Dornier Do 132
__NOTOC__
{{Infobox Aircraft Begin
|name=Do 132 |image=File:Dornier Do 132 mock up.jpg |caption=Do 132 mockup }}{{Infobox Aircraft Type |type=Utility helicopter |manufacturer=Dornier |designer= |first flight= |introduced= |retired= |status=Canceled project |primary user= |more users= |produced= |number built= |variants with their own articles= }} |
The Dornier Do 132 was a utility helicopter under development in Germany in the late 1960s. While the design was a conventional pod-and-boom layout, the propulsion system was unusual in that it used a turbine engine, not to drive the rotor directly, but to provide a source of hot gas that was fed through the rotor shaft, along the blades, and out through tip jets. The intention was to eliminate the weight and mechanical complexity of a gearbox and an anti-torque system for the tail.
This engine system underwent extensive static tests while a full-size mockup was built to prove the aerodynamics in a wind tunnel. Ultimately, however, the programme was cancelled in 1971 before a prototype was actually constructed.
Specifications (as designed)
{{Aircraft specs
|ref=Jane's All the World's Aircraft 1969–70Taylor 1969, p. 92.
|prime units?=met
|genhide=
|crew=1
|capacity=4 passengers
|length m=7.50
|length ft=
|length in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=2.80
|height ft=
|height in=
|empty weight kg=675
|empty weight lb=
|gross weight kg=1430
|gross weight lb=
|max takeoff weight kg=1650
|max takeoff weight lb=
|more general=
|eng1 number=1
|eng1 name=Pratt & Whitney Canada PT6-A20
|eng1 type=gas generator
|eng1 kw=
|eng1 hp=
|eng1 shp=720
|eng1 kn=
|eng1 lbf=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|more power=
|rot number=1
|rot dia m=10.70
|rot dia ft=
|rot dia in=
|rot area sqm=89.9
|rot area sqft=
|perfhide=
|max speed kmh=229
|max speed mph=
|max speed kts=
|cruise speed kmh=221
|cruise speed mph=
|cruise speed kts=
|range km=450
|range miles=
|range nmi=
|endurance=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|lift to drag=
|disk loading kg/m2=
|disk loading lb/sqft=
|more performance=
|avionics=
}}
{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}
References
{{commons category}}
{{reflist}}
- {{cite book|editor-last=Taylor|editor-first=John W. R.|title=Jane's All the World's Aircraft 1969–70|year=1969|publisher=Sampson Low Marston & Co. Ltd.|location=London}}
- {{cite book|last=Taylor|first=Michael J. H.|title=Jane's Encyclopedia of Aviation|year=1989|publisher=Studio Editions|location=London|pages=331}}
- [http://www.eads-nv.com/800/en/eads/history/airhist/1960_1969/dornier_do132_1969.html EADS website]{{Dead link|date=July 2019 |bot=InternetArchiveBot |fix-attempted=yes }}
{{Dornier aircraft}}
Category:1960s German civil utility aircraft
Category:1960s German helicopters
Category:Single-turbine helicopters
Category:Tipjet-powered helicopters
Category:Single-rotor helicopters
Category:Aircraft with skid landing gear
{{Aero-1960s-stub}}