Manzolini Libellula

{{Infobox aircraft

|name = Libellula

|image =

|caption =

|type = Light experimental helicopter

|manufacturer = Manzolini

|designer = Ettore Manzolini

|first_flight = 7 January 1952

|introduction =

|retired =

|status =

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|produced =

|number_built = 3

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}}

The Manzolini Libellula was a 1950s Italian co-axial twin-rotor helicopter designed by Ettore Manzolini. "Libellula" is the Italian word for "Dragonfly".

Design and development

Ettore Manzolini established a company in Rome, Italy to develop a helicopter he had designed. The design was the Manzolini Libellula an unusual co-axial helicopter. The co-axial arrangement eliminating the need for an anti-torque rotor allowed the helicopter to have a twin fin arrangement. The Libellula (Registered I-MANZ) first flew on 7 January 1952. An improved version was the single-seat Libellula II which went on to gain Italian certification on 15 October 1962. A three-seater version (the Libellula III) was built and a four-seat Libellula IV was planned but Manzolini stopped development in the late 1960s.

Variants

;Libellula

:Prototype, one built.

;Libellula II

:Prototype single-seat version powered by a 75kW (101hp) Walter Minor 4-III engine, one built.

;Libellula III

:Prototype two-seat version powered by a 104kW (140hp) Walter M 332 engine, one built but not flown.

;Libellula IV

:Proposed four-seat version powered by a 236kW (317shp) Allison 250-CT18 turboshaft, not built.

Specifications (Libellula II)

{{Aircraft specs

|ref=Jane's All The World's Aircraft 1965–66Taylor 1965, p. 95.

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|capacity=

|length m=4.85

|length ft=

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|empty weight kg=498

|empty weight lb=

|max takeoff weight kg=650

|max takeoff weight lb=

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|eng1 number=1

|eng1 name=Walter Minor 4-III

|eng1 type=air-cooled 4-cylinder inline engine

|eng1 kw=

|eng1 hp=101

|power original=

|more power=

|rot number=2

|rot dia m=9.00

|rot dia ft=

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|rot area sqm=127.2

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|max speed kmh=110

|max speed mph=

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|cruise speed kmh=90

|cruise speed note=(econ cruise)

|range km=200

|range miles=

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|range note=max fuel, 10 min reserve

|endurance=

|ceiling m=2900

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|roll rate=

|climb rate ms=

|climb rate ftmin=780

|lift to drag=

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|avionics=

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{{aircontent|

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References

{{Reflist}}

  • Apostolo, Giorgio. The Illustrated Encyclopedia of Helicopters. New York: Bonanza Books, 1984. Pg.123 {{ISBN|0-517-439352}}.
  • {{cite book|last=Taylor|first=John W. R.|author-link=John W. R. Taylor|title=Jane's All The World's Aircraft 1965–66|year=1965|publisher=Sampson Low, Marston & Co., Ltd.|location=London}}
  • {{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|publisher= Orbis Publishing}}