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Zanzottera MZ 201

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Adapted from the English Wikipedia article Zanzottera MZ 201, available under CC BY-SA 4.0Updated 29 November 20255 sources
Fiate Aviation Co., Ltd.
IndustryAircraft engine manufacturing
Headquarters
Hefei
,
China


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The Zanzottera MZ 201 and MZ 202 represent a series of twin-cylinder, in-line two-stroke, dual ignition aircraft engines tailored for ultralight aircraft and motor glider applications.[1][2][3]

Initially engineered and manufactured by Italy-based Zanzottera Technologies, the entire lineup of two-stroke ultralight aircraft engines, including these models, was later transferred in ownership to Compact Radial Engines located in Surrey, British Columbia, Canada.[3] Subsequently, in August 2017, Fiate Aviation Co., Ltd., headquartered in Hefei, Anhui, China, acquired Compact Radial Engines.[4]

Development

The MZ 202 was first introduced as a lightweight powerplant delivering approximately 60 hp (45 kW), designed to compete with the liquid-cooled 64 hp (48 kW) Rotax 582. Following this, the MZ 201 emerged as a de-rated version producing around 45 hp (34 kW), intended primarily for motorgliders and single-seat ultralight aircraft requiring greater output than the single-cylinder Zanzottera MZ 34.[1][2][3]

Both the MZ 201 and MZ 202 utilize cylinder barrels coated with Nikasil, sharing identical bore and stroke dimensions with the single-cylinder MZ 34. The MZ 201 can be equipped with either a recoil starter or electric start system, whereas the MZ 202 is exclusively fitted with electric starting. Regarding reduction drives, the MZ 201 offers a choice between a belt-driven or gearbox reduction system, while the MZ 202 is supplied only with a gearbox featuring selectable reduction ratios of 2.18:1, 2.55:1, 2.88:1, 3.11:1, or 3.66:1.[1][2][3][5]

The engine's user manual explicitly outlines the inherent design limitations:

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Variants

MZ 201
A twin-cylinder, air-cooled, two-stroke aircraft engine featuring dual ignition, delivering 45 hp (34 kW). It is specifically designed for motorgliders and single-seat ultralight aircraft. This model utilizes a single Tillotson carburetor.
MZ 202
An air-cooled, twin-cylinder, two-stroke engine with dual ignition, producing 60 hp (45 kW). It comes equipped with two Bing carburetors.
MZ 202i
This version is a twin-cylinder, air-cooled, two-stroke engine with dual ignition, generating 67 hp (50 kW). It features electronic fuel injection managed by an advanced computerized engine control system. Production of this model has been discontinued.

Applications

MZ 201
MZ 202

Specifications (MZ 202)

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See also

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References

  1. ↑ 1.0 1.1 1.2 Cite error: Invalid <ref> tag; no text was provided for refs named Cliche
  2. ↑ 2.0 2.1 2.2 Cite error: Invalid <ref> tag; no text was provided for refs named CRE201
  3. ↑ 3.0 3.1 3.2 3.3 Cite error: Invalid <ref> tag; no text was provided for refs named CRE202
  4. ↑ Cite error: Invalid <ref> tag; no text was provided for refs named Fiate
  5. ↑ Cite error: Invalid <ref> tag; no text was provided for refs named MZ202Manual

External links

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