in (37.32 m)
Length: 69 ft 0 in (21.03 m).
Height: 5.8 m / 19 ft 0 in
Max take-off weight: 20360 kg / 44886 lb
Empty weight: 13600 kg / 29983 lb
Max. speed: 880 km/h / 547 mph
Ceiling: 25000 m / 82000 ft
Range w/max.fuel: 6440 km / 4002 miles
Typical endurance: Over 10 hr
Crew: 2
Armament: None




The prototype of an improved Martin 3-0-3 had been flown on 20 June 1947, but with it was decided instead to develop a new Martin 4-0-4. This incorporated the wing structural revisions and introduced a pressurised and slightly lengthened fuselage, accommodating as standard a crew of three or four and 40 passengers.
The airliner was unveiled in 1949 and immediately ordered by a variety of air carriers, gaining 101 orders from TWA and Eastern. The subsequent 4-0-4 was introduced in 1950 with a fuselage 39 inches longer, slightly more powerful engines than the 202, and pressurization.
The onset of the Korean War suddenly made airplane materials significantly more expensive, and Martin found itself filling orders at a loss and stopped production.
Two or these 40-passenger transports were in service with the U.S. Coast Guard in 1955 as the RM-1, similar to the civil Martin 4-0-4 airliner.

A total of 148 of the 2-0-2, 3-0-3, and 4-0-4 types were built until 1952. Examples served well into the 1980s with commuter airlines.
RM-1
Engines: two 2,400 h.p. Pratt & Whitney R2800-34W
Span: 93 ft. 3 in.
Weight: 44,900 lb.
Max. Speed: 312 m.p.h.
4-0-4
Engines: 2 x 2400hp Pratt Whitney R-2800 CB-16
Max take-off weight: 20366 kg / 44900 lb
Empty weight: 13211 kg / 29125 lb
Wingspan: 28.42 m / 93 ft 3 in
Length: 22.73 m / 74 ft 7 in
Height: 8.66 m / 28 ft 5 in
Wing area: 80.27 sq.m / 864.02 sq ft
Cruise speed: 502 km/h / 312 mph
Ceiling: 8840 m / 29000 ft
Range: 3058 km / 1900 miles
Seats: 52


Along with the unpressurized Model 202, Martin offered a companion pressurized model, known as the Model 303. United Air Lines was the primary sponsor of the 303, having invested one million dollars of its own money in the development. In addition to the 50 slated for delivery to United, Martin also had orders from Northwest Airlines, Braniff Airways, and Pan American-Grace Airways (PANAGRA) for 59 more.
Apart from cabin pressurization, the 303 differed from the 202 in that the wing span was shortened by about 4ft (1.2m) in an attempt to gain cruise performance at the expense of takeoff and climb performance. The 303 made its first flight on July 3, 1947; however, United canceled its large order a short time later.
Because of prevailing market conditions and serious stability problems encountered with the 202 and a need to redesign the wing structure, Martin dropped the 303 program the following December with a reported loss of more than $15 million. The prototype and almost all records were then scrapped for tax purposes.
A total of 148 of the 2-0-2, 3-0-3, and 4-0-4 types were built until 1952.

Attempting to gain a share of the post-World War II demand for civil airliners, the Glenn L. Martin Company flew on 22 November 1946 the prototype of a twin-engine 36/40-seat unpressurised transport designated Martin 2-0-2.
Power was provided by twin Pratt & Whitney 18-cylinder air cooled radial engines capable of developing a normal output of 1,800 hp, 2,100 hp for takeoff or 2,400 hp with water injection. The engines turned Hamilton Standard three-blade reversible-pitch airscrews.
The “Two- O-Two” was the first twin-engine airliner of postwar design to receive certification for airline use. Accommodations provided for a crew of three or four plus 36 to 40 passengers. A version of the 202 was outfitted with larger fuel tanks to increase its range to 2,365.
The first of these entered service in October 1947, but the loss of a 2-0-2 in 1948 as a result of wing structural failure led to modification of other in-service aircraft and production of this version was brought to an end.
When production ended in early 1953 a total of 103 had been built, this number including two supplied to the Coast Guard as staff transports under the designation RM-1G (later RM-1Z and finally VC-3A); they were subsequently transferred to the US Navy.
A total of 148 of the 2-0-2, 3-0-3, and 4-0-4 types were built until 1952.
Martin 202
Engines two 2,100-hp Pratt & Whitney R-2800 CB-16.
Wingspan: 28.42 m / 93 ft 3 in
Length: 21.74 m / 71 ft 4 in
Height: 8.66 m / 28 ft 5 in
Wing area: 80.27 sq.m / 864.02 sq ft
MTOW 19504 kg / 42999 lb
Empty wt. 26,930 lb
Top speed 311 mph.
Cruise 286 mph.
Stall 76 mph.
Initial climb rate 2,200 fpm
Range 3220 km / 2001 miles
Ceiling 33,000 ft
Takeoff distance (50′) 1,565 ft
Landing distance (50′) 1,720 ft
Seats 40.


