| 词条 | Morane-Saulnier P | ||||||||||||||||
| 释义 |
The Morane-Saulnier Type P (official designations MS.21, MS.24 and MS.26) was a French parasol wing two-seat reconnaissance aeroplane of the First World War. Morane-Saulnier built 595 for the French air force, and it was also used by the British until 1916-17. DevelopmentIn addition to being fitted with ailerons and having a more streamlined fuselage, the Type P was faster and better armed than its better known ancestor, the Type L (MS.3) and had a more developed structure compared to the intermediate Morane-Saulnier LA (MS.4). Three versions were built under Morane-Saulnier's factory designation of Type P, the first being the MS.21, which although externally similar to the Type LA, had its internal structure completely redesigned, with the most visible evidence being the more robust center section struts, and with other details borrowed from the Type N (MS.5), such as a substantial spinner, known as the "casserole". The MS.24 was built specifically for the Royal Flying Corps to operate alongside their Morane-Saulnier LAs while replacing those lost to attrition, but due to shortages of the {{convert|110|hp|abbr=on}} Le Rhône rotary engine used in the MS.21, it was powered by an {{convert|80|hp|abbr=on}} Le Rhône. The RFC also operated the MS.21. The MS.26 was similar to the MS.21, but was fitted with a {{convert|120|hp|abbr=on}} Le Rhône engine which was enclosed in a full cowling, and like the 24, dispensed with the spinner commonly found on the MS.21. Variants
Operators
Specifications (Type P/MS.21){{Aircraft specifications|plane or copter?=plane |jet or prop?=prop |ref=The Aeroplanes of the Royal Flying Corps (Military Wing)[1] |crew=two |capacity= |payload main= |payload alt= |length main= 7.2 m |length alt= 23 ft 7⅜ in |span main= 11.2 m |span alt= 36 ft 8⅞ in |height main= 3.47 m |height alt= 11 ft 4⅝ in |area main=18 m² |area alt=194 sq ft |airfoil= |empty weight main=433 kg |empty weight alt=953 lb |loaded weight main= 733 kg |loaded weight alt= 1,613 lb |useful load main= |useful load alt= |max takeoff weight main= |max takeoff weight alt= |more general= |engine (prop)= Le Rhone 9J |type of prop=rotary engine |number of props=1 |power main= 82 kW |power alt= 110 hp |power original= |max speed main=156 km/h |max speed alt= 97 mph |max speed more=at 2,000 m (6,560 ft) |cruise speed main= |cruise speed alt= |stall speed main= |stall speed alt= |never exceed speed main= |never exceed speed alt= |range main= |range alt= |endurance=2½ hours |ceiling main= 4,800 m |ceiling alt= 15,740 ft |climb rate main= |climb rate alt= |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance=*Climb to 3,000 m (9,840 ft): 15 min 50 s |guns=1 × Vickers machine gun and 1× Lewis gun or 2× Lewis guns |bombs=Light load of bombs |avionics= }} See also{{Aircontent||related=
|similar aircraft= |lists=
|see also= }} References{{commons category|Morane-Saulnier P}}Citations1. ^Bruce 1982, p. 312. Bibliography
6 : French military reconnaissance aircraft 1910–1919|Morane-Saulnier aircraft|Parasol-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1914|Rotary-engined aircraft |
||||||||||||||||
| 随便看 |
|
开放百科全书收录14589846条英语、德语、日语等多语种百科知识，基本涵盖了大多数领域的百科知识，是一部内容自由、开放的电子版国际百科全书。