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词条 Zenair CH 150
释义

  1. Development

  2. Specifications Zenair CH-150

  3. See also

  4. Notes

  5. References

  6. External links

name=CH 150 image= caption=

}}{{Infobox Aircraft Type

type=Homebuilt light aircraft national origin=Canada manufacturer=Zenair designer=Chris Heintz first flight=1980 introduced=1980 retired= status= primary user= more users= produced= number built= program cost= unit cost= developed from= Zenair CH 100 variants with their own articles=
}}

The Zenith CH 150 Acro Zenith is a Canadian single-engine, low wing, all-aluminum aircraft designed by Chris Heintz and produced by Zenair in kit form for amateur construction. The aircraft is intended for aerobatic use and was introduced at the Experimental Aircraft Association convention in 1980.[1][2]

The CH 150 is one of only six amateur-built aircraft types specifically approved by Transport Canada for aerobatics, without other restrictions.[3]

Development

After emigrating to Canada and setting up Zenair to sell plans and kits for amateur construction of his Zenith two seat-light aircraft, the German aircraft designer Chris Heintz started design of a smaller, single seat development of the Zenith, the Zenair CH 100 Mono-Zenith. The first CH 100 made its maiden flight on 8 May 1975, powered by a 55 hp (41 kW) Volkswagen air-cooled engine of 1600 cc.[4] Heintz used the Mono-Zenith as a starting point to develop a single-seat aircraft for aerobatic training and competition flying, the resulting aircraft, the CH 150 Acro-Zenith making its maiden flight on 19 May 1980. It was designed to be powered by engines of between 100–180 hp (75–134 kW) and had a tailwheel undercarriage instead of the nosewheel undercarriage of the earlier aircraft.[4] Zenair continued to produce kits until 1988.[4]

In a 1983 advertisement Zenair described the design goals of the CH150:

{{quotation|A dandy little aircraft for the serious student in aerobatics. The Acro Zenith has strength for learning and competition (+/-12G). Light on the controls and beautiful to fly. Discover how it does things best - Lady flyers especially will find its roll and pitch forces easy on the arms. Approved for all aerobatic maneuvres - fully inverted system. Suitable for engines from 115 to 180 HP to give marvelous inexpensive flying to any aerobatic pilot.[2] }}

Specifications Zenair CH-150

{{Aircraft specs
|ref=Jane's All The World's Aircraft 1982–83[5]
|prime units?=met


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|crew=1
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|length m=6.17
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|span m=6.15
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|empty weight lb=730
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|max takeoff weight lb=1150
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|eng1 number=1
|eng1 name=Lycoming 0-320
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|eng1 hp=150
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|eng1 note=
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|prop blade number=
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|prop dia m=
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|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=150
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=139
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=48
|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=
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|minimum control speed note=
|range km=
|range miles=760
|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=
|ceiling ft=16000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=2200
|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=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk 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=
}}

See also

{{aircontent
|see also=
|related=*Zenair CH 200
|similar aircraft=
|lists=
}}

Notes

1. ^{{cite journal|magazine=Sport Aviation|author=Jack Cox|date=Oct 1980}}
2. ^Zenair, Zenair pamphlet, circa 1986.
3. ^{{cite web|url = http://www.tc.gc.ca/eng/civilaviation/regserv/cars/part5-standards-a507sd-1833.htm|title = Part V - Standard 507 Appendix D - Standardised Operating Conditions and Limitations - Standard Operating Conditions - Aerobatic Flight Certification|accessdate = 15 August 2010|last = Transport Canada|authorlink = |date=October 1996}}
4. ^Chris Heintz:Light Aircraft Design History {{webarchive |url=https://web.archive.org/web/20110719115519/http://www.zenair-deutschland.de/Downloads/pdf/601-Design-History.pdf |date=July 19, 2011 }}. zenair-deutschland.de. Retrieved 28 February 2010.
5. ^Taylor 1982, p. 494.

References

{{refbegin}}
  • Taylor, John W. R. Jane's All The World's Aircraft 1982-83. London:Jane's Yearbooks, 1982. {{ISBN|0-7106-0748-2}}.
{{refend}}

External links

{{Zenair}}

7 : Canadian sport aircraft 1980–1989|Homebuilt aircraft|Zenair aircraft|Single-engined tractor aircraft|Low-wing aircraft|Aerobatic aircraft|Aircraft first flown in 1980

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