Morane-Saulnier MS.140: Difference between revisions

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{{single source|date=January 2021}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
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{|{{Infobox Aircraft Begin
{|{{Infobox aircraft begin
| name=MS.140
| name = MS.140
| image = Morane-Saulnier MS.140 side L'Aéronautique March,1928.jpg
| image=
| caption=
| caption =
}}{{Infobox Aircraft Type
}}{{Infobox aircraft type
| type=[[Air ambulance]]/[[Training aircraft]]
| type = [[Air ambulance]]/[[Training aircraft]]
| national origin=[[France]]
| national origin = [[France]]
| manufacturer=[[Morane-Saulnier]]
| manufacturer = [[Morane-Saulnier]]
| designer=
| designer =
| first flight=c.1927
| first flight = c.1927
| introduced=
| introduced =
| retired=
| retired =
| status=
| status =
| primary user=
| primary user =
| more users= <!--Limited to three in total; separate using <br /> -->
| more users = <!--Limited to three in total; separate using <br /> -->
| produced= <!--years in production-->
| produced = <!--years in production-->
| number built=1
| number built = 1
| program cost= <!--Total program cost-->
| program cost = <!--Total program cost-->
| unit cost= <!--Incremental or flyaway cost for military or retail price for commercial aircraft-->
| unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft-->
| developed from=
| developed from =
| variants with their own articles=
| variants with their own articles =
}}
}}
|}
|}
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For a 1927 design it was backward looking, particularly in it use of a [[rotary engine]], an 80&nbsp;hp (60&nbsp;kW) [[Le Rhône 9]]C. It had an all wood structure with [[aircraft fabric covering|fabric covering]]. The MS.140 was a [[Wing configuration#Wing support|single bay biplane]] with wings of equal span but [[sweepback]] on the upper wing only. The bays were defined by pairs of parallel [[interplane strut]]s. On each side a shorter pair of struts ran from the upper [[fuselage]] to the upper wing and another pair from the upper fuselage to the lower wing immediately above the attachment point of the main landing leg. The [[conventional landing gear|conventional undercarriage]] had a wide track, with single wheels on a split axle formed from V-shaped struts hinged at the fuselage lower centreline. The fuselage was square sided with a rounded decking, the pilot sitting below a cut-out in the upper wing for upward visibility. The engine was cowled.<ref name=Howson/>
For a 1927 design it was backward looking, particularly in it use of a [[rotary engine]], an 80&nbsp;hp (60&nbsp;kW) [[Le Rhône 9]]C. It had an all wood structure with [[aircraft fabric covering|fabric covering]]. The MS.140 was a [[Wing configuration#Wing support|single bay biplane]] with wings of equal span but [[sweepback]] on the upper wing only. The bays were defined by pairs of parallel [[interplane strut]]s. On each side a shorter pair of struts ran from the upper [[fuselage]] to the upper wing and another pair from the upper fuselage to the lower wing immediately above the attachment point of the main landing leg. The [[conventional landing gear|conventional undercarriage]] had a wide track, with single wheels on a split axle formed from V-shaped struts hinged at the fuselage lower centreline. The fuselage was square sided with a rounded decking, the pilot sitting below a cut-out in the upper wing for upward visibility. The engine was cowled.<ref name=Howson/>


The MS.140 had a generous wing area, giving it a low [[wing loading]] of about 25&nbsp;kg/m³ (5&nbsp;lb/ft<sup>2</sup>). Combined with a high lift [[airfoil]] section, this gave it the ability to operate from very small fields.<ref name=Howson/>
The MS.140 had a generous wing area, giving it a low [[wing loading]] of about 25&nbsp;kg/m<sup>3</sup> (5&nbsp;lb/ft<sup>2</sup>). Combined with a high lift [[airfoil]] section, this gave it the ability to operate from very small fields.<ref name=Howson/>


==Operational history==
==Operational history==


Only one MS.140 was built and there are few reports of its history. It was noted in the [[Villacoublay]] aircraft "graveyard" in 1937 and may have been sold to the [[Second Spanish Republic|Republicans]] at the start of the [[Spanish Civil War]] with others from that store.<ref name=Howson/>
Only one MS.140 was built and there are few reports of its history. It was noted in the [[Vélizy – Villacoublay Air Base|Villacoublay]] aircraft "graveyard" in 1937 and may have been sold to the [[Second Spanish Republic|Republicans]] at the start of the [[Spanish Civil War]] with others from that store.<ref name=Howson/>
<!-- ==Variants== -->
<!-- ==Units using this aircraft/Operators (choose)== -->


