Morane-Saulnier MoS-50: Difference between revisions
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{{More citations needed|date=August 2017}} |
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{{Infobox aircraft |
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|name=MoS-50 |
|name=MoS-50 |
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|image=Morane-Saulnier MS 50C (MS-52) K-SIM 02.jpg |
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|image= |
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|caption=Morane-Saulnier MS 50C at Aviation Museum of Central Finland |
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|caption= |
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}}{{Infobox Aircraft Type |
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|type=Trainer aircraft |
|type=Trainer aircraft |
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|manufacturer=[[Morane-Saulnier]] |
|manufacturer=[[Morane-Saulnier]] |
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|designer= |
|designer= |
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|first_flight= |
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|first flight= |
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|introduction=1924 |
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|retired=1930s |
|retired=1930s |
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|status= |
|status= |
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|primary_user=[[French Air Force]] |
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|more_users=[[Finnish Air Force]]<br>[[Turkish Air Force]] |
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|produced= |
|produced= |
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|number_built= |
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|number built= |
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|unit cost= |
|unit cost= |
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|developed_from= |
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|developed from= |
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|variants |
|variants= |
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'''Morane-Saulnier MoS-50''' (also '''MS.50''') was a [[France|French]] trainer aircraft of parasol type from 1924. The twin-seat monoplane aircraft was of wooden construction. It was one of the last aircraft to have a rotary engine - a 130 hp [[Clerget]] 9B. |
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'''Morane-Saulnier MoS-50''' (also '''MS.50''') was a French [[Parasol wing|parasol configuration]] |
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In 1925, six MS.50Cs were sold to Finland, where they were used as trainers until 1932. It was very popular in service. Five aircraft of the modified type MS.53 were sold to Turkey. |
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trainer aircraft built in 1924. The twin-seat aircraft was of wooden construction and was one of the last aircraft to have a [[rotary engine]], a {{convert|130|hp|kW|abbr=on|order=flip}} [[Clerget 9B]]. |
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In 1925 six MS.50Cs were sold to Finland, where they were used as trainers until 1932. It was very popular in service. Five aircraft of the modified MS.53 type were sold to Turkey. |
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==Versions== |
==Versions== |
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[[File:Morane_Saulnier_MS.122_L'Aérophile-Salon1926.jpg|thumb|Morane Saulnier MS.122 photo from L'Aérophile-Salon1926]] |
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; Morane-Saulier M.S.50 |
; Morane-Saulier M.S.50 |
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: Three seat prototype, powered by a {{convert|120|hp|kW|abbr=on|order=flip}} [[Salmson 9AC|Salmson AC9]] 9-cylinder [[radial engine]].<ref name=Lailes1/> |
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: Two-seat primary trainer aircraft. Also known as the '''M.S.50C'''. |
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; M.S.50C |
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: Two-seat primary trainer aircraft powered by a {{convert|130|hp|kW|abbr=on|order=flip}} [[Clerget 9B]] rotary engine. |
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: Powered by a 180-hp (134-kW) [[Hispano-Suiza 8a]]b 8-cylinder piston engine. Only three were built. |
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; |
;M.S.51 |
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: Powered by a {{convert|180|hp|kW|abbr=on|order=flip}} [[Hispano-Suiza 8a]]b V-8 cylinder piston engine. Only three were built. |
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: Improved version. |
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;M.S.53 |
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: Improved version of M.S.51, with same engine.<ref name=Lailes2/> |
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;M.S.120 |
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:M.S.53 with a {{convert|230|hp|kW|abbr=on|order=flip}} [[Salmson]] engine.<ref name=Lailes2/> |
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==Survivors== |
==Survivors== |
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The only preserved aircraft of this type is at the [[Aviation Museum of Central Finland]]. |
The only preserved aircraft of this type is at the [[Aviation Museum of Central Finland]].<ref name=Ogden/> |
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==Operators== |
==Operators== |
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;{{FRA}}: [[French Air Force]] |
;{{FRA}}: [[French Air Force]]{{citation needed|date=April 2017}} |
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;{{FIN}}: [[Finnish Air Force]] |
;{{FIN}}: [[Finnish Air Force]] |
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;{{TUR}}: [[Turkish Air Force]] |
;{{TUR}}: [[Turkish Air Force]] |
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==Specifications ( |
==Specifications (MS 50C)== |
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[[File:Moraine_Saulnier_MoS.53_3-view_Les_Ailes_May_27,_1926.png|thumb|Morane-Saulnier MoS.53 3-view drawing from Les Ailes May 27, 1926]] |
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{{Aircraft specs |
{{Aircraft specs |
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|ref=Thulinista Hornettiin |
|ref=Thulinista Hornettiin<ref name=TH/> |
