Morane-Saulnier MS.130

MS.129 and MS.130–MS.136

Role	Military trainer
National origin	France
Manufacturer	Morane-Saulnier
First flight	1925
Primary user	Frency Navy
Number built	>150

The Morane-Saulnier MS.129 and its derivatives in the MS.130 series were a family of military trainer aircraft produced in France in the 1920s.^[1]^[2] They were conventional, parasol-wing monoplanes with open cockpits in tandem and fixed tailskid undercarriage. The initial version, the MS.129, was produced in small numbers for the Romanian Air Force and civil users, but the major production version was the MS.130, which equipped the French Navy and a number of foreign air arms.^[1]^[2]

The second MS.130 prototype won the 1929 Coupe Michelin, flown by Michel Detroyat with an average speed of 190 km/h (120 mph).^[2]^[3]

The MS.130 was further developed as the MS.230, and at least two MS.130s were later rebuilt to this new standard.^[4]

Variants

MS.129 - initial production version with Hispano-Suiza 8Ab engine
MS.130 - major production version with Salmson 9AB engine
MS.131 - MS.130 converted to use a Lorraine engine (1 converted for US military attaché in Paris)
MS.132 - version with Salmson 7Ac engine for French Navy (5 built)
MS.133 - version with Gnome-Rhône 5Kc engine (3 converted from MS.129, 1 converted from MS.130)
MS.134 - conversion of MS.130 with Clerget 9B engine
MS.136 - conversion of MS.130 with Salmson 9AC engine

The MS.137, MS.138, and MS.139 were of a different design, and not related to the MS.130.^[4]

Operators

France France
- Aéronavale (MS.130)
- Aéronautique Militaire (MS.130)
Brazil Brazil (15 × MS.130)
- Brazilian Air Force
- Varig (MS.130)
Belgium Belgium (2 × MS.130)
China (MS.130)
Guatemala (MS.130)
Portugal
- Portuguese Air Force
Romania (MS.129)
Turkey (MS.130)

Specifications (MS.130)

Data from The Illustrated Encyclopedia of Aircraft 2554

General characteristics

Crew: Two, pilot and instructor
Length: 6.97 m (22 ft 10 in)
Wingspan: 10.70 m (35 ft 1 in)
Height: 2.85 m (9 ft 4 in)
Wing area: 19.7 m² (212 ft²)
Empty weight: 793 kg (1,740 lb)
Gross weight: 1,149 kg (2,528 lb)
Powerplant: 1 × Salmson 9Ab, 170 kW (230 hp)

Performance

Maximum speed: 208 km/h (130 mph)
Range: 510 km (320 miles)
Service ceiling: 5,000 m (16,000 ft)

Notes

1 2 Taylor 1989, 685
1 2 3 The Illustrated Encyclopedia of Aircraft 2553
↑ "The Michelin Cup", 223
1 2 The Illustrated Encyclopedia of Aircraft 2554

References

Wikimedia Commons has media related to Morane-Saulnier MS.130.

The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing.
"The Michelin Cup". Flight: 623. 8 July 1932. Retrieved 2008-11-14.
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. ISBN 0-7106-0710-5.

Aircraft produced by Morane-Saulnier

Designation Letters	A B C F G GA GB H I L LA M N Nm O P S T TRK U V WR Y AC AE AF AFH AI AN/ANB/ANR/ANL/ANS AR AS BB BH

Numerical Sequence	MoS.1 MoS.2 MoS.3 MoS.4 MoS.5 MoS.6 MoS.7 MoS.8 MoS.9 MoS.10 MoS.13 MoS.21 MoS.22 MoS.23 MoS.25 MoS.26 MoS.27 MoS.28 MoS.29 MoS.30 MoS.31 MoS.32 MoS.33 MoS.34 MoS.35 MoS.42 MoS.43 MoS.50 MoS.51 MoS.53 MoS.121 MoS.129 MoS.130 MoS.131 MoS.132 MoS.133 MoS.134 MoS.136 MoS.137 MoS.138 MoS.139 MoS.140 MoS.141 MoS.147 MoS.148 MoS.149 MoS.152 MS.180 MS.181 MoS.185 MS.200 MS.221 MS.222 MS.223 MS.224 MS.225 MS.226 MS.227 MS.229 MS.230 MS.250 MS.251 MS.275 MS.278 MS.300 MS.301 MS.302 MS.315 MS.316 MS.317 MS.325 MS.340 MS.341 MS.342 MS.343 MS.345 MS.350 MS.405 MS.406 MS.408 MS.410 MS.411 MS.430 MS.433 MS.435 MS.450 MS.470 MS.472 MS.474 MS.470 MS.475 MS.476 MS.477 MS.479 MS.500 MS.501 MS.502 MS.504 MS.505 MS.506 MS.560 MS.570 MS.603 MS.700 MS.701 MS.703 MS.704 MS.730 MS.731 MS.732 MS.733 MS.755 MS.760 MS.880 MS.1500

Names & Nicknames	Alcyon Borel Bullet Criquet Epervier Fleuret Monococque Paris Pétrel Rallye Vanneau

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