Curti Zefhir

 

A two-seat ultralight helicopter meant for recreational or training flights. This aircraft is unique as it is the only helicopter to feature a ballistic parachute, which is located above the main rotor.

 

 

Attribution
Overview
Parent type *No Type assigned
Variant *No Variant assigned
Design authority Curti Aerospace
Primary manufacturer Curti Aerospace
Key Characteristics
Operational status In development
Max gross weight (ground)   388 700 kg 1,543 lb
Crew 1-2
Seating arrangement Side-by-side
Configuration
VTOL type Helicopter
Compound type None
Lift configuration Single main rotor
Control device type Tail rotor
Features
Number of engines 1
Number of propulsors 0
Number of lift devices 1
Number of control devices 1

Curti Zefhir

 

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Curti Zefhir

 

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Curti Zefhir

 

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Curti Zefhir

 

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Curti Zefhir

 

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Curti Zefhir

 

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Curti Zefhir

 

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Articles from the Journal of the American Helicopter Society related to the Curti Zefhir

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Articles from NASA Technical Reports Server related to the Curti Zefhir

 

Patent information from the US Patent and Trademark Office related to the Curti Zefhir

 

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Curti Zefhir

 

Overview

 

 

Layout

 

 

Main rotor

 

 

Curti Zefhir

Aircraft Notes

Ref. Author(s) Title Source Date Type
388 Curti Aerospace Zefhir Brochure http://www.zefhir.eu/pdf/Zefhir-helicopter-brochure-2018.pdf?utm_source=pdf_download&utm_medium=pdf_onsite&utm_campaign=zefhir_sito July 9, 2018 Website
390 PBS Aerospace Turbshaft engine PBS TS100 https://www.pbs.cz/en/our-business/aerospace/aircraftgines/turboshaftgine-pbs-ts100 July 9, 2018 Website
391 PBS Aerospace Turboshaft egnine PBS TS100 https://www.pbs.cz/en/our-business/aerospace/aircraftgines/turboshaftgine-pbs-ts100 July 9, 2018 Website