Engineering:Stampe et Vertongen RSV.32

From HandWiki
RSV.32
RSV 32-90 O-BOEL.jpg
RSV 32-90
Role trainer aircraft
National origin Belgium
Manufacturer Stampe et Vertongen
Designer Alfred Renard
First flight 1923
Primary user Belgian Air Force [1]
Number built 57[1][2] (disputed[3])

The Stampe et Vertongen RSV.32[4] was a trainer aircraft produced in Belgium in the early 1920s.[1] Designed originally for the Stampe et Vertongen flying school,[5] the Belgian Air Force became a major operator of the type,[6] where it became the first aircraft of entirely Belgian design and manufacture to enter service.[2][3] Many others were purchased by flying clubs and private owners.[7] No RSV.32 was in existence by the end of World War II.[8]

History

Jean Stampe and Maurice Vertongen, veterans of World War I, founded a flying school at Deurne in 1923.[9] Their research into the training aircraft then available led them to believe that the British-built Central Centaur IV was the best choice for their school.[5] When they discovered that the Centaur IV had just ceased production, their friend, Maurice Boel, introduced them to engineer Alfred Renard, whom Stampe and Vertongen contracted to design a similar aircraft that could be built cheaply and locally.[5] Renard's response was a conventional two-bay biplane with unstaggered wings of equal span.[10] Power was provided by a radial engine in the nose.[10] The student pilot and instructor sat in tandem in a single, open cockpit[10] and communicated through a speaking tube.[11] The main units of the fixed undercarriage shared a common axle, and the tail was supported by a skid.[10] Construction was of wood throughout, braced with wire and covered in fabric,[8] and stressed to withstand rough treatment by student pilots.[12][13] To reduce costs, many parts were interchangeable, including the struts, longerons, undercarriage legs,[13] and even the upper and lower wings.[12] Initial construction of the prototype commenced in a dance hall in Evere[2][8] and was completed in the hangar of the Administration de l'Aéronautique[2] (the Belgian Aviation Administration) on 23 April 1923,.[13] The aircraft was registered O-BOEL in honour of the friend who introduced Renard to Stampe and Vertongen.[2][13] After the prototype had been tested, King Albert I paid a royal visit to Stampe et Vertongen and asked for a joy ride over Antwerp in it.[8]

The RSV.32 was produced between 1923 and 1932[2][11] and the total number built is sometimes given as fifty-seven,[14] however Paul de Meyer, writing for Air-Britain Digest in 1980 called this number "unlikely" and "greatly exaggerated".[3] The type saw service with not only Stampe et Vertongen's school, but flying schools at Gosselies and Saint-Hubert as well.[2] The Belgian Air Force purchased nineteen examples in three batches.[6] These served until 1936, when surviving machines were sold to private owners.[8] Flying clubs that operated the type included the Antwerp Aviation Club[7] and the Aéro-Club Royal Belge.[7] At least one private owner added a third seat to the aircraft,[15] and at least three examples were converted to 2+2 seating[8] with a fuselage modification designed by Renard.[2] This latter configuration was designated the RSV.32/2X2.[2]

Variants

The RSV.32 was built in at least seven variants. The precise subtype is known for forty-one aircraft:[16]

RSV.32/90
version with 67-kW (90-hp) Anzani 10C[1] engine (at least 9 built).[17]
RSV.32/100
version with 75-kW (100-hp) Renard engine (at least 8 built)
RSV.32/105
version with 78-kW (105-hp) Hermes engine (at least 1 built)
RSV.32/110
version with 82-kW (110-hp) Lorraine engine (at least 19 built, main production version for the Belgian Air Force [11])
RSV.32/120
version with 90-kW (120-hp) Renard engine (at least 2 built)
RSV.32/GII[18]
version with 90-kW (120-hp) de Havilland Gipsy engine, a fuselage oval in cross-section, and extra cabane struts to reduce wire bracing and make the forward cockpit more accessible[19] (1 built)
RSV.32/130
version with 97-kW (130-hp) Walter engine (at least 1 built)
RSV.32/2X2[20]
fuselage conversion to provide 2+2 seating (3 converted, including 1 32/100[15] and 2 32/120[7])

Additionally, one RSV.32 was to be fitted with an 82-kW (110-hp) Renard engine and possibly amphibious undercarriage, but this machine was never built.[21]

