SPAD S.XIII

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S.XIII
SPAD S.XIII in the colors and markings of
National Museum of the U.S. Air Force
near Dayton, Ohio.
Role biplane fighter
National origin France
Manufacturer
SPAD
Designer Louis Béchéreau
First flight 4 April 1917[1]
Primary users Aéronautique Militaire
Royal Flying Corps (Royal Air Force from April 1918)
United States Army Air Service
Number built 8,472[2]

The SPAD S.XIII is a French

Société Pour L'Aviation et ses Dérivés (SPAD) from the earlier and highly successful SPAD S.VII
.

During early 1917, the French designer

Armistice.[2]

By the end of the First World War, the S.XIII had equipped virtually every fighter squadron of the Aéronautique Militaire. In addition, the United States Army Air Service also procured the type in bulk during the conflict, and some replaced or supplemented S.VIIs in the Royal Flying Corps (RFC), pending the arrival of Sopwith Dolphins. It proved popular with its pilots; numerous aces from various nations flew the S.XIII during their flying careers. Following the signing of the Armistice of 11 November 1918, which effectively marked the end of the First World War, surplus S.XIIIs were sold in great numbers to both civil and military operators throughout the world.

Development

Background

The origins of the SPAD S.XIII lies in the performance of its predecessor, the

Aéronautique Militaire during August 1916.[3] By early 1917, however, the S.VII had been surpassed by the latest German fighters such as the Albatros D.I.[4]

The emergence of increasingly capable German fighters, which soon resulted in a shift in aerial supremacy towards the Central Powers, led to calls for superior aircraft to be developed and procured.[5] French flying ace Georges Guynemer personally lobbied for an improved version of the S.VII, telling the SPAD designer Louis Béchereau that "The 150 hp SPAD is not a match for the Halberstadt ... More speed is needed."[6] An initial and quick solution to the problem was to increase the compression ratio of the Hispano-Suiza engine, which increased its power to 180 hp (130 kW) to provide for significantly improved performance, allowing the SPAD S.VII to remain competitive for the time being.[7]

Spanish manufacturer Hispano-Suiza were already in the process of developing a more powerful geared version of the 8A engine,[4] and this engine was unsurprisingly chosen by Béchereau to power two developed versions of the S.VII. The British S.E.5a and Sopwith Dolphin fighters would also be powered by the same engine.[5]

Intro flight

The first of Béchereau's designs to fly with the new, gear-reduction HS.8B engine design series was the S.XII in its HS.8BeC (or "HS-38") version, which was armed with an unusual 37 mm (1.457 in) cannon that fired through the propeller shaft. However, this aircraft only saw limited use, having been rapidly followed into production by the more conventionally armed S.XIII, which was deemed to be a preferable configuration by several French pilots and officials.[8] Aviation author C.F. Andrews has claimed that a large portion of the credit for the S.XIII lies with Marc Birkigt, the designer of the engine, who had chosen to introduce various innovative features upon it, such as monobloc aluminium cylinders, which were furnished with screwed-in steel liners, which improved its performance.[9]

On 4 April 1917, the SPAD S.XIII performed its maiden flight.[10][11] An early distinguishing feature of the S.XIII - as with the SPAD S.XII - was that its similarly-geared HS.8Be V8 engine mandated a left-handed propeller rotating in the opposite rotation to the earlier, direct-drive HS.8A-powered S.VII. Early on, similarly to the British Sopwith Dolphin also powered with HS.8B-series geared V8s, problems were encountered with the HS.8B engine's gearing; however, Béchereau opted to persist with the engine, which was soon refined and became fairly reliable.[11] Efforts to ramp up production of the type commenced almost immediately after the first flight was conducted. Within months of its first flight, the S.XIII had not only entered service with the Aéronautique Militaire but had quickly proven itself to be a successful fighter.[11]

Design

The SPAD S.XIII was a single-engine biplane fighter aircraft. In terms of its construction, it shared a similar configuration and layout to the earlier S.VII,

fabric covering;[12] however, it was generally larger and heavier than its predecessor. Other changes included the tapered chord of its ailerons, the rounded tips of the tailplanes, bulkier cowling accommodating the gear-drive Hispano-Suiza 8B engine choice, and enlarged fin and rudder.[11] The S.XIII was armed with a pair of forward-mounted Vickers machine guns with 400 rounds per gun, which took the place of the single gun that had been used on the earlier aircraft.[10]

