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Morane-Saulnier MS.315

The Morane-Saulnier MS.315 was a primary training monoplane designed and built in France by Morane-Saulnier.

MS.315
Morane-Saulnier MS.317
Role Primary trainer
National origin France
Manufacturer Morane-Saulnier
First flight 1932
Primary user French Air Force
Number built 356
Developed from Morane-Saulnier MS.300

Development edit

The MS.315 was developed from the earlier MS.300 primary trainer and related variants and first flew in October 1932. The MS.315 is a parasol-wing monoplane with a tailskid, with divided main landing gear, and powered by a 135 hp (101 kW) Salmson 9Nc radial engine. A production run of 346 aircraft followed the four prototypes (including 33 built after the Second World War). Five high-powered MS.317/2 variants were also produced for the civil market, and a single MS.316 was built, powered by a Régnier inverted Vee engine.

In the 1960s 40 MS.315 used as civil glider tugs were modified with a 220 hp (164 kW) Continental W670-K radial engine and re-designated the MS.317.

Variants edit

MS.315
Production version with a 135hp (101kW) Salmson 9Nc radial engine, 350 built.
MS.315/2
Higher powered civil version, five built.
MS.316
Variant powered by a Regnier inverted Vee engine, one built.
MS.317
1960s conversions with a 220hp (164kW) Continental W670-K radial engine, 40 converted.

Operators edit

  France
  Peru

Specifications (MS.315) edit

Data from [1]

General characteristics

  • Crew: 2
  • Length: 7.60 m (24 ft 11.25 in)
  • Wingspan: 12.00 m (39 ft 4.5 in)
  • Height: 2.80 m (9 ft 2.25 in)
  • Wing area: 21.60 m2 (232.51 sq ft)
  • Empty weight: 548 kg (1,208 lb)
  • Gross weight: 860 kg (1,896 lb)
  • Powerplant: 1 × Salmson 9Nc radial engine , 101 kW (135 hp)

Performance

  • Maximum speed: 170 km/h (106 mph, 92 kn)
  • Service ceiling: 5,500 m (18,045 ft)

See also edit

Related lists

References edit

  1. ^ Orbis 1985, page 2556

Further reading edit

  • Lacaze, Henri & Lherbert, Claude (2013). Morane Saulnier: ses avions, ses projets [Morane Saulnier: Their Aircraft and Projects] (in French). Outreau, France: Lela Presse. ISBN 978-2-914017-70-1.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.

morane, saulnier, primary, training, monoplane, designed, built, france, morane, saulnier, 315morane, saulnier, 317role, primary, trainernational, origin, francemanufacturer, morane, saulnierfirst, flight, 1932primary, user, french, forcenumber, built, 356deve. The Morane Saulnier MS 315 was a primary training monoplane designed and built in France by Morane Saulnier MS 315Morane Saulnier MS 317Role Primary trainerNational origin FranceManufacturer Morane SaulnierFirst flight 1932Primary user French Air ForceNumber built 356Developed from Morane Saulnier MS 300 Contents 1 Development 2 Variants 3 Operators 4 Specifications MS 315 5 See also 6 References 7 Further readingDevelopment editThe MS 315 was developed from the earlier MS 300 primary trainer and related variants and first flew in October 1932 The MS 315 is a parasol wing monoplane with a tailskid with divided main landing gear and powered by a 135 hp 101 kW Salmson 9Nc radial engine A production run of 346 aircraft followed the four prototypes including 33 built after the Second World War Five high powered MS 317 2 variants were also produced for the civil market and a single MS 316 was built powered by a Regnier inverted Vee engine In the 1960s 40 MS 315 used as civil glider tugs were modified with a 220 hp 164 kW Continental W670 K radial engine and re designated the MS 317 Variants editMS 315 Production version with a 135hp 101kW Salmson 9Nc radial engine 350 built MS 315 2 Higher powered civil version five built MS 316 Variant powered by a Regnier inverted Vee engine one built MS 317 1960s conversions with a 220hp 164kW Continental W670 K radial engine 40 converted Operators edit nbsp FranceFrench Air Force French Navy nbsp PeruPeruvian Air ForceSpecifications MS 315 editData from 1 General characteristicsCrew 2 Length 7 60 m 24 ft 11 25 in Wingspan 12 00 m 39 ft 4 5 in Height 2 80 m 9 ft 2 25 in Wing area 21 60 m2 232 51 sq ft Empty weight 548 kg 1 208 lb Gross weight 860 kg 1 896 lb Powerplant 1 Salmson 9Nc radial engine 101 kW 135 hp Performance Maximum speed 170 km h 106 mph 92 kn Service ceiling 5 500 m 18 045 ft See also editRelated lists List of Interwar military aircraft List of military aircraft of FranceReferences edit Orbis 1985 page 2556Further reading edit nbsp Wikimedia Commons has media related to Morane Saulnier MS 317 Lacaze Henri amp Lherbert Claude 2013 Morane Saulnier ses avions ses projets Morane Saulnier Their Aircraft and Projects in French Outreau France Lela Presse ISBN 978 2 914017 70 1 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions The Illustrated Encyclopedia of Aircraft Part Work 1982 1985 Orbis Publishing Retrieved from https en wikipedia org w index php title Morane Saulnier MS 315 amp oldid 1152443073, wikipedia, wiki, book, books, library,

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