| 词条 | SAIMAN 202 | |||||||||||||||
| 释义 |
The SAIMAN 202 was a 1930s Italian two-seat cabin monoplane designed and built by the Società Industrie Meccaniche Aeronautiche Navali (SAIMAN). DevelopmentDesigned in response to an Italian Air Ministry requirement for a two-seat cabin monoplane, the SAIMAN 202 prototype (registered I-BOTT) first flew in early 1938. The 202 was a low-wing cantilever monoplane with a fixed tailwheel landing gear. It had a nose-mounted 120 hp (74 kW) de Havilland Gipsy Major engine. An enclosed cockpit had side-by-side seating for two. The first production aircraft were for civilian use with Italian training organisations and designated SAIMAN 202bis. The 202bis had only minor cabin changes but the next variant (the 202/I) was a major re-design with an improved fuselage re-positioned tailplane. To compete in a 1939 touring aircraft rally two special aircraft were developed; a 202 RL with an Alfa Romeo 110 engine which were now standard for the civilian production aircraft, and the 204 R which was a four-seater with lengthened cabin and longer nose and powered by an Alfa Romeo 115 engine. Operational historyTo meet an urgent operational requirement for military trainers, the Regia Aeronautica ordered a simplified version of the 202 RL as the 202/M in October 1939. CNA built 85, SACA built 65 and SAIMAN built 215 aircraft for the Regia Aeronautica flying schools. Aircraft were also used for liaison duties and Italian Air Attaches. A number of aircraft were captured. Variants
Prototype with 120hp (74kW) de Havilland Gipsy Major engine.
Civil production aircraft
Improved version
One special variant for rally use.
Military production aircraft, 365 built.
One four-seat variant for rally use. Operators
Specifications{{aerospecs|ref=[4] |met or eng?=met |crew=2 |capacity= |length m=7.65 |length ft=25 |length in=1¼ |span m=10.66 |span ft=34 |span in=11¾ |swept m= |swept ft= |swept in= |rot number= |rot dia m= |rot dia ft= |rot dia in= |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m=1.91 |height ft=6 |height in=3¼ |wing area sqm=17.66 |wing area sqft=190.10 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=670 |empty weight lb=1477 |gross weight kg=930 |gross weight lb=2050 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Alfa Romeo 110-1 inline piston engine |eng1 kw=89 |eng1 hp=120 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh=220 |max speed mph=137 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=600 |range miles=373 |endurance h= |endurance min= |ceiling m=5050 |ceiling ft=16,570 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent|see also= |related= |similar aircraft= |sequence= |lists=* List of aircraft of World War II }} References{{commons category|Saiman 202}}1. ^aeroflight 2. ^ 3. ^aeroflight 4. ^Orbis 1985, p 2838
5 : Italian civil utility aircraft 1930–1939|Italian military trainer aircraft 1930–1939|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1938 |
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