==Specifications==
==Specifications==
[[File:Morane_Saulnier_MS.140_3-view_Les_Ailes_February_2,_1928.png|thumb|Morane Saulnier MS.140 3-view drawing from Les Ailes February 2, 1928]]
{{Aircraft specs
{{Aircraft specs
|ref=Howson<ref name=Howson/>
|ref=''Howson'' <ref name=Howson/>
|prime units?=met
|prime units?=met
<!--
<!--
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|wing area sqft=
|wing area sqft=
|wing area note=
|wing area note=
|aspect ratio=<!-- give where relevant eg sailplanes -->
|aspect ratio=<!-- give where relevant e.g. sailplanes -->
|airfoil=
|airfoil=
|empty weight kg=610
|empty weight kg=610
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|climb rate note=
|climb rate note=
|time to altitude=
|time to altitude=
|wing loading kg/m2
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading lb/sqft=
|wing loading note=
|wing loading note=
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{{reflist|refs=
{{reflist|refs=


<ref name=Howson>{{cite book |title= Aircraft of the Spanish Civil War|last=Howson|first=Gerald| year=1990|volume=|publisher=Putnam Aeronautical Books|location=London |isbn=0 85177 842 9|pages=240}}</ref>
<ref name=Howson>{{cite book |title= Aircraft of the Spanish Civil War|last=Howson|first=Gerald| year=1990|publisher=Putnam Aeronautical Books|location=London |isbn=0-85177-842-9|pages=240}}</ref>}}


⚫
==Further reading==
}}
{{commons category|Morane-Saulnier MS.140}}
⚫
<!-- ==Further reading== -->
*{{cite book |last1=Lacaze |first1=Henri |last2=Lherbert |first2=Claude |title=Morane Saulnier: ses avions, ses projets |date=2013 |publisher=Lela Presse |location=Outreau, France |isbn=978-2-914017-70-1 |language=fr|name-list-style=amp|trans-title=Morane Saulnier: Their Aircraft and Projects}}
<!-- ==External links== -->

<!-- Navboxes go here -->


{{Morane-Saulnier aircraft}}
{{Morane-Saulnier aircraft}}
{{Aviation lists}}


[[Category:Morane-Saulnier aircraft|MS.140]]
[[Category:Morane-Saulnier aircraft|MS.140]]
[[Category:French military utility aircraft 1920–1929]]
[[Category:1920s French military utility aircraft]]
[[Category:French military trainer aircraft 1920–1929]]
[[Category:1920s French military trainer aircraft]]
[[Category:Biplanes]]
[[Category:Aircraft first flown in 1927]]
[[Category:Rotary-engined aircraft]]

Latest revision as of 18:21, 4 July 2023

MS.140
Role Air ambulance/Training aircraft
National origin France
Manufacturer Morane-Saulnier
First flight c.1927
Number built 1

The Morane-Saulnier MS.140 was designed in France as an ambulance aircraft with the ability to operate from small fields and which could double as a trainer. Only one of these single engine, wooden biplanes was built, first flying about 1927.

Design and development[edit]

The MS.140 was designed as an ambulance aircraft, with a hatch behind the pilot into which a stretcher could be slid. For maximum utility a second seat with dual control could be fitted instead, the aircraft then able to perform as a trainer.[1]

For a 1927 design it was backward looking, particularly in it use of a rotary engine, an 80 hp (60 kW) Le Rhône 9C. It had an all wood structure with fabric covering. The MS.140 was a single bay biplane with wings of equal span but sweepback on the upper wing only. The bays were defined by pairs of parallel interplane struts. On each side a shorter pair of struts ran from the upper fuselage to the upper wing and another pair from the upper fuselage to the lower wing immediately above the attachment point of the main landing leg. The conventional undercarriage had a wide track, with single wheels on a split axle formed from V-shaped struts hinged at the fuselage lower centreline. The fuselage was square sided with a rounded decking, the pilot sitting below a cut-out in the upper wing for upward visibility. The engine was cowled.[1]

The MS.140 had a generous wing area, giving it a low wing loading of about 25 kg/m3 (5 lb/ft2). Combined with a high lift airfoil section, this gave it the ability to operate from very small fields.[1]

Operational history[edit]

Only one MS.140 was built and there are few reports of its history. It was noted in the Villacoublay aircraft "graveyard" in 1937 and may have been sold to the Republicans at the start of the Spanish Civil War with others from that store.[1]

Specifications[edit]

Morane Saulnier MS.140 3-view drawing from Les Ailes February 2, 1928

Data from Howson [1]

General characteristics

  • Capacity: 1
  • Length: 7.43 m (24 ft 5 in)
  • Wingspan: 11.1 m (36 ft 5 in)
  • Height: 3.13 m (10 ft 3 in)
  • Wing area: 35 m2 (380 sq ft)
  • Empty weight: 610 kg (1,345 lb)
  • Gross weight: 864 kg (1,905 lb)
  • Powerplant: 1 × Le Rhône 9C 9-cylinder rotary engine, 60 kW (80 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 131 km/h (81 mph, 71 kn)

References[edit]

  1. ^ a b c d e Howson, Gerald (1990). Aircraft of the Spanish Civil War. London: Putnam Aeronautical Books. p. 240. ISBN 0-85177-842-9.

Further reading[edit]

Wikimedia Commons has media related to Morane-Saulnier MS.140.
  • 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.
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