Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft PDF Download

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Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft

Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft PDF Author: Frank M. Bugg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Book Description

Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft

Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft PDF Author: Frank M. Bugg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Book Description

Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft

Low-speed Tests of an All-flexible Parawing for Landing a Lifting-body Spacecraft PDF Author: Frank M. Bugg
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Low-speed Wind-tunnel Investigation of All-flexible Twin-keel Tension-structure Parawings

Low-speed Wind-tunnel Investigation of All-flexible Twin-keel Tension-structure Parawings PDF Author: Paul G. Fournier
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 92

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 518

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Wind-tunnel Investigation of Several Large-scale All-flexible Parawings

Wind-tunnel Investigation of Several Large-scale All-flexible Parawings PDF Author: Michael D. Falarski
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52

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Wind-tunnel Investigation of Aerodynamic Characteristics of a 1/2-scale Model of an Ejection Seat with a Rigid-wing Recovery System

Wind-tunnel Investigation of Aerodynamic Characteristics of a 1/2-scale Model of an Ejection Seat with a Rigid-wing Recovery System PDF 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 .

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1730

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Government-wide Index to Federal Research & Development Reports

Government-wide Index to Federal Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1062

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Book Description

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1330

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Book Description

Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1348

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Book Description