- Development and design
- Specifications (SAM-5bis)
- See also
- References Notes Bibliography
| name=Moskalyev SAM-5 | image= | caption= }}{{Infobox Aircraft Type | type=Transport and air ambulance monoplane | national origin=Soviet Union | manufacturer=Moskalyev | designer=Aleksandr Moskalyev | first flight=1930s | introduced= | retired= | status= | primary user= | number built=40 | developed from= | variants with their own articles=
}} |
The Moskalyev SAM-5 was a 1930s Soviet transport or air ambulance monoplane designed by Aleksandr Moskalyev. Development and designThe SAM-5 was a cantilever high-wing monoplane with fixed conventional landing gear and an enclosed cabin for a pilot and four passengers. Moskalyev then worked on an improved variant, the SAM-5-2bis, tested with a 200 hp (149 kW) engine; the aircraft established distance and height records. Specifications (SAM-5bis){{Aircraft specs
|ref=
|prime units?=met
|genhide=
|crew=1
|capacity=3 patients and one attendant
|length m=8.00
|length ft=
|length in=
|length note=approx
|span m=12.50
|span ft=
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=24.00
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=710
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=1219
|max takeoff weight lb=
|max takeoff weight note=
|lift kg=
|lift lb=
|lift note=
|more general=
|eng1 number=1
|eng1 name=Shvetsov M-11
|eng1 type=five-cylinder radial piston engine
|eng1 kw=
|eng1 hp=100
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=173
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|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=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=900
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=2800
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2
|disk loading lb/sqft=
|disk loading note=
|power/mass met=
|power/mass imp=
|power/mass note=
|thrust/weight=
|thrust/weight note=
|more performance=
}}
See also{{aircontent
|see also=
|related=
|similar aircraft=
|sequence=
|lists=- List of aircraft of World War II
}}ReferencesNotesBibliography{{refbegin}}- {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}} 2 : Soviet civil utility aircraft 1930–1939|High-wing aircraft |