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|prime units?=met |
|prime units?=met |
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<!-- |
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|upper span m= |
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|upper span ft= |
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|upper span in= |
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|upper span note= |
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|mid span m= |
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|mid span ft= |
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|mid span in= |
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|mid span note= |
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|lower span m= |
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|lower span ft= |
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|lower span in= |
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|lower span note= |
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|swept m=<!-- swing-wings --> |
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|swept ft=<!-- swing-wings --> |
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|swept in=<!-- swing-wings --> |
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|swept note= |
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|dia m=<!-- airships etc --> |
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|dia ft=<!-- airships etc --> |
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|dia in=<!-- airships etc --> |
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|width m=<!-- if applicable --> |
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|width ft=<!-- if applicable --> |
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|width in=<!-- if applicable --> |
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|width note= |
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|height m=3.1 |
|height m=3.1 |
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|height ft= |
|height ft= |
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|wing area sqft= |
|wing area sqft= |
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|wing area note= |
|wing area note= |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|swept area note= |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|volume note= |
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|aspect ratio=<!-- sailplanes --> |
|aspect ratio=<!-- sailplanes --> |
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|airfoil= |
|airfoil= |
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|max takeoff weight note= |
|max takeoff weight note= |
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|fuel capacity= |
|fuel capacity= |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|lift note= |
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|more general= |
|more general= |
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<!-- |
<!-- |
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|eng1 kw=100 |
|eng1 kw=100 |
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|eng1 hp=<!-- prop engines --> |
|eng1 hp=<!-- prop engines --> |
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|eng1 shp=<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 note= |
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|power original= |
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|thrust original= |
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|eng1 kn-ab=<!-- afterburners --> |
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|eng1 lbf-ab=<!-- afterburners --> |
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|eng2 number= |
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|eng2 name= |
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|eng2 type= |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- prop engines --> |
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|eng2 shp=<!-- prop engines --> |
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|eng2 kn=<!-- jet/rocket engines --> |
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|eng2 lbf=<!-- jet/rocket engines --> |
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|eng2 note= |
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|eng2 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
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|eng3 number= |
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|eng3 name= |
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|eng3 type= |
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|eng3 kw=<!-- prop engines --> |
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|eng3 hp=<!-- prop engines --> |
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|eng3 shp=<!-- prop engines --> |
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|eng3 kn=<!-- jet/rocket engines --> |
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|eng3 lbf=<!-- jet/rocket engines --> |
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|eng3 note= |
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|eng3 kn-ab=<!-- afterburners --> |
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|eng3 lbf-ab=<!-- afterburners --> |
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|more power= |
|more power= |
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|prop blade number= |
|prop blade number=2 |
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|prop name= |
|prop name= |
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|prop dia m=<!-- propeller aircraft --> |
|prop dia m=<!-- propeller aircraft --> |
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|prop dia note= |
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|rot number=<!-- helicopters --> |
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|rot dia m=<!-- helicopters --> |
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|rot dia ft=<!-- helicopters --> |
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|rot dia in=<!-- helicopters --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|rot area note= |
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<!-- |
<!-- |
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Performance |
Performance |
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|max speed kts= |
|max speed kts= |
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|max speed note= |
