Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
MS.130 · Length
Single source6.97 m (22 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | Morane-Saulnier MS.130 | Morane-Saulnier MS.230 |
|---|---|---|
| Type | Military trainer[source] | Elementary Trainer[source] |
| National origin | France[source] | — |
| Manufacturer | Morane-Saulnier[source] | Morane-Saulnier[source] |
| Primary user | French Navy[source] | Armée de l'Air Flight School, Reims, France |
6.942 m (22 ft 9 in)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | >150[source] | 1000+[source] |
|---|
| First flight | 1925[source] | February 1929[source] |
|---|
| Fuel capacity | — | 220 L (58 US gal; 48 imp gal) jettison-able fuselage tank with a 22 L (5.8 US gal; 4.8 imp gal) centre-section gravity tank[source] |
|---|
| Propellers | — | 2-bladed fixed-pitch wooden propeller[source] |
|---|
| Never exceed speed | — | 260 km/h (160 mph, 140 kn)[source] |
|---|
| Time to altitude | — | 3,000 m (9,800 ft) in 11 minutes 18 seconds[source] |
|---|
| Wing loading | — | 61.3 kg/m 2 (12.6 lb/sq ft)[source] |
|---|
| Power/mass | — | 0.1429 kW/kg (0.0869 hp/lb)[source] |
|---|
| Reported operators |
| — |
|---|