William H. Martin of Canton, Ohio, died in March, 1937. Mr. Martin’s funeral had to be postponed, as international travelers wished to pay their respects to this gentleman who had the courage to stay with his convictions…
William H. Martin’s funeral caravan stretched for five miles…
With the experience gained from the conversion of Motor Cadet PFA.1385, P.J.Martin began building a definitive motor glider which he call the Martin Slug.
It was given the PFA number 1388 and was to be powered by a VW engine.
A single-seat biplane with a 90 hp Gnôme rotary engine. It was built for daredevil pilot Lincoln Beachey, but he rejected it on the grounds that it lacked necessary performance.
In 1910 Glenn L. Martin built another biplane machine with a slightly larger upper wing, interplane ailerons, a triangular stabilizer at the front rudder and a 50 hp Hall-Scott engine with which he set a few flight records of distance, duration and altitude in 1910 with flights from Newport-Beach to Catalina Island.
To meet a US Navy requirement for a high-performance multi-role flying-boat, Martin offered its Model 275 design. This had an all-metal hull of high length/beam ratio, mounting a cantilever high-set sharply-swept wing incorporating so much anhedral that the stabilising floats at the wing-tips could be attached permanently; the tail unit was of T-tail configuration with all-swept surfaces. Above the wing, to minimise spray ingestion, were mounted four Allison turbojet engines, and pressurised accommodation was provided for a crew of five. A beaching cradle allowed the SeaMaster to taxi in and out of the water under its own power. The P6M used a rotary bomb bay (as used on Martin’s licence-built Canberras and the XB-51). This permitted weapons release at high speeds without the drag of conventional bomb doors.
The first XP6M-1 prototype was flown on 14 July 1955, the second following on 18 May 1956. Ejection seats were fitted to the second and subsequent aircraft. These proved useful when the second SeaMaster pitched up, went into a loop and disintegrated. The original position of the engine exhausts caused stress on the rear fuselage which resulted in structural damage. The angle of the exhausts was adjusted after testing.
Martin received orders for six pre-production YP6M-1 boats powered by Allison J71 turbojets each developing a maximum 5897kg afterburning thrust. Successful flight testing led to an order for 24 production P6M-2 aircraft named SeaMaster, which differed primarily by having 7711kg thrust non-afterburning Pratt & Whitney J75-P-2 turbojet engines. The cockpit glazing was modified on later models to give a much better overhead and side view. However, the contract was cancelled on 21 August 1959 after only three had been built and these, together with the YP6M-1s, were scrapped at a later date. They were the fastest flying-boats ever built.
YP6M-1 Engines: 4 x J71 turbojet. Speed: 600 mph.
P6M Engines: 4 x Pratt & Whitney J75-P-2 turbojets, 7938kg Wingspan: 30.48 m / 100 ft 0 in Length: 40.84 m / 133 ft 12 in Height: 9.45 m / 31 ft 0 in Max take-off weight: 72575 kg / 160001 lb Payload: 13600kg / 29983 lb Max. speed: 965 km/h / 600 mph Ceiling: 12200 m / 40050 ft Range: 4830 km / 3001 miles Armament: 6 x 12.7mm machine-guns, 1800kg of weapons Crew: 4
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.
RB-57D
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.
Martin B-57B
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.
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.
B-57E
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.
Martin B-57 modified to test the Boeing Bomarc interceptor missile
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.
RB-57F
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.
NASA’s WB-57F
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
In World War lithe USAAF made widespread and effective use of the attack bomber for battlefield tasks. For post¬war service the USAAF wanted a higher-speed successor, and the specification produced two types in the Douglas XB-43 and Martin Model 234 XB-51.
The Martin was designed originally to meet a US Army Air Force requirement for a close-support bomber, being allocated the designation XA-45. However, it was developed instead as a medium bomber with turbojet power-plant and two prototypes were ordered under the designation XB-51.
The XB-51 featured a tandem-unit landing gear arrangement, a thin variable ¬incidence wing whose leading edges were swept at 35 degrees, a swept T-tail. It was powered by three 2640kg thrust General Electric J47-GE-7 or -13 turbo-jets, one pylon-mounted low on each side of the forward fuselage and the third within the rear fuselage.
Other features included pressurised accommodation for the two-man crew, provisisions for JATO (jet-assisted take-off) units, and a braking parachute.
The first of two aircraft flew in October 1949, Martin’s Director of Flight O.E. (Pat) Tibbs making the first flight, taking off from Baltimore and lading at Naval Air Test Centre at Patuxent, in a flight of 35 minutes.
XB-51 first take off
Although flight trials confirmed that the XB-51 had very good performance, they revealed that the type had poor handling qualities in the air. The XB-51 did not proceed past the prototype stage and the USAF opted instead for licence-production of the English Electric Canberra as the Martin B-57.
Engines: 3 x 2360kg General Electric J47-GE-13 Max take-off weight: 25393 kg / 55982 lb Empty weight: 13431 kg / 29610 lb Wingspan: 16.18 m / 53 ft 1 in Length: 25.93 m / 85 ft 1 in Height: 5.28 m / 17 ft 4 in Wing area: 50.91 sq.m / 547.99 sq ft Max. speed: 1038 km/h / 645 mph Cruise speed: 857 km/h / 533 mph Ceiling: 12344 m / 40500 ft Range: 2576 km / 1601 miles
During 1944 the US Army Air Force issued its first specification for a large jet bomber. By December 1944 proposals had been received from Boeing, Convair, Martin and North American for medium bomber for tactical- and operational-level use. The Martin Model 223 XB-48 being one of the contenders to meet this requirement.
Two XB-48 prototypes were ordered, the first of them flying on 14 June 1947 as a large shoulder mounted, straight wing monoplane with the capability of carrying up to 9072kg of bombs. Power was provided by six 1701kg thrust Allison J35-A-5 turbo-jets, three mounted beneath each wing. The landing gear was of the new bicycle form with main units ahead of and behind the bomb bay. The 33.02m span Model 223 failed to achieve the performance required and failed to win a production contract.
Engines: 6 x General Electric J35-C-7, 16.7kN Wingspan: 33.02 m / 108 ft 4 in Length: 26.14 m / 85 ft 9 in Wing area: 120.77 sq.m / 1299.96 sq ft Max take-off weight: 46539 kg / 102601 lb Empty weight: 26578 kg / 58595 lb Max. speed: 830 km/h / 516 mph Armament: 9000kg of bombs
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.
Martin RM-1
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.