|max speed note= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh= |
|cruise speed kmh= |
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|cruise speed mph= |
|cruise speed mph= |
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|wing loading lb/sqft= |
|wing loading lb/sqft= |
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|wing loading note= |
|wing loading note= |
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|disk loading kg/m2= |
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|disk loading lb/sqft= |
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|disk loading note= |
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|fuel consumption kg/km= |
|fuel consumption kg/km= |
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|fuel consumption lb/mi= |
|fuel consumption lb/mi= |
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|related= |
|related= |
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|similar aircraft= |
|similar aircraft= |
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|sequence= |
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|lists= |
|lists= |
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* [[List of |
* [[List of interwar military aircraft]] |
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* [[List of military aircraft of France]] |
* [[List of military aircraft of France]] |
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|see also= |
|see also=}} |
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==References== |
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{{reflist|refs= |
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<ref name=TH>{{cite book |title=Thulinista Hornettiin - 75 vuotta Suomen Ilmavoimien koneita|last=Heinonen|first=Timo |year=1992|publisher=Keski-Suomen Ilmailumuseon|isbn=9519568824}}</ref> |
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<ref name=Ogden>{{cite book |title=Aviation Museums and Collections of Mainland Europe |last= Ogden |first=Bob |year=2009|publisher= Air Britain (Historians) Ltd|page=93 |isbn=978 0 85130 418 2}}</ref></ref> |
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<ref name=Lailes1>{{cite journal |last=Serryer |first=J. |date=5 March 1925|title=L'avion Morane, type 50|journal=Les Ailes|issue=194 |pages=2|url=http://gallica.bnf.fr/ark:/12148/bpt6k6568226g/f2 }}</ref> |
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<ref name=Lailes2>{{cite journal |last=Serryer |first=J. |date=20 May 1926|journal=Les Ailes| title=Les avions Morane-Saulnier |issue=257|pages=2–3|url=http://gallica.bnf.fr/ark:/12148/bpt6k65682890/f2}}</ref>}} |
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==Further reading== |
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{{commons category|Morane-Saulnier MS.50}} |
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*{{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}} |
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}} |
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{{Morane-Saulnier aircraft}} |
{{Morane-Saulnier aircraft}} |
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{{Aviation lists}} |
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{{DEFAULTSORT:Morane-Saulnier Mos-50}} |
{{DEFAULTSORT:Morane-Saulnier Mos-50}} |
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[[Category:French military trainer aircraft |
[[Category:1920s French military trainer aircraft]] |
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[[Category: |
[[Category:Parasol-wing aircraft]] |
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[[Category:Single- |
[[Category:Single-engined tractor aircraft]] |
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[[Category:Aircraft first flown in 1924]] |
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[[Category:Morane-Saulnier aircraft]] |
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[[Category:Rotary-engined aircraft]] |
Latest revision as of 02:02, 12 September 2024
This article needs additional citations for verification. (August 2017) |
MoS-50 | |
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General information | |
Type | Trainer aircraft |
Manufacturer | Morane-Saulnier |
Primary users | French Air Force |
History | |
Introduction date | 1924 |
Retired | 1930s |
Morane-Saulnier MoS-50 (also MS.50) was a French parasol configuration trainer aircraft built in 1924. The twin-seat aircraft was of wooden construction and was one of the last aircraft to have a rotary engine, a 97 kW (130 hp) Clerget 9B.
In 1925 six MS.50Cs were sold to Finland, where they were used as trainers until 1932. It was very popular in service. Five aircraft of the modified MS.53 type were sold to Turkey.
Versions
[edit]- Morane-Saulier M.S.50
- Three seat prototype, powered by a 89 kW (120 hp) Salmson AC9 9-cylinder radial engine.[1]
- M.S.50C
- Two-seat primary trainer aircraft powered by a 97 kW (130 hp) Clerget 9B rotary engine.
- M.S.51
- Powered by a 130 kW (180 hp) Hispano-Suiza 8ab V-8 cylinder piston engine. Only three were built.
- M.S.53
- Improved version of M.S.51, with same engine.[2]
- M.S.120
- M.S.53 with a 170 kW (230 hp) Salmson engine.[2]
Survivors
[edit]The only preserved aircraft of this type is at the Aviation Museum of Central Finland.[3]
Operators
[edit]Specifications (MS 50C)
[edit]Data from Thulinista Hornettiin[4]
General characteristics
- Crew: 2
- Length: 7.6 m (24 ft 11 in)
- Wingspan: 11.7 m (38 ft 5 in)
- Height: 3.1 m (10 ft 2 in)
- Wing area: 24 m2 (260 sq ft)
- Max takeoff weight: 860 kg (1,896 lb)
- Powerplant: 1 × Clerget 9B 9-cyl air-cooled rotary piston engine, 100 kW (130 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 170 km/h (110 mph, 92 kn)
- Endurance: 2½ hours
- Service ceiling: 5,500 m (18,000 ft)
- Rate of climb: 2 m/s (390 ft/min)
See also
[edit]Related lists
References
[edit]- ^ Serryer, J. (5 March 1925). "L'avion Morane, type 50". Les Ailes (194): 2.
- ^ a b Serryer, J. (20 May 1926). "Les avions Morane-Saulnier". Les Ailes (257): 2–3.
- ^ Ogden, Bob (2009). Aviation Museums and Collections of Mainland Europe. Air Britain (Historians) Ltd. p. 93. ISBN 978 0 85130 418 2.
- ^ Heinonen, Timo (1992). Thulinista Hornettiin - 75 vuotta Suomen Ilmavoimien koneita. Keski-Suomen Ilmailumuseon. ISBN 9519568824.
Further reading
[edit]Wikimedia Commons has media related to Morane-Saulnier MS.50.
- 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.