Aestrup-Lavigne Aeroplane: Difference between revisions
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===Performance=== | ===Performance=== | ||
* '''Maximum Speed:''' | * '''Maximum Speed:''' | ||
==See Also== | ==See Also== | ||
[[Category:Acrea]] | [[Category:Acrea]] | ||
Latest revision as of 16:10, 7 October 2021
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| The Aestrup-Lavign Avr. III during testing in January 1903 | |
| Role | Experimental aircraft |
| National origin |  Acrea
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| Designer | Johannes Aestrup Cédric Lavigne |
| First flight | 10 December 1901 |
The Aestrup-Lavigne Aeroplane refers to a series of early, powered heavier-than-air aircraft designed, built, and tested by Johannes Aestrup and Cédric Lavigne in the first years of the 20th century. Developed from their glider which they successfully tested from 1898 to 1900, the aircraft are retrospectively classified as the Avr. I, Avr. II, Avr. III, and Avr. IV.
Design
Specifications
General Characteristics
- Crew: 1
- Length:
- Wingspan:
- Height:
- Wing Area:
- Empty Weight:
- Powerplant:
Performance
- Maximum Speed: