Morane-Saulnier MS.560: Difference between revisions
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==Specifications (MS.560)== |
==Specifications (MS.560)== |
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{{Aircraft specs |
{{Aircraft specs |
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|ref=<ref name="orbis" />, New French Personal Planes Mark Revival of Tricolor Industry <ref name="av546 p41">Charriou 1946, p. 41.</ref> |
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|ref=<ref name="orbis" /> |
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|prime units?=met |
|prime units?=met |
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|crew=1 |
|crew=1 |
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|capacity= |
|capacity= |
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|length m= |
|length m=7 |
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|length ft= |
|length ft= |
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|length in= |
|length in= |
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|length note= |
|length note= |
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|span m= |
|span m=9 |
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|span ft= |
|span ft= |
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|span in= |
|span in= |
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|span note= |
|span note= |
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|height m=2 |
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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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|dia note= |
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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= |
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|height ft= |
|height ft= |
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|height in= |
|height in= |
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|height note= |
|height note= |
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|wing area sqm= |
|wing area sqm= |
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|wing area sqft= |
|wing area sqft=126.9 |
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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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|empty weight kg= |
|empty weight kg= |
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|empty weight lb= |
|empty weight lb=765 |
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|empty weight note= |
|empty weight note= |
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|gross weight kg= |
|gross weight kg= |
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|gross weight lb= |
|gross weight lb=2170 |
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|gross weight note= |
|gross weight note= |
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|max takeoff weight kg= |
|max takeoff weight kg= |
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|max takeoff weight lb= |
|max takeoff weight lb= |
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|max takeoff weight note= |
|max takeoff weight note= |
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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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|perfhide= |
|perfhide= |
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|max speed kmh= |
|max speed kmh= |
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|max speed mph= |
|max speed mph=145 |
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|max speed kts= |
|max speed kts= |
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|max speed note= |
|max speed note=at {{convert|1640|ft|m|disp=flip|abbr=on}} |
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|max speed mach=<!-- supersonic aircraft --> |
|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=129 |
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|cruise speed kts= |
|cruise speed kts= |
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|cruise speed note= |
|cruise speed note= |
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|minimum control speed note= |
|minimum control speed note= |
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|range km= |
|range km= |
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|range miles= |
|range miles=620 |
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|range nmi= |
|range nmi= |
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|range note= |
|range note= |
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|endurance=<!-- if range unknown --> |
|endurance=<!-- if range unknown --> |
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|ceiling m= |
|ceiling m= |
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|ceiling ft= |
|ceiling ft=22960 |
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|ceiling note= |
|ceiling note= |
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|g limits=<!-- aerobatic --> |
|g limits=<!-- aerobatic --> |
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Revision as of 00:24, 22 February 2016
| MS.560 | |
|---|---|
| Role | Aerobatic monoplane |
| National origin | France |
| Manufacturer | Morane-Saulnier |
| First flight | 1 September 1945 |
| Number built | 3 |
| Variants | Morane-Saulnier MS.570 |
The Morane-Saulnier MS.560 was a French civil aerobatic monoplane designed and built by Morane-Saulnier.[1]
Development
First flown in 1945 the MS.560 was a single-seat low-wing monoplane with a retractable landing gear.[1] Powered by a 75 hp (56 kW) Train 6D-01 piston engine three variants followed all using different engines.[1] In 1946 a two-seat touring variant was produced as the Morane-Saulnier MS.570.[1]
Variants
- MS.560
- Prototype powered by a 75 hp (56 kW) Train 6D-01 engine, one built.[2]
- MS.561
- Variant powered by a 100 hp (75 kW) Mathis G4-Z engine, one built.[2]
- MS.562
- Variant powered by a 100 hp (75 kW) Blackburn Cirrus Minor engine.
- MS.563
- Variant powered by a 100 hp (75 kW) Mathis G4-Z or Walter Minor 4-III engine.
- MS.564
- 1949 variant powered by a Walter Minor 4-III engine, one built.[2]
Specifications (MS.560)
Data from [1], New French Personal Planes Mark Revival of Tricolor Industry [3]
General characteristics
- Crew: 1
- Length: 7 m (23 ft 0 in)
- Wingspan: 9 m (29 ft 6 in)
- Height: 2 m (6 ft 7 in)
- Wing area: 11.79 m2 (126.9 sq ft)
- Empty weight: 347 kg (765 lb)
- Gross weight: 984 kg (2,170 lb)
- Powerplant: 1 × Train 6D-01 piston engine, 56 kW (75 hp)
Performance
- Maximum speed: 233 km/h (145 mph, 126 kn) at 500 m (1,640 ft)
- Cruise speed: 208 km/h (129 mph, 112 kn)
- Range: 1,000 km (620 mi, 540 nmi)
- Service ceiling: 7,000 m (22,960 ft)
References
Wikimedia Commons has media related to Morane-Saulnier.
- Notes
- Bibliography
- Charriou, Marc. "New French Personal Planes Mark Revival of Tricolor Industry". Aviation. Vol. 45, no. 5. pp. 40–42.
{{cite magazine}}: Unknown parameter|registration=ignored (|url-access=suggested) (help) - The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help) - Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing. ISBN 1-85310-194-X.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help)