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Short Type 184

The Short Type 184 was a two-seat , bombing, and torpedo-carrying developed by during the First World War, entering service with the Royal Naval Air Service (RNAS) in 1915 as the first purpose-built aircraft capable of carrying and launching aerial torpedoes. It measured 40 feet 7 inches in length with a of 63 feet 6 inches, weighed 3,704 pounds empty, and was powered by a 260 horsepower Maori engine, achieving a top speed of 88 miles per hour and a service ceiling of 9,000 feet. Over 936 units were produced by and nine other firms, making it the most numerous of its era, and it remained in limited service until the early 1930s with operators including the , , Chile, Estonia, , Greece, , and the . Designed as an evolution of the earlier Short Type 166, the Type 184 featured a conventional layout with fabric-covered wooden wings and , twin floats for water operations, and an open cockpit for a pilot and observer. Its armament typically included a single .303-inch for the observer and provision for either a 14-inch or up to 520 pounds of bombs, enabling versatile roles in coastal patrols, , and naval . The 's development began with two prototypes ordered in 1914, initially fitted with a 225 horsepower engine before upgrades to more powerful Sunbeam variants improved performance; the first flight occurred in early 1915, leading to rapid production amid wartime demands. Operationally, the Short Type 184 achieved several milestones, including the first successful torpedo strike from an aircraft on August 17, 1915, when Flight Commander Charles Edmonds sank a Turkish vessel in the Dardanelles, and the only British aircraft reconnaissance during the Battle of Jutland on May 31, 1916, flown by Flight Lieutenant Frederick Rutland from HMS Engadine. It supported Allied operations across the North Sea, Mediterranean, and Eastern Front, including anti-submarine duties and bombing raids, and post-war variants like the single-seat Type D bomber and landplane Short Bomber extended its utility until retirement by 1923 in British service.

Design and development

Origins and requirements

was founded in November 1908 by Eustace, Oswald, and Horace Short in , initially as a involved in ballooning before pivoting to powered flight with the construction of Wright-style biplanes under license. By 1914, amid the escalating tensions leading to , the company had relocated to , and increasingly focused on military aviation contracts for the Royal Navy Air Service (RNAS), leveraging their expertise in design to meet wartime demands. In September 1914, shortly after the war's outbreak, the Royal Navy issued a specification for a twin-float capable of , bombing, and delivery, aiming to equip its growing fleet of seaplane carriers with versatile aircraft for naval operations in contested waters. This requirement emphasized a robust design that could carry a 14-inch (356 mm) or equivalent bomb loads while operating from ships with limited deck space. responded by adapting their existing seaplane technology to fulfill this need. The firm secured an initial contract for two prototypes, assigned serial numbers 184 and 185, dedicated to torpedo trials. Influenced by prior designs like the Short Type 135—a folding-wing used in early RNAS operations—the Type 184 incorporated articulated wings that could fold for compact shipboard storage, operable even from the cockpit. The first prototype achieved its in early 1915 at , marking a key milestone in British development. During prototyping, the prototypes were initially fitted with a 160 hp rotary engine before various other options, including the 260 hp Maori, were evaluated to ensure sufficient power for the aircraft's multi-role capabilities.

Construction and features

The Short Type 184 was constructed as a three-bay with equal-span wings that incorporated a folding operated via a hand-winch and spigot system, allowing for compact storage on . The adopted a rectangular-section wire-braced wooden box-girder design, featuring spruce longerons reinforced with manganese fittings, while the overall structure was covered in fabric for lightweight durability. This wooden framework, including in the two-spar wings, was fabric-covered and braced with cabling, emphasizing simplicity and strength for operations. Adapted for water-based takeoffs and landings, the utilized twin unstepped main constructed from wood, supported by struts on front and rear cross-tubes, complemented by a incorporating a water-rudder for directional control. These , along with underwing cylindrical metal airbags or wooden tip , provided stability on the sea surface, with the overall dimensions measuring 40 ft 7.5 in in length, a of 63 ft 6.25 in, and a height of 13 ft 6 in. The design's large surfaces, nearly half the length and canvas-covered, further enhanced aerodynamic balance in configuration. Power was initially supplied by a 225 hp V-12 liquid-cooled engine, mounted with pressed steel crossbeams between the longitudinal beams and driving a four-bladed wooden . Subsequent upgrades included the 240 hp or the more powerful 260 hp Maori V-12, with a 12.27 L and a positioned above the fuselage ahead of the upper to optimize . The arrangement was a tandem two-seater, with the pilot positioned forward and the observer/gunner aft, separated by the , facilitating coordinated and attack roles. Communication was enabled through a foldable radio transmitter/receiver powered by a wind-driven , supplemented by a basket for carrier pigeons as a reliable backup method in remote naval scenarios. Armament provisions centered on a trainable rear mounting for a single 0.303 in Lewis machine gun handled by the observer, with structural adaptations under the wings and between the floats for suspending a 14 in or up to 520 lb of bombs, reflecting its dual and strike capabilities.

