SIAI-Marchetti SM.101
| {{Infobox Aircraft Begin
|name=SIAI-Marchetti SM.101 |image= |caption= }}{{Infobox Aircraft Type |type=Single-engined transport cabin monoplane |manufacturer=SIAI-Marchetti |designer= |first flight=1947 |introduced= |retired= |status= |primary user= |more users= |produced= |number built=1 |developed from= |variants with their own articles= }} |
The SIAI-Marchetti SM.101 was a 1940s Italian single-engined light transport cabin monoplane designed and built by SIAI-Marchetti.
Development
The SM.101 was a single-engined low-wing cantilever monoplane with a tailwheel landing gear with retractable main gear. It had an enclosed cabin for two crew and six passengers and was powered by a nose-mounted 235 hp (175 kW) Walter Bora radial engine. The prototype and only SM.101 first flew on 20 December 1947 but the company soon decided that a single-engined passenger transport was not likely to sell and the company developed the design with two engines as the SM.102.
Specifications (SM.101)
{{Aircraft specs
|ref=Jane's all the World's Aircraft 1947 {{cite book |title=Jane's all the World's Aircraft 1947 |editor1-last=Bridgman |editor1-first=Leonard |year=1947 |publisher=Sampson Low, Marston & Co |location=London |page=150c}}
|prime units?=met
|crew=2
|capacity=6 passengers
|length m=10.2
|span m=16.5
|height m=3
|wing area sqm=29.91
|aspect ratio=9
|airfoil=
|empty weight kg=1320
|gross weight kg=2190
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Walter Bora
|eng1 type=9-cylinder air-cooled radial engine
|eng1 hp=235
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|max speed kmh=240
|max speed note=at sea level
|cruise speed kmh=225
|cruise speed note= 70% power at {{convert|2750|m|abbr=on}}
- Landing speed: {{convert|75|km/h|mph kn|abbr=on}}
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
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|minimum control speed kts=
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|range km=1250
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=4800
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading kg/m2=73.2
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=12.71 kg/kW (20.9 lb/hp)
|more performance=
|avionics=
}}
See also
References
{{reflist}}
Further reading
- {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }}
- {{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|publisher= Orbis Publishing|pages=2853–4}}
{{Savoia-Marchetti aircraft}}
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Category:Savoia-Marchetti aircraft
Category:1940s Italian civil utility aircraft