Morane-Saulnier MS.755 Fleuret

Airplanes

Length

9.7 m

Flat Wing Span

9.56 m

Height

2.73 m

Flat Wing Area

18 m²

Flat Wing Aspect Ratio

5.12

Max Speed

720 km/h

Max Ceiling

12000 m

Number of Engines

Aircraft Engine

First Flight

1953-01-29

Number Built

Maximum Take-Off Weight

3.05 t (paragliders: kg)

Total Fuel Capacity

680

Maximum Range

725 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Morane-Saulnier MS.755 Fleuret	3.05	680	725

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Cessna T-37 Tweet	Teledyne CAE J69	8.8392	10.0584		Compare
Mikoyan-Gurevich MiG-9		9.75	10		Compare
Akaflieg Berlin B9	Hirth HM 500	9.06	9.4		Compare
Morane-Saulnier MS.760 Paris		10.05	10.15	2	Compare
Convair Model 48 Charger	Pratt & Whitney Canada PT6	10.3632	9.144	6	Compare
Focke-Wulf F 19 Ente		10.53	10		Compare

All data (21 fields)

Name: Morane-Saulnier MS.755 Fleuret
Manufacturer: Morane-Saulnier
Description: The Morane-Saulnier MS.755 Fleuret was a prototype French two-seat jet trainer designed and built by Morane-Saulnier.
First Flight: 1953-01-29
Designer: Morane-Saulnier
Length (m): 9.7
Height (m): 2.73
Cockpit Crew: 2
Max Speed (km/h): 720
Max Ceiling (m): 12000
Rate of Climb (m/s): 16.9977
Armament: 2× 7.5mm machine guns in nose; 2× 50 kg bombs; 4× 3.5 in rockets
National Origin: France
Number Built: 1
Powerplant Description: 2 × Turbomeca Marboré II turbojets
Wikipedia Article (URL): en.wikipedia.org/wiki/Morane-Saulnier_MS.755_Fleuret
Flat Wing Span (m): 9.56
Flat Wing Area (m²): 18
Flat Wing Aspect Ratio: 5.12
Aircraft Engine: Turbomeca Marboré
Number of Engines: 2