Operational history

World War I service

The Short Type 184 entered service with the Royal Naval Air Service (RNAS) in early 1915, initially deployed aboard seaplane carriers such as HMS Ben-my-Chree for operations in the during the . By the end of , production had reached a total of 936 aircraft, built by multiple manufacturers to meet the demands of , bombing, and missions across various theaters. These floatplanes proved versatile, with their design allowing carriage of a 14-inch or up to 520 pounds of bombs, enabling adaptation to emerging needs. A landmark achievement came on 17 August 1915, when Flight Commander Charles H. K. Edmonds, flying a Short Type 184 from Ben-my-Chree in the , conducted the world's first successful attack, sinking a Turkish supply ship in the . This operation, part of broader efforts to disrupt naval movements during the , demonstrated the aircraft's potential for anti-shipping strikes, though subsequent missions were limited by operational challenges like rough seas and enemy defenses. Earlier, on 12 August, Edmonds had attempted the first-ever air-launched drop against a Turkish tug, but the weapon missed its target. In home waters, the Short Type 184 played a pivotal role during the on 31 May 1916, where a single , serial number 8359, launched from the seaplane carrier HMS Engadine and piloted by J. Rutland with Assistant Paymaster G. S. Trewin as observer, conducted the only British of the engagement. Spotting the German fleet at 3:08 p.m., Rutland's report via wireless helped the Grand Fleet maneuver, though heavy weather prevented further sorties from Engadine's other Short 184s. The endured anti-aircraft fire and returned safely after approximately 40 minutes aloft, underscoring the type's endurance in combat conditions. The Short Type 184 also supported land operations in , where RNAS units used the aircraft for and supply drops during of Kut-al-Amara from April to May 1916. Operating from bases along the River, such as at Ora, pilots delivered essential food and medical parcels to the besieged , marking one of the earliest sustained airlifts in , though high temperatures limited payload capacity to 200-250 pounds per flight. In the and , squadrons equipped with bomb-laden Short 184s conducted extensive anti-submarine patrols starting in 1916, focusing on U-boat hunting through visual spotting and or bomb attacks; while numerous sightings were reported, no confirmed U-boat sinkings were attributed to the type, but these missions contributed to numerous sorties by RNAS seaplanes overall, enhancing protection and deterring German submarine activity.

Post-war operations

Following the , surviving Short Type 184 aircraft in service were primarily repurposed for mine-spotting patrols over coastal waters to clear wartime hazards from shipping lanes. These duties continued into , after which the type was phased out of frontline use, with the last units retired by and all withdrawn from circulation by early 1923. Several ex-military examples were converted for civilian operations, including modifications to four-seat configurations for passenger joyrides. In 1919, the Eastbourne Aviation Company acquired and adapted two such aircraft, registered G-EAJT (formerly N2998) and G-EALC (formerly N2986), both originally built by , to offer short flights from coastal bases. Internationally, the Short Type 184 saw limited but extended post-war military service. Estonia received eight examples in 1919 for its nascent , retaining them for coastal and patrol duties until the final unit, serial 40, crashed in the on 3 November 1933. Japan also operated the type after , though specific roles remain sparsely documented beyond general tasks. Preservation efforts highlight the aircraft's historical legacy. In 2011, a full-scale non-flying of the Short Type 184 was completed by aviation enthusiasts and installed in 2012 at the Seaplane Harbour branch of the Estonian Maritime Museum in , where it remains on display as of 2025 to represent early interwar .

