2 prototypes, designed by Cantinieau, were actually built at the SNCAN workshops in France for Aerotécnica. Anti-torque control was provided through a gas ejection outlet at the end of the tail boom with deflectors that could control the direction of thrust.

Source: ”Helicopters & Autogyros of the World”, Paul Lambermont with Anthony Pirie, Second edition 1970, Cassell & Company Ltd, SBN 304 93390 2

Overview

Data on design, manufacture and status

Design authority: Aerotécnica

Primary manufacturer: Aerotécnica

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Thruster

Crew required: 1 in Other arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

Resources related to the AC-13 , provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.
Images from the VFS Gallery
Enter a search term in the box above.

Related Public Resources

Resources related to the AC-13 , provided by public sources across the internet.

Images