The US Navy made several attempts to gain the benefit of high over-target performance combined with long range by introducing mixed powerplant. The Martin Model 219 patrol bomber represented one of the results of such a specification, two XP4M-1 prototypes being ordered on 6 July 1944. The first was flown on 20 September 1946 as a cantilever shoulder-wing monoplane with retractable tricycle landing gear. Its powerplant comprised two 2218kW Pratt & Whitney R-4360-4 Wasp Major radial engines, but each nacelle also incorporated a 17,350kg thrust Allison J33-A-17 turbojet. After a protracted development programme 19 P4M-1 production aircraft were built, the first being delivered to US Navy Squadron VP-21 on 28 June 1950, and all served with this unit. Most of them were converted into P4M-1Q Elint aircraft, one being shot down.

P4M-1
Engines: 2 x Pratt Whitney R-4360-20A piston engines, 2424kW + 2 x Allison J33-A-10A, 2087kg
Max take-off weight: 40000 kg / 88185 lb
Wingspan: 34.75 m / 114 ft 0 in
Length: 25.50 m / 83 ft 8 in
Height: 7.95 m / 26 ft 1 in
Wing area: 121.79 sq.m / 1310.94 sq ft
Max. speed: 660 km/h / 410 mph
Ceiling: 10545 m / 34600 ft
Range: 4570 km / 2840 miles
Armament: 2 x 20mm cannons, 4 x 12.7mm machine-guns, 2700kg of bombs

As a new US Navy patrol flying-boat, Martin developed the Model 237 design, combining the wing and upper hull of the Mariner with the new lower hull structure. A PBM-5 Mariner served as the prototype XP5M-1 which, when ordered into production, was given the name Marlin.
The modified hull of the XP5M-1 incorporated radar-directed nose and tail turrets, as well as a power-operated dorsal turret, and power was provided by two 2424kW Wright R-3350 radial engines.
This prototype flew for the first time on 30 May 1948, but it was not until two years later that the P5M-1 was ordered into production, the first of these series aircraft being flown on 22 June 1951.
Initial deliveries, to US Navy Squadron VP-44, began on 23 April 1952 and the type remained in service until the mid-1960s.

In addition to those operated by the US Navy, 12 of the later P5M-2 version were supplied to France under the American MAP for use by the Aeronavale in 1959. In the French Aeronavale, where they were used for maritime patrol out of Dakar, West Africa, until 1964, after which they were returned to the Navy. The P5M 2 Marlin could carry up to 8,000 lb (3,629 kg) of assorted weapons. The P5M-1 has a low mounted ” dihedral ” tailplane, different hull shape and lower-powered engines, compared to the P5M-2.
The first of 28 P5M-2 Marlins to undertake a modernisation program was delivered to the US Navy in 1959.
Martin aircraft production ceased December 20,1960 when the last P5M- 2 Marlin was handed over to U.S. Navy.

Claiming high operational costs, the Coast Guard turned over all of its P5Ms to the Navy in 1961. Lacking most military equipment, they were used as crew trainers as P5M-1T and P5M-2Ts.
In September 1962, when all American military forces adopted the tri-service designation scheme, the P5M-1 became the P-5A, the P5M-1S the SP-5A, the P5M-1T the TP-5A, the P5M-2 the P-5B, the P5M-2S and P5M-2T the PT-2B.