Variants

Standard Type 184

The Short Type 184 was initially developed as a two-seat reconnaissance and torpedo-carrying floatplane, powered by a 225 hp Sunbeam Mohawk V-12 engine for its early prototypes and initial torpedo trials conducted in 1915. This configuration featured a three-bay biplane structure with folding wings, a rectangular wooden fuselage covered in fabric, and twin main floats for water operations, emphasizing stability and payload capacity for naval use. From 1916 onward, production shifted to the Improved Type 184, which adopted the more powerful 260 hp Maori V-12 engine as the standard powerplant, enabling better performance with heavier loads such as torpedoes or bombs while retaining the core design. Minor tweaks included enhancements to the ailerons and , with the Maori's quad-bladed design improving reliability and thrust for operational demands. This variant became the baseline for most wartime , balancing , bombing, and roles. The Short Cut variant represented an aerodynamic refinement of the Improved Type 184, featuring a reduced on the lower wings, added deflecting boards beneath the wings to minimize , and a smaller area to optimize . These changes, applied to a limited number of airframes, yielded a 6-knot increase in top speed and improved climb rate without altering the engine or overall dimensions, focusing on enhanced maneuverability for specific testing and patrol duties. A specialized adaptation was the Type D single-seat bomber version, where the observer's position was eliminated and the pilot relocated to the rear cockpit to accommodate internal bomb storage. This configuration carried nine 65 lb bombs slung nose-up forward of the cockpit, with improvised Lewis gun mountings for defense, prioritizing bombing capacity over dual-crew reconnaissance while using the standard Improved Type 184 airframe and engine.

Modified and export variants

The Type 184 was a specialized adaptation of the standard , featuring enlarged main floats and revised wingtip floats to enhance in rougher seas encountered during North Sea patrols by the Dover Patrol. These modifications allowed for operations from bases at and , prioritizing seaworthiness over the baseline design's coastal focus. The Short Bomber represented a landplane conversion of the Type 184, replacing the floats with a wheeled to enable shore-based and bombing missions. This variant, developed in response to requirements for long-range operations, incorporated the same folding-wing mechanism but adapted for terrestrial takeoffs and landings, serving both the Royal Flying Corps and . Some production examples were equipped with a 240 hp 12F engine, built by British firms such as Robey and Saunders, to align with local manufacturing and supply chains. These aircraft, constructed by firms like Robey, maintained the core structure but benefited from the Renault's reliability for continental operations. One Short Type 184 was acquired by the for evaluation in engine testing and early carrier compatibility trials, akin to those on British vessels like HMS Argus. In theaters like , some aircraft received enhanced bomb racks under the wings to carry multiple 112 lb ordnance, facilitating extended anti-ground support in arid environments.

Operators

United Kingdom

The Royal Naval Air Service (RNAS) served as the primary operator of the Short Type 184 from its introduction in 1915, employing it extensively for reconnaissance, bombing, and torpedo delivery roles during World War I. Upon the formation of the Royal Air Force (RAF) in April 1918 through the merger of the RNAS and Royal Flying Corps, operational responsibility for surviving Type 184s transitioned seamlessly to the new service. Key RNAS units included No. 1 Wing, which deployed Type 184s during the Dardanelles Campaign in 1915 for spotting and torpedo attacks against Ottoman naval targets. These aircraft were also embarked on seaplane carriers such as HMS Ben-my-Chree, which carried up to four Type 184s and supported operations in the Aegean Sea, including the historic first aerial torpedo strike on 12 August 1915. Other carriers like HMS Engadine and HMS Ark Royal similarly integrated the Type 184 into fleet air operations for anti-submarine patrols and coastal reconnaissance. Post-war, a small number of surplus Type 184s entered civilian service, notably with the Aviation Company, which modified at least two examples for four-seat passenger configuration and conducted joyriding flights along the coast from 1919 to 1920. Of the total 936 Type 184s produced, approximately 700 were operated by military forces, with the remainder allocated to exports or other uses; all were retired from RAF service by 1922 following the Geddes Axe defense cuts.

