MS.315 - 316 - 317 @·AIRCRAFTUBE

  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • Brussels RMM - MS.315 Brussels RMM - MS.315
    Brussels RMM - MS.315
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • MS.317 - Ferté-Alais 2010 MS.317 - Ferté-Alais 2010
    MS.317 - Ferté-Alais 2010
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • Morane-Saulnier MS.317 Morane-Saulnier MS.317
    Morane-Saulnier MS.317
  • MS.317 - Tannkosh 2011 MS.317 - Tannkosh 2011
    MS.317 - Tannkosh 2011

Morane-Saulnier MS.315, 316, 317

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

Development

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 tailwheel, with divided main landing gear, and powered by a 135hp (101kW) 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 220hp (164kW) Continental W-670K radial engine and re-designated the MS.317.

Variants

  • 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 W-670K radial engine, 40 converted.

Operators

  • French Air Force.
  • French Navy.
  • Peruvian Air Force.

— — — = = — — —

This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Morane-Saulnier MS.315 of Wikipedia ( authors )

Specifications (MS.315)

  • Crew : 2.
  • Length : 7.60 m (24 ft 11¼ in).
  • Height : 2.80 m (9 ft 2¼ in).
  • Wingspan : 12 m (39 ft 4½ in).
  • Wing area : 21.60 m² (232.51 ft²).
  • Empty weight : 548 kg (1208 lb).
  • Gross weight : 860 kg (1896 lb).
  • Maximum speed : 170 km/h (106 mph).
  • Service ceiling : 5500 m (18,045 ft).
  • Powerplant : A Salmson 9Nc radial engine.
  • Power : 101 kW (135 hp).

— — — = = — — —

This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Morane-Saulnier MS.315 of Wikipedia ( authors )
Morane-Saulnier MS.315 - 316 - 317 : Your comments on this subject
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