In 1964, in an attempt to boost take-off power, one SP-3B was tested with a tail mounted 3000 lb.st Pratt & Whitney J60 turbojet engine. They were not adopted for service.
No Marlins went to the reserves. As they were retired, they were stored until sold as scrap. A Navy SP-5B of VP-40 made the last operational flight on 6 November 1967.

The XP5M-1 prototype was later used (as the model 270) to test the 15:1 hull configuration for the P4M SeaMaster.
P5M
Engines: 2 x Wright R-3350-32WA Turbo-Compound, 2573kW
Max take-off weight: 38555 kg / 85000 lb
Empty weight: 22900 kg / 50486 lb
Wingspan: 36.02 m / 118 ft 2 in
Length: 30.66 m / 100 ft 7 in
Wing area: 130.62 sq.m / 1405.98 sq ft
Max. speed: 404 km/h / 251 mph
Ceiling: 7300 m / 23950 ft
Range: 3300 km / 2051 miles
Armament: 3600kg of weapons
Crew: 11
P5M-2 Marlin
Naval patrol bomber flying boat
Engines: 2 x Wright R3350-32W Turbo-Cyclone, 3450 h.p
Wingspan: 118 ft. 2in (36.02 m)
Wing area: 1406.3 sq.ft
Length: 100 ft. 7in (30.66 m)
Height: 32 ft 8.5 in (9.97 m)
Empty weight: 50,485 lb
Max TO wt: 85,000 lb (38,555 kg).
Loaded weight: 73,055 lb
MTOW: 76,635 lb
Fuel capacity: 4410 gal
Max speed: 251 mph at SL
Ceiling: 22,400 ft
Normal range: 2050 mi
Max range: 3,600 miles
Armament: 2 x 20mm tail mounted guns
Bombload: 16,000 lb
Crew: 7


The XPBM-1 prototype flying-boat patrol bomber was originally ordered by the US Navy in 1936. Before it was built, a quarter-size prototype (Model 162A) was constructed and flown. The full-size aircraft was flown for the first time in February 1939.
The production PBM-1 – fitted with two 1,192 kW Wright R-2600-6 radial engines, a dihedral tail and retractable wingtip floats – was ordered in 1938 and 20 of these went into Navy service in 1941. A single XPBM-2 was ordered at the same time as a long-range version specially strengthened for catapult take-off.
The PBM-3, with two 1,267kW Wright R-2600-12 engines, was ordered in quantity in 1940 and deliveries began in 1942. In this version the crew was increased from seven to nine, the armament was revised and the fuel capacity increased. The retractable wingtip floats of the PBM-1 were replaced by fixed floats. In 1942 the PBM-3 was adopted also as a naval transport carrying 20 passengers or 3,629-4,082kg of cargo (PBM-3R). Twenty-six PBM-3B patrol bombers were also used by RAF Coastal Command, delivered under Lend-Lease. At the end of the war a specialised anti-submarine version was also developed as the PBM-3S.

The final two production versions of the Mariner were the PBM-5 and PBM-5A, powered by 1,565kW R-2800-22 and R-2800-34 engines respectively. The last PBM-5A was delivered to the US Navy in April 1949. This version was basically an amphibious version of the PBM-5 and ended its career as a general utility aircraft.

630 PBM-5 flying boats were built, followed by 36 PBM-5A amphibians, used for air-sea rescue duties, primarily by the U.S.C.G.
In 1963 the US Navy tested vertical floats designed by General Dynamics/Convair, on a PBM-5.

These made the seaplane a stable working platform for anti-submarine warfare with little motion from 4-5 ft waves.