International operators

The Short Type 184 saw limited export and foreign service beyond the , primarily for and coastal patrol roles in the . Several nations acquired small numbers through purchase, transfer, or internment during or shortly after , often adapting the aircraft for local conditions with minimal modifications. operated Short Type 184s with the Royal Canadian Naval Air Service. Chile acquired six Short Type 184 seaplanes in 1919 for use by the 1° Grupo de Aviación Naval, employing them in coastal reconnaissance duties until retirement in 1933. These aircraft, serialed 1 through 6, represented one of the larger foreign acquisitions and supported Chile's nascent naval aviation efforts along its Pacific coastline. Greece received five Short Type 184 hydroplanes by the end of World War I, including serials 8094, N1651, N1652, N1654, and N1655, which were transferred from British stocks. Powered by either Renault 240 hp or Sunbeam Maori 260 hp engines, they served briefly as bombers in the Hellenic Naval Air Service but saw no recorded combat action, with no surviving photographs bearing Greek markings. The Netherlands operated a single Short Type 184, interned from the Royal Naval Air Service in 1917, which remained in Dutch naval service until 1920 for training and evaluation purposes. This isolated example highlighted the aircraft's adaptability in neutral territories during wartime. Estonia purchased eight Short Type 184s in 1919 for the , utilizing them extensively for maritime patrol duties in the . At least two survived into the early , with the last operational loss occurring on November 3, 1933, when one crashed in the ; this made the longest-serving foreign operator of the type. France received two Short Type 184s (serials 8083 and 8084) transferred from production in for government evaluation, likely assessing their potential for Aéronautique Navale in the Mediterranean. These did not enter widespread operational and were not modified with local engines as initially considered. Japan acquired one Short Type 184, redesignated as the Yokosuka Navy Short Seaplane, which the used primarily as a trainer in the early to support initial carrier and experiments, including operations from vessels like the Wakamiya. This sole example influenced early Japanese development but was not produced in quantity.

Production

Manufacturers

The Short Type 184 was primarily designed and manufactured by , a pioneering firm based in , with additional production facilities at Eastchurch on the Isle of Sheppey. As the originators of the design in response to an Admiralty specification issued in early 1915, handled the initial prototypes and led the development process, incorporating feedback from naval trials to refine the seaplane's structure for , bombing, and roles. Their Rochester works focused on assembling complete aircraft, emphasizing quality control and integration of the 225 hp Sunbeam engine, while Eastchurch supported component fabrication and testing in a coastal environment suited to seaplane operations. To meet escalating wartime demand amid , the initiated a licensing program in 1915, subcontracting production to several engineering firms with established manufacturing capabilities in and . This dispersal strategy aimed to accelerate output for the Royal Naval Air Service, leveraging factories across southern and central , including sites on of Wight, in the , and near . oversaw design dissemination and provided technical support to licensees, ensuring adherence to specifications despite varying subcontractor expertise. Brush Electrical Engineering Co. Ltd., based in , , was one of the largest licensees, adapting its electrical machinery production lines to aircraft assembly and contributing robust fuselages and structures suited for marine corrosion resistance. Their capacity allowed for efficient scaling, drawing on pre-war experience in heavy engineering to produce reliable frames under high-pressure wartime schedules. Robey & Co. Ltd., an agricultural machinery manufacturer in , , similarly pivoted to , excelling in rigging and engine mounting, with their facilities enabling rapid prototyping of modifications for different operational theaters. J. Samuel White & Co. Ltd., a firm at on of , leveraged its maritime expertise to specialize in floatplane hulls and seaworthy components, integrating seamlessly with the Type 184's naval requirements. Nearby, S.E. Saunders Ltd. in also on of , focused on advanced float designs, including enlarged variants for improved stability, and assembled complete aircraft using boat-building techniques that enhanced water-handling performance. These Isle of Wight operations benefited from proximity to naval bases, facilitating direct testing and delivery. Subcontractors like Phoenix Dynamo Manufacturing Co. Ltd. in , , primarily handled specialized components such as electrical systems and sub-assemblies, supporting full-aircraft production at other sites while building a smaller number of complete units. This division of labor helped mitigate bottlenecks in skilled labor and materials, though it occasionally led to minor quality variations in fit and finish across licensees, addressed through inspections. Overall, the collaborative network underscored the Type 184's role as a of wartime expansion.