Finally, note that some of these aircraft were converted from other subtypes, so the same airframe might in some cases be counted twice in the production figures.[3]

Operators

 Belgium
 Spanish Republic

Specifications (RSV.32/90)

Data from Jouhaut 1999, p.33, except as noted

General characteristics

  • Crew: two
  • Length: 7.35 m (24 ft 1 in)
  • Wingspan: 11.20 m (36 ft 9 in)
  • Height: 2.80 m (9 ft 2 in)
  • Wing area: 32.0 m2 (344 sq ft)
  • Empty weight: 500 kg (1,100 lb)
  • Gross weight: 800 kg (1,800 lb)
  • Powerplant: 1 × Anzani 10C[1] , 67 kW (90 hp)

Performance

  • Maximum speed: 125 km/h (78 mph, 68 kn)
  • Service ceiling: 5,000 m (16,000 ft)
  • Rate of climb: 2.3 m/s (450 ft/min)

See also

Related lists

Notes

  1. ↑ 1.0 1.1 1.2 1.3 1.4 The Illustrated Encyclopedia of Aircraft, p.2955
  2. ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 Hauet 1984, p.9
  3. ↑ 3.0 3.1 3.2 3.3 de Maeyer 1980, p.4
  4. ↑ Stampe et Vertongen designated their designs with two numbers; the first signifying the wing area of the design in square metres, the second signifying the power of the engine in horsepower (Hauet 1984, p.9). Stampe et Vertongen aircraft designed by Alfred Renard gained the prefix "R" (Hauet 1984, p.7).
  5. ↑ 5.0 5.1 5.2 Jouhaut 1999, p.26
  6. ↑ 6.0 6.1 Jouhaut 1999, p.31
  7. ↑ 7.0 7.1 7.2 7.3 Jouhaut 1999, p.31–32
  8. ↑ 8.0 8.1 8.2 8.3 8.4 8.5 Jouhaut 1999, p.35
  9. ↑ Jouhaut 1999, p.25
  10. ↑ 10.0 10.1 10.2 10.3 Jouhaut 1999, p.34
  11. ↑ 11.0 11.1 11.2 Jouhaut 1999, p.30
  12. ↑ 12.0 12.1 Hauet 1984, p.10
  13. ↑ 13.0 13.1 13.2 13.3 Jouhaut 1999, p.29
  14. ↑ for example, by Jouhaut (1999, p.30), Hauett (1984, p.9), and The Illustrated Encyclopedia of Aircraft (p.2955)
  15. ↑ 15.0 15.1 Jouhaut 1999, p.32
  16. ↑ Jouhaut 1999, p.30, who bases his numbers on Hauet's (1984, p.9)
  17. ↑ Grey, C.G. (1924). Jane's all the World's Aircraft 1924. London: Sampson, Low, Marston & co Ltd.. p. 5b. 
  18. ↑ Taylor (1989, p.839) and Jouhaut (1999, pp.32–33,69–70) name this variant the 32/GII. Hauet (1984, p.9) and The Illustrated Encyclopedia of Aircraft (p.2955) describe the Gipsy-powered version as the 32/120, although Hauet distinguishes it from the 90-kW (120-hp) Renard-powered variant.
  19. ↑ Jouhaut 1999, p.69
  20. ↑ Jouhaut refers to this conversion (1999, pp.31–32,35) but does not name it
  21. ↑ de Maeyer 1980, p.5
  22. ↑ "Spanish Civil War Aircraft". http://www.zi.ku.dk/personal/drnash/model/spain/did.html. 

References

  • de Mayer, Paul (January–February 1980). "Built in Belgium: Part 1". Air-Britain Digest 32 (1): 3–6. 
  • Hauet, André (1984). Les avions Renard. Brussels: Éditions AELR. 
  • The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing. 
  • Jouhaud, Reginald (1999). Les Avions Stampe. Amsterdam: Wimpel. 
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. 
  • Wauthy, Jean-Luc; de Neve, Florian (June 1995). "Les aéronefs de la Force Aérienne Belge, deuxième partie 1919–1935" (in fr). Le Fana de l'Aviation (305): 28–33. ISSN 0757-4169. 



Retrieved from "https://handwiki.org/wiki/index.php?title=Engineering:Stampe_et_Vertongen_RSV.32&oldid=2448954"