The S.XIII featured relatively conventional construction, that being a wire-braced biplane with a box-shaped fuselage and a front-mounted engine, except for its interposed wing struts located half-way along the wing span, which gave the fighter the deceptive appearance of being a double-bay aircraft instead of a single bay.[13] This change prevented the landing brace wires from whipping and chafing during flight, and was attributed by Andrews as a key factor for the aircraft's high rate of climb. Otherwise, it had an orthodox structure, comprising wooden members attached to metal joint fixtures.[13] The fuselage consisted of four square-section longerons, complete with wooden struts and cross-members while braced with heavy-gauge piano wire; wire cable was instead used for the flying and landing wires.[14]

A SPAD S.XIII of the American 103rd Aero Squadron - note exposed aileron bellcrank protruding from lower wing, also used for the A.2 "pulpit fighter" and S.VII.
A SPAD S.XIII at Air Service Production Center No. 2, Romorantin Aerodrome, France, 1918

To facilitate its two-hour endurance, the S.XIII was furnished with an assortment of underbelly fuel tanks held within the forward fuselage area; these were fed into the main service tank located in the center of the upper wing by an engine-driven pump.

blinds as a means of regulating the temperature of the engine.[12]

The upper wing was a single-piece structure, featuring hollow box-section short spars which connected with linen-bandaged scarf joints, Andrews claims that long runs of spruce were difficult to obtain.[14] The ribs consisted of plywood webs and spruce capping strips, which were internally braced with piano wire. The upper wing was provisioned with ailerons, which were actuated by the pilot via a series of tubular pushrods which ran vertical directly beneath the ailerons, with external, 90º bellcranks exposed above the lower wing panels' top fabric covering.[15] The lower wing consisted of spruce leading edges and wire-cable trailing edges, while the surfaces were fabric-covered and treated with aircraft dope to produce a scalloped effect, much as with the contemporary German Fokker D.VII that also used a wire trailing-edge component, along the trailing edges.[14]

While the forward Vickers machine guns were installed as standard, they were not always present upon all aircraft. As a result of fears of a shortage of Vickers guns during the last few months of the war, several American squadrons equipped with the S.XIII decided to replace their existing Vickers .303 machine guns with the lighter (25 lbs/11.34 kg apiece)

.30/06-calibre Marlin Rockwell M1917 and M1918 aircraft machine guns,[16][17] saving some sixteen pounds (7.3 kg) in weight[18]
over the twin-mount Vickers' total weight of 66 lbs (29.94 kg) for the guns alone. Reportedly, by the end of the war, roughly one half of the aircraft in American service had been converted in this fashion.

The powerplant of the S.XIII was a geared Hispano-Suiza engine, at first a 8Ba providing 200 hp (150 kW),

Royal Aircraft Factory SE.5 which could be landed with power off.[11]

While giving the Spad XIII outstanding performance, the geared engines proved to be unreliable, suffering from vibration and poor lubrication. This significantly and severely affected serviceability, with it being stated in November 1917 that the Spad S.XIII was "incapable of giving dependable service". Even in April 1918, an official report stated that two-thirds of the 200 hp SPADs were out of use at any one time due to engine problems.[20] At least one American observer believed at the time that the French were giving the US SPAD XIII squadrons lower-quality engines from their least favored manufacturers while keeping the best for themselves.[citation needed] Allegedly, the reliability issues encountered with the engine were considered an acceptable price to pay for the improved performance, however,[21] as time went by, a combination of improved build quality and changes to the engine design led to increased levels of serviceability.[22]

At the beginning of 1918 the Aviation Militaire issued a requirement for a more powerful fighter, in a C1 (Chasseur single-seat) specification. SPAD responded by fitting the 300 hp (220 kW) Hispano-Suiza 8Fb in the SPAD XIII airframe. The structure was strengthened and improved aero-dynamically, retaining the dimensions of the SPAD XIII. Twenty SPAD XVII fighters were built and issued to units with GC 12 (Les Cigones).

Operational history

A SPAD XIII painted to represent the aircraft flown by Arizona native Frank Luke Jr., the first aviator awarded the Medal of Honor, the highest military decoration in the United States, in World War I.

