Arrow 1 and 2. Flight tests required for stability and control and damper development
Arrow 1 and 2. Flight tests required for stability and control and damper development
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DOI | Resolve DOI: https://doi.org/10.4224/40002206 |
Creator | Search for: ; Search for: |
Format | Text, Technical Report |
Physical description | 1 PDF/A (13 MB), 53 p. |
Subject | Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor |
Publication date | 1959-01 |
Date distributed online | 2021-06-07 |
Publisher | Avro Aircraft Limited (Canada). Engineering Division |
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Note | Publisher is assumed to be "Avro Aircraft Limited (Canada). Engineering Division" by the National Research Council of Canada. Distributed online by the National Research Council of Canada |
Language | English |
Identifier | 71/FAR/23 Issue 2 |
Export citation | Export as RIS |
Collection | Avro Canada CF-105 Arrow |
Record identifier | b63324ad-1de4-4977-b4e6-9d4d1835b463 |
Record created | 2021-06-03 |
Record modified | 2021-06-07 |
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