Production totals and distribution

A total of 936 Short Type 184 aircraft were produced between 1915 and 1918 to meet the demands of World War I naval aviation. This figure encompassed the initial prototypes and subsequent production models, marking a significant scaling effort from early trials to mass manufacturing across multiple facilities to support reconnaissance, bombing, and torpedo operations on various fronts. Production was distributed among ten British manufacturers, reflecting the wartime urgency to expand output beyond ' Rochester works. The breakdown is as follows:
ManufacturerNumber Built
117
Brush Electrical Engineering Co. Ltd.190
Frederick Sage & Co. Ltd.72
110
Mann, Egerton & Co. Ltd.22
Phoenix Dynamo Manufacturing Company62
Robey & Co. Ltd.256
S E Saunders Limited80
Supermarine Aviation Works Ltd.15
Westland Aircraft Works Ltd.12
Robey & Co. Ltd. emerged as the largest subcontractor, contributing over a quarter of the total to bolster supply rates during peak demand in 1916 and 1917. The vast majority of these aircraft—over 700—were allocated to the Royal Naval Air Service (RNAS) and later the Royal Air Force (RAF) for service in home waters, the Mediterranean, and other theaters. Fewer than 100 were exported to international operators, including , , (eight aircraft), , , (two for testing), and the , with some remaining in use into the early 1930s. This distribution underscored the type's primary role in British while enabling limited to allies.

Specifications

General characteristics

The Short Type 184 accommodated a crew of two, consisting of a pilot and an observer. Its dimensions included a length of 40 ft 7.5 in (12.38 m), a of 63 ft 6.25 in (19.36 m), a of 13 ft 6 in (4.11 m), and a wing area of 688 sq ft (63.9 m²). The aircraft had an empty weight of 3,703 lb (1,680 kg) and a gross weight of 5,363 lb (2,433 kg). It was powered by a single 260 hp (194 kW) Maori V-12 engine, serving as the basis for the improved variant.

Performance

The Short Type 184 exhibited reliable flight performance suited to and delivery roles during , achieving a maximum speed of 88.5 mph (142 km/h) at 2,000 ft (610 m) in its improved configuration powered by the 260 hp Maori engine. This represented a notable enhancement over early prototypes, which attained approximately 70 mph with initial 160-225 hp powerplants like the Gnome or , underscoring the impact of engine upgrades on overall velocity and operational efficiency. Operational range extended to 243 mi (391 km) under standard conditions, complemented by an of 2.75 hours, enabling extended patrols from seaplane carriers or coastal bases without frequent refueling. The aircraft's service ceiling reached 9,000 (2,700 ), providing sufficient altitude for spotting surface vessels while maintaining visibility over maritime theaters. Additionally, time to 2,000 (610 ) was 8 min 35 , allowing reasonable ascent times to operational heights despite the biplane's inherent drag from floats and open . These metrics, derived from trials with the 225-260 hp variants, balanced speed, loiter time, and payload capacity, making the Type 184 a versatile platform that influenced subsequent designs.

Armament

The Short Type 184 was equipped with a single .303 in (7.7 mm) mounted on a trainable pivot in the rear , operated by the observer for defensive fire. For its primary offensive role, the carried either one 14 in (356 mm) weighing approximately 900 lb (408 kg) or up to 520 lb (236 kg) of bombs, depending on the mission requirements. The was slung externally on an under-fuselage rack designed for release at low altitude, marking the Type 184 as the first to successfully deploy a against an enemy vessel in . Bomb configurations varied for versatility in reconnaissance and bombing duties; representative loads included four 112 lb (51 kg) bombs or nine 65 lb (29 kg) bombs, particularly in the single-seat Type D variant adapted for bombing. The same under-fuselage rack allowed adaptability for other ordnance, such as depth charges in post-war anti-submarine patrol variants, reflecting an evolution from initial torpedo-centric designs to more flexible bomb-carrying setups amid changing naval threats.

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