During May 1917, only one month following the type's maiden flight, deliveries to the Armée de l'Air commenced.[23] The new aircraft quickly became an important element in the French plans for its fighter force, being expected to replace the SPAD S.VII as well as the few remaining Nieuport fighters in front line service. However, these plans were disrupted by deliveries occurring at a much slower rate than had been initially forecast; by the end of March 1918, 764 fighters had been delivered compared with a planned force of 2,230.[24]

Eventually, the S.XIII equipped virtually every French fighter squadron, 74

escadrilles, during the First World War.[25] At the end of the war, plans were underway to replace the S.XIII with several fighter types powered by the 300 hp (220 kW) Hispano-Suiza 8F, such as the Nieuport-Delage NiD 29, the SPAD S.XX and the Sopwith Dolphin II.[26] These plans lapsed following the signing of the Armistice of 11 November 1918, which ended the First World War and the SPAD S.XIII remained in French service as a fighter aircraft until 1923.[16]

The S.XIII was flown by numerous famous French fighter pilots such as

Rene Fonck (the highest scoring Allied ace, credited with 75 victories), Georges Guynemer (54 victories), and Charles Nungesser (45 victories), and also by the leading Italian ace Francesco Baracca (34 victories).[27] Aces of the United States Army Air Service who flew the S.XIII include Eddie Rickenbacker (America's leading First World War ace with 26 confirmed victories) and Frank Luke (18 victories). Andrews attributes the S.XIII's natural stability, which lent itself to being a steady gun platform, as having been a key attribute for its success.[28]

USAAS

Other Allied forces were quick to adopt the new fighter as well; the SPAD XIII equipped 15 of the 16 operational American pursuit squadrons of the USAAS by the signing of the Armistice. Even prior to America's entry into the conflict, American volunteers flying with the Allies had been piloting the type.

Thomas-Morse MB-3 fighter (which used SPAD-type wings in its construction) in 1922; according to Andrews, the Wright-Hispano engine was incapable of matching the performance of the original powerplant.[29]

RFC

During December 1917, No 23 Squadron of the Royal Flying Corps (RFC) equipped with the SPAD S.XIII, retaining them until April 1918 when it re-equipped with the Dolphin, while No. 19 Squadron (officially equipped with the earlier S.VII) also operated at least a single S.XIII for a time.[30] It was alleged by Andrews that the type was sometimes used as an interim fighter while awaiting the delivery of British-built aircraft.[29]

In his memoir Sagittarius Rising, Cecil Lewis described an aerial competition between himself and a SPAD flown by Guynemer, while Lewis was flying an SE5, "Their speeds were almost identical, but the high-compression Spad climbed quicker. After the race was over, Guynemeyer and I held a demonstration combat over the aerodrome. Again I was badly worsted. Guynemeyer was all over me. In his hands the Spad was a marvel of flexibility. In the first minute I should have been shot down a dozen times".[31]

Corpo Aeronautico Militare

The S.XIII was also acquired by Italy for the Corpo Aeronautico Militare.[29] Andrews has claimed that Italian pilots expressed an overall preference for another French-built fighter, the Hanriot HD.1, which was more maneuverable but considerably less powerful in comparison. Belgium also operated the S.XIII; one Belgian ace, Edmond Thieffry, came to prominence while piloting the type.[29] After the end of the war, the S.XIII was also exported to further nations, including Japan, Poland and Czechoslovakia.[citation needed]

Gallery

  • SPAD XIII Georges Guynemer
    SPAD XIII Georges Guynemer
  • SPAD XIII René Fonck
    SPAD XIII René Fonck
  • SPAD XIII Edward Rickenbacker
    SPAD XIII
    Edward Rickenbacker
  • SPAD XIII David "Duffy" Lewis
    SPAD XIII David "Duffy" Lewis

Operators

 Argentina
 Belgium
 Brazil
  • Aviação Militar do Exército Brasileiro (Brazilian Army Aviation) - 1920 to 1930
 Czechoslovakia
 France

Aéronautique Militaire

 Greece
 Kingdom of Italy
 Empire of Japan
Poland Second Polish Republic
 Romania
 Russian Empire
 Kingdom of Serbia
 Soviet Union
  • Soviet Air Force
    – Taken over from the Imperial Russian Air Force.
Siam
Kingdom of Spain
  • Spanish Air Force
 Turkey
United Kingdom United Kingdom
 United States
 Uruguay

Surviving aircraft

Belgium

France

United States

Specifications (SPAD S.XIII)

Data from French Aircraft of the First World War[42]

General characteristics

  • Crew: 1
  • Length: 6.25 m (20 ft 6 in)
  • Wingspan: 8.25 m (27 ft 1 in) late examples had a span of 8.08 m (26.5 ft)
  • Height: 2.60 m (8 ft 6 in)
  • Wing area: 21.11 m2 (227.2 sq ft) late examples had a wing area of 20.2 m2 (217 sq ft)
  • Empty weight: 601.5 kg (1,326 lb)
  • Gross weight: 856.5 kg (1,888 lb)
  • Powerplant: 1 × Hispano-Suiza 8Ba, Bb or Bd Water cooled 8-cylinder vee-type, 150 kW (200 hp)

