Morane-Saulnier P.
Morane-Saulnier P. | |
---|---|
Type: | Reconnaissance plane |
Design country: | |
Manufacturer: | |
First flight: |
Late 1915 |
Commissioning: |
1916-17 |
Production time: |
1916 |
Number of pieces: |
565 |
The Morane-Saulnier Type P was an umbrella monoplane developed by the French company Société Anonyme des Aéroplanes Morane-Saulnier , which was used as a reconnaissance aircraft during the First World War .
development
The Type P was the further development of the Morane-Saulnier L and LA models built by Morane-Saulnier, with a more powerful engine, more powerful armament and improved aerodynamics . The slim fuselage with a round cross-section clearly distinguished the aircraft from its predecessor with its box-like fuselage. The wings received ailerons, and the rudder unit was modified. The rotary engine was initially surrounded by a horseshoe-shaped cladding, but was later clad all around the side. The tapered propeller hood typical of Morane aircraft was retained.
commitment
From the beginning of 1916 , the French air force deployed the "Parasol" under the designation MS.21 for the type P with the Le Rhône 9J engine and MS.26 for the Morane Saulnier P with the improved Le Rhône 9Jb engine as a reconnaissance aircraft and light bomber. The British Royal Flying Corps also procured 142 machines; Among other things, Squadrons 1 and 3 used in the Battle of the Somme were equipped with them. The Imperial Russian war air fleet received about ten P-type aircraft, referred to there as Morane IV or Mortschet for short ("Морчет"). These flew in the 19th squadron under Staff Captain Kasakow , later during the Brusilov offensive in his 1st fighter squadron.
The armament usually consisted of a machine gun that was permanently mounted above the wing and fired forward over the propeller, usually a 7.7 mm Vickers or 7.9 mm Hotchkiss machine gun. The Russians also used available machine guns of the Colt and Madsen types . In later series machines, the forward-firing machine gun intended for the pilot was synchronized with the propeller shaft and attached to the fuselage. A second machine gun was placed in the rear seat for the observer. Two aircraft of a single-seat version were tested, but did not go into series production.
The Morane-Saulnier P was not easy to fly, but was popular with experienced pilots. It was used as a two-seat fighter, light bomber and close-up reconnaissance aircraft and, due to its long flight duration, was particularly useful for artillery observation.
After the war, the air forces of Japan and Brazil were also supplied with Morane-Saulnier P.
Morane-Saulnier developed the Type P further to the successor model Morane-Saulnier AR , which was still used as a training aircraft until the 1930s. The Parasol P were withdrawn from the front in 1917, mostly equipped with 80 hp Le Rhône 9C rotary engines and used as training aircraft.
The Morane-Saulnier P in a performance comparison
Surname | country | Motor power | Max. speed | Takeoff weight | Armament | Summit height |
---|---|---|---|---|---|---|
Morane-Saulnier P. | France | 110 hp | 163 km / h | 760 kg | 2 MG, bombs | 4,800 m |
Morane-Saulnier L | France | 80 hp | 123 km / h | 480 kg | 1 MG | 4,700 m |
Morane-Saulnier AR | France | 80 hp | 125 km / h | 764 kg | no | 4,600 m |
Nieuport 12 | France | 110 hp | 144 km / h | 875 kg | 2 MG | 4,300 m |
Sopwith 1½ strutter | United Kingdom | 130 hp | 164 km / h | 975 kg | 2 MG, 100 kg bombs | 3,960 m |
RAFRE8 | United Kingdom | 150 hp | 164 km / h | 1,302 kg | 2-3 MG, 102 kg bombs | 4,115 m |
Roland C.II | German Empire | 160 hp | 165 km / h | 1,284 kg | 2 MG, bombs | 4,000 m |
Rumpler CI | German Empire | 160 hp | 150 km / h | 1.330kg | 1-2, 100 kg bombs | 5,000 m |
Technical specifications
Morane-Saulnier P : | |
Parameter | Data |
---|---|
span | 11.20 m |
Length: | 7.18 m |
Height: | 3.48 m |
Wing area | 18.00 m² |
Empty weight | 433 kg |
Takeoff weight | 730 kg |
engine | 1 × rotary motor Le Rhône 9J , 110 PS (82 kW) |
Armament | 1-2 Lewis or Vickers machine guns , bombs |
Top speed | 163 km / h in NN |
Top speed | 156 km / h at an altitude of 2,000 m |
Climbing time to 2,000m | 7 min 30 s |
Climbing time to 3,000m | 15 min 50 s |
Service ceiling | 4,880 m |
Flight duration | 2 h 30 min |
number of pieces | 565 |
crew | 1 pilot, 1 observer |
References
literature
- Enzo Angelucci, Paolo Matricardi: The planes. From the beginning to the First World War. Falken-Verlag, Wiesbaden 1976, ISBN 3-8068-0391-9 , ( Falken manual in color. )
- JM Bruce: The Airplanes of the Royal Flying Corps (Military Wing). Putnam, London 1982, ISBN 0-370-30084-X .
- Kenneth Munson: Warplanes. Fighter and training aircraft 1914–1919. 2nd revised edition. Orell Füssli Verlag, Zurich 1976, ISBN 3-280-00824-7 , ( Airplanes of the World in Colors. ) Pp. 24, 121–122.
- Heinz Nowarra: The Development of Airplanes 1914–1918. Lehmanns, Munich 1959.
Individual evidence
- ↑ cf. [1] - accessed on January 19, 2012
- ↑ Archived copy ( memento of the original from November 13, 2013 in the Internet Archive ) Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice. - accessed on January 12, 2013
- ↑ cf. Enzo Angelucci, Paolo Matricardi: The planes. From the beginning to the First World War. Falken-Verlag, Wiesbaden 1976, ISBN 3-8068-0391-9 , ( Falken-Handbuch in color. ), P. 131.
- ↑ according to [2] 760 kg - accessed on January 19, 2013
- ↑ [3] - accessed on January 19, 2013
Web links
- [4] Description (French) - accessed January 19, 2013
- [5] Description (Russian) - accessed on January 19, 2013
- [6] Description (Russian) - accessed on January 19, 2013
- [7] Description / color profile - accessed on January 19, 2013
- [8] Description / photo (French) - accessed January 19, 2013
- [9] Description - accessed on January 19, 2013
- [10] Color profile - accessed on January 19, 2013