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词条 CSIR Sara II
释义

  1. Development

  2. Design

  3. Specifications

  4. See also

  5. References

     Notes  Bibliography 
name=SARA II image= caption=

}}{{Infobox aircraft type

type=Two-seat experimental autogyro national origin=South Africa manufacturer=Council for Scientific and Industrial Research designer= first flight=30 November 1972 introduced= retired= status= produced= primary user= number built=1 developed from= variants with their own articles= developed into=
}}

The CSIR SARA II (SARA - South African Research Autogyro) is a South African two-seat experimental autogyro designed and built by the Aeronautics Research Unit of the Council for Scientific and Industrial Research.

Development

As part of the support to South African aircraft manufacturing industry the ARU developed a single-seat autogyro as a research vehicle. Design of the autogyro was started in 1965 and construction followed in April 1967, by 1972 the autogyro, registered ZS-UGL, was ready for tethered tests mounted on a lorry-platform, it made its first free flight on 30 November 1972 at Swartkop Air Force Base. Following the test flights the autogyro was modified.

Design

The autogyro had a box-like fuselage structure made from light-alloy and was fitted with twin fins and rudders with a fixed incidence tail-plane mounted between them. It was fitted with a two-bladed teetering rotor, the rotor could be spun up using a shaft drive through a clutch from the engine. The engine located at the rear was a {{convert|180|hp|kW|0|abbr=on}} Continental O-360-A air-cooled engine driving a two-bladed constant-speed pusher propeller. The crew sat side by side in the enclosed fuselage with dual controls, entrance is through a forward-opening glazed door on each side. The landing gear was a fixed tricycle type with a self-centering and steerable nosewheel.

Specifications

{{Aircraft specs
|ref=[1]
|prime units?=met


|crew=2
|capacity=
|length m=4.65
|length note=fuselage
|height m=
|height note=to top of rotor hub
|width m=1.2
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=840
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|136|l|USgal impgal|abbr=on}}
|more general=


|eng1 number=1
|eng1 name=Lycoming O-360-A
|eng1 type=4-cyl. air-cooled horizontally-opposed piston engine
|eng1 hp=180
|prop blade number=2
|prop name=Hartzell constant-speed propeller
|prop dia m=1.83
|rot number=2
|rot dia m=11.13
|rot area sqm=97.2
|rot area note=NACA 8-H-12 section teetering rotor


|perfhide=
|max speed kmh=154
|cruise speed kmh=122
|cruise speed note=

  • Min flying speed: {{convert|48|kph|abbr=on}}

|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=193
|range km=
|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=4267
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|climb rate ms=4.066
|time to altitude=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|sequence=
|lists=
  • List of rotorcraft

}}

References

Notes

1. ^{{cite book|editor1-last=Taylor|editor1-first=John W.R.|title=Jane's all the world's aircraft, 1975-76|date=1975|publisher=Franklin Watts Inc.|location=New York|isbn=978-0531032503|edition=66th annual}}

Bibliography

{{refbegin}}
  • {{cite book |editor-last= Taylor|editor-first= John W.R. |authorlink= |title= Jane's All the World's Aircraft 1973-74|year= 1973|publisher= Jane's Yearbooks |location=London, United Kingdom|isbn=0-354-00117-5}}
{{refend}}{{Mitsubishi aircraft}}

2 : South African experimental aircraft 1970–1979|Single-engined pusher autogyro

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