Performance

  • Maximum speed: 211 km/h (131 mph, 114 kn) at 1,000 m (3,300 ft)
    • 208.5 km/h (129.6 mph; 112.6 kn) at 2,000 m (6,600 ft)
    • 205.5 km/h (127.7 mph; 111.0 kn) at 3,000 m (9,800 ft)
    • 201 km/h (125 mph; 109 kn) at 4,000 m (13,000 ft)
    • 190 km/h (120 mph; 100 kn) at 5,000 m (16,000 ft)
  • Endurance: 2 hours
  • Service ceiling: 6,800 m (22,300 ft)
  • Time to altitude:
    • 2 minutes 20 seconds to 1,000 m (3,300 ft)
    • 5 minutes 17 seconds to 2,000 m (6,600 ft)
    • 8 minutes 45 seconds to 3,000 m (9,800 ft)
    • 13 minutes 5 seconds to 4,000 m (13,000 ft)
    • 20 minutes 10 seconds to 5,000 m (16,000 ft)
  • Wing loading: 40 kg/m2 (8.2 lb/sq ft)

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

References

Notes

  1. bay wings, they were fitted with tie struts to support the bracing wires halfway along the wing, which gave the appearance of a two-bay wing.[11]

Citations

  1. ^ Winchester 2006, p. 23.
  2. ^ a b Sharpe 2000, p. 272.
  3. ^ Bruce Air Enthusiast Fifteen, pp. 58–60.
  4. ^ a b Andrews 1965, p. 4.
  5. ^ a b Andrews 1965, pp. 4-5.
  6. ^ Bruce Air International May 1976, p. 240.
  7. ^ Bruce Air Enthusiast Fifteen, pp. 61–62.
  8. ^ Bruce Air International May 1976, pp. 240–242.
  9. ^ Andrews 1965, p. 5.
  10. ^ a b c Bruce Air International June 1976, p. 289.
  11. ^ a b c d e f g Andrews 1965, p. 6.
  12. ^ a b Andrews 1965, pp. 7–8.
  13. ^ a b Andrews 1965, pp. 6–7.
  14. ^ a b c Andrews 1965, p. 7.
  15. ^ a b Andrews 1965, p. 8.
  16. ^ a b Bruce Air International June 1976, p. 312.
  17. ^ Maurer 1978, pp. 146–147.
  18. ^ Archived Marlin M1917/18 machine gun specification page
  19. ^ Bruce Air International June 1976, p. 292.
  20. ^ Bruce Air International June 1976, p. 291.
  21. ^ Bruce Air International June 1976, p. 293.
  22. ^ Bruce et al. 1969, p. 9.
  23. ^ Bruce Air International June 1976, p. 280.
  24. ^ Bruce Air International June 1976, pp. 290–291.
  25. ^ Bruce Air International June 1976, pp. 293–294.
  26. ^ Bruce Air International June 1976, p. 310.
  27. ^ Andrews 1965, pp. 8-10.
  28. ^ Andrews 1965, p. 9.
  29. ^ a b c d e Andrews 1965, p. 10.
  30. ^ Bruce 1982, pp. 561–563.
  31. ^ Sagittarius Rising, Cecil Lewis
  32. ^ "Modelism International - Spad Vii-Xiii en Romania PDF" (in Romanian).
  33. ^ Bruce 1982, pp. 561–564.
  34. ^ "Airframe Dossier – Societe Pour lAviation et ses Derives (SPAD)XIII, c/n SP-49". Aerial Visuals. AerialVisuals.ca. Retrieved 11 May 2017.
  35. ^ "Spad XIII C1". Memorial Flight. Retrieved 11 May 2017.
  36. ^ "Immatriculation des aéronefs [F-AZFP]" (in French). Retrieved 12 May 2017.
  37. ^ "Airframe Dossier – Societe Pour lAviation et ses Derives (SPAD)XIII, s/n S5295 RAF, c/n S5295". Aerial Visuals. AerialVisuals.ca. Retrieved 11 May 2017.
  38. ^ "Spad XIII "Smith IV"". Smithsonian National Air and Space Museum. Retrieved 11 May 2017.
  39. ^ "Airframe Dossier – Societe Pour lAviation et ses Derives (SPAD)XIII, s/n 7689". Aerial Visuals. AerialVisuals.ca. Retrieved 12 May 2017.
  40. ^ "SPAD XIII C.1". National Museum of the US Air Force. 7 April 2015. Retrieved 11 May 2017.
  41. ^ "SPAD XIII at Sky Harbor International". Skytamer. Retrieved 5 March 2019.
  42. ^ Davilla, 1997, p.509

Bibliography

External links

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