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词条 TNCA Series C
释义

  1. Design

  2. Specifications

  3. References

name= Series C Microplano image= caption=

}}{{Infobox Aircraft Type

type=Single-seat fighter national origin=Mexico manufacturer= Talleres Nacionales de Construcciones Aeronáuticas (TNCA) designer=Guillermo Villasana and Francisco Santarini first flight=c. February 1918 introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The TNCA Series C Microplano was a single-engine, single-seat fighter designed and built in Mexico during World War I.

Design

From 1915 the Talleres Nacionales de Construcciones Aeronáuticas - (National Aeronautical Construction Workshops), sometimes known as the Military Aviation Factory, produced several series of Mexican aircraft. Some of these were based on European designs but others were indigenous. Pressure for local designs and production was increased by the concentration of European manufacturers on war production, in addition to the tensions between Mexico and the United States. In 1917 rights to build Spanish Hispano-Suiza engines was acquired and a factory established.

The Series C Microplano was an unequal span single bay biplane, with wings without sweep or stagger connected by pairs of vertical, parallel interplane struts on each side, the forward ones a little closer to the fuselage. Both wings had constant chord and squared tips. There was a triangular cut-out in the trailing edge of the upper wing to improve the pilot's view.

The Microplano had a flat sided, rectangular section fuselage. The nose housed a 115 kW (157 hp) Hispano-Suiza water-cooled engine, driving a two bladed propeller. Behind the underwing single seat open cockpit the fuselage narrowed strongly in both height and width. Both the near circular rudder and semi-circular tailplane were all-moving. There was a fixed conventional undercarriage with mainwheels on V-form struts, assisted by a tailskid.

Specifications

{{Aircraft specs
|ref=Jane's Fighting Aircraft of World War I
|prime units?=met


|crew=One
|capacity=
|length m=6.60
|length note=
|upper span m=8.00
|upper span note=
|lower span m=6.88
|lower span note=
|height m=2.55
|height note=maximum
|wing area sqm=18
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=460
|empty weight note=
|gross weight kg=650
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Hispano-Suiza
|eng1 type=water-cooled
|eng1 kw=112
|eng1 note=- 119 kW (160 hp)
|power original=
|more power=
|prop blade number=2
|prop name=Anahuac
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=190
|max speed note=to 220 km/h (137 mph; 119 kn)
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
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|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=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
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|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=


|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|other armament=
|avionics=
}}

References


}}

1 : Mexican military aircraft

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