Engines: 2 x Wright R-2800A-5B, 1250kW
Max take-off weight: 25400 kg / 55998 lb
Empty weight: 14660 kg / 32320 lb
Wingspan: 36.0 m / 118 ft 1 in
Length: 34.4 m / 112 ft 10 in
Height: 8.4 m / 27 ft 7 in
Wing area: 130.0 sq.m / 1399.31 sq ft
Max. speed: 325 km/h / 202 mph
Cruise speed: 240 km/h / 149 mph
Ceiling: 6150 m / 20200 ft
Armament: 8 x 12.7mm machine-guns, 2000kg of bombs
Crew: 7
PBM-5A Mariner
Air-sea rescue amphibian
Engines: 2 x Pratt & Whitney R2800-34, 2,100 h.p.
Wingspan: 118ft
Length: 79ft. 10in
Loaded weight: 60,300 lb
Max speed: over 200 m.p.h.
Ceiling: 20,200 ft.
Max range: 2,900 miles at 143 m.p.h.
Armament: (when fitted) 8x.50 in machine-guns
Bombload: 4,000 lb
Martin PBM 3 D Mariner
Engines: 2 x Wright R-2600-22 Cyclone, 1874 hp
Length: 79.823 ft / 24.33 m
Height: 27.493 ft / 8.38 m
Wingspan: 118.012 ft / 35.97 m
Wing area: 1407.931 sq.ft / 130.8 sq.m
Max take off weight: 58009.1 lb / 26308.0 kg
Weight empty: 33180.8 lb / 15048.0 kg
Max. speed: 184 kts / 340 km/h
Service ceiling: 19800 ft / 6035 m
Wing load: 41.21 lb/sq.ft / 201.00 kg/sq.m
Range: 1947 nm / 3605 km
Crew: 8
Armament: 8x MG cal.50 (12,7mm), 3629kg Bomb./Depth Chrgs.


The Martin 187 was developed from the Maryland to specific British requirements. It differed primarily by having more powerful engines and a deeper fuselage to allow direct communication between crew members. Its narrow-section fuselage did make it virtually impossible for injured crew members to change positions in flight.
An order of 400 of these aircraft, named Baltimore by the RAF, was placed in May 1940, and following introduction of the US Lend-Lease Act two batches, of 575 and 600, were ordered in June and July 1941 respectively, and the full total of 1,575 aircraft was duly produced for the RAF.

This full total was not received, for some Mk III and Mk IIIA aircraft were lost during transatlantic delivery when two cargo ships carrying them were sunk. Initial deliveries of Baltimore Mk Is were made in late 1941, being issued first to Operational Training Units, and were followed by deliveries of Mk IIs in 1942 to Nos 55 and 223 Squadrons operating in the Middle East. All Baltimores were used operationally entirely in the Mediterranean theatre, proving to be effective day and night bombers. In addition to those used by the RAF, Baltimores were allocated by the RAF for service with the Royal Australian Air Force, Free French Air Force, Greek No. 13 (Hellenic) Squadron, Italian Co-Belligerent Air Force, and the South African, and Turkish air forces.
Martin 187 Baltimore
Engines: 2 x Wright GR-2600-A5B Cyclone 14, 1637 hp
Length: 48.507 ft / 14.785 m
Height: 17.749 ft / 5.41 m
Wingspan: 61.319 ft / 18.69 m
Wing area: 538.523 sqft / 50.030 sq.m
Max take off weight: 23198.8 lb / 10521.0 kg
Weight empty: 15463.7 lb / 7013.0 kg
Max. speed: 265 kts / 491 km/h
Cruising speed: 195 kts / 362 km/h
Service ceiling: 23294 ft / 7100 m
Wing load: 43.05 lbs/sq.ft / 210.00 kg/sq.m
Maximum range: 2433 nm / 4506 km
Range: 940 nm / 1741 km
Crew: 4
Armament: 8x MG cal.303 (7,7mm), 6x MG cal .30 (7,62mm), 907kg Bomb.
Baltimore Mk IV
Engines: 2 x Wright R-2600-10 Cyclone 14 radial, 1238kW
Max take-off weight: 10251 kg / 22600 lb
Empty weight: 7013 kg / 15461 lb
Wingspan: 18.69 m / 61 ft 4 in
Length: 14.8 m / 48 ft 7 in
Height: 5.41 m / 17 ft 9 in
Wing area: 50.03 sq.m / 538.52 sq ft
Max. speed: 491 km/h / 305 mph
Ceiling: 7100 m / 23300 ft
Range: 1741 km / 1082 miles
