| Download | - View final version: De-icing flight tests on an ALOUETTE III helicopter during the season 1965-1966 (PDF, 7.3 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40004030 |
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| Author | Search for: Price, R. D.1 |
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| Affiliation | - National Research Council Canada. National Aeronautical Establishment
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| Format | Text, Technical Report |
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| Physical description | 22 p. |
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| Abstract | Flight tests were performed in an icing cloud on a Sud-Aviation Alouette III helicopter equipped with electrothermal rotor blade de-icing. The de-icing system operated satisfactorily down to the minimum ambient temperature experienced during the trials. Modifications to the engine inlet anti-icing system proved satisfactory. The Alouette III helicopter powered by the Artouste IIIB engine is now considered satisfactory for operation in icing down to a temperature of -25°C. |
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| Date published | 1966-06 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 3d8e5275-652c-48a5-a3f5-8800f5325195 |
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| Record created | 2026-05-07 |
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| Record modified | 2026-05-07 |
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