Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft PDF Download
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Author: Frank M. Bugg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
Author: Frank M. Bugg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
Author: Frank M. Bugg
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
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Book Description
Author: Paul G. Fournier
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 92
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 518
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Book Description
Author: Michael D. Falarski
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
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Author: Sanger M. Burk
Publisher:
ISBN:
Category : Pilot ejection seats
Languages : en
Pages : 44
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Book Description
A wind-tunnel investigation has been conducted in the Langley full-scale tunnel to determine the static longitudinal and l a t e r a l characteristics of a model of an ejection seat equipped with a rigid-wing recovery system. Several wing and vertical-tail arrangements were tested as well as various configurations of the ejection seat alone, ranging from unfaired to completely faired s e a t s .
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1730
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1062
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1330
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1348
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