Author: John T. Dorsey
Publisher:
ISBN:
Category : Brakes
Languages : en
Pages : 36
Book Description
Structural Performance of Two Aerobrake Hexagonal Heat Shield