Morane-Saulnier MS.755 Fleuret: Difference between revisions
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==Specifications== |
==Specifications== |
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{{aerospecs |
{{aerospecs |
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|ref=Jane's All The World's Aircraft 1953–54<ref name="JAWA53p143">Bridgman 1953, p. 143.</ref> |
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|ref= |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met |
|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met |
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|length ft=31 |
|length ft=31 |
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|length in=10 |
|length in=10 |
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|span m= |
|span m=9.56 |
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|span ft= |
|span ft=31 |
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|span in= |
|span in=4 |
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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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|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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|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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| ⚫ | |||
|height ft=8 |
|height ft=8 |
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|height in= |
|height in=11 |
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|wing area sqm= |
|wing area sqm=18.0 |
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|wing area sqft= |
|wing area sqft=194 |
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|swept area sqm=<!-- swing-wings --> |
|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
|swept area sqft=<!-- swing-wings --> |
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|volume m3=<!-- lighter-than-air --> |
|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
|volume ft3=<!-- lighter-than-air --> |
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|aspect ratio=<!-- sailplanes --> |
|aspect ratio=5.12:1<!-- sailplanes --> |
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|empty weight kg= |
|empty weight kg=1,905 |
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|empty weight lb= |
|empty weight lb=4,190 |
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|gross weight kg= |
|gross weight kg=2,650 |
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|gross weight lb= |
|gross weight lb=5,830 |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|eng1 number=2 |
|eng1 number=2 |
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|eng1 kw=<!-- prop engines --> |
|eng1 kw=<!-- prop engines --> |
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|eng1 hp=<!-- prop engines --> |
|eng1 hp=<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines -->3. |
|eng1 kn=<!-- jet/rocket engines -->3.9 |
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|eng1 lbf=<!-- jet/rocket engines --> |
|eng1 lbf=<!-- jet/rocket engines -->880 |
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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 type= |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- 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 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
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|max speed kmh=720 |
|max speed kmh=720 |
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|cruise speed kmh=<!-- if max speed unknown --> |
|cruise speed kmh=<!-- if max speed unknown --> |
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|cruise speed mph=<!-- if max speed unknown --> |
|cruise speed mph=<!-- if max speed unknown --> |
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|range km=725 |
|range km=725{{fact}} |
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|range miles=450 |
|range miles=450 |
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|endurance h=<!-- if range unknown --> |
|endurance h=<!-- if range unknown --> |
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|endurance min=<!-- if range unknown --> |
|endurance min=<!-- if range unknown --> |
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|ceiling m= |
|ceiling m=12,000 |
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|ceiling ft= |
|ceiling ft=39,360 |
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|glide ratio=<!-- sailplanes --> |
|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
|climb rate ms=17 |
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|climb rate ftmin= |
|climb rate ftmin=3,346 |
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|sink rate ms=<!-- sailplanes --> |
|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
|sink rate ftmin=<!-- sailplanes --> |
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Revision as of 18:10, 30 December 2010
| MS.755 Fleuret | |
|---|---|
| Role | Two-seat jet trainer |
| National origin | France |
| Manufacturer | Morane-Saulnier |
| First flight | 29 January 1953 |
| Number built | 1 |
| Developed into | Morane-Saulnier MS.760 Paris |
The Morane-Saulnier MS.755 Fleuret was a prototype French two-seat jet trainer designed and built by Morane-Saulnier. It failed to gain any orders but was developed into the larger four-seat MS.760 Paris.[1]
Development
The Fleuret was designed and built to compete in an order for the French Air Force for a two-seat jet trainer.[2] It was a side-by-side low mid-wing cantilever monoplane with a T-tail and powered by two 800lbf (3.6kn) Turbomeca Marboré II turbojets.[1] The prototype with French test registration F-ZWRS first flew on 29 January 1953.[1] The aircraft was not ordered with the Air Force buying the Fouga Magister instead and only one Fleuret was built.[2]
The Fleuret II an enlarged four-seat development was designed and produced as the MS.760 Paris.[1]
Specifications
Data from Jane's All The World's Aircraft 1953–54[3]
General characteristics
- Crew: 2
- Aspect ratio: 5.12:1
Performance
See also
Related development
Aircraft of comparable role, configuration, and era
References
Notes
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help) - Bridgman, Leonard (1953). Jane's All The World's Aircraft 1953–54. London: Jane's All The World's Aircraft Publishing Company.
- Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing. ISBN 1 85310 104 X.
{{cite book}}: Check|isbn=value: checksum (help); Cite has empty unknown parameter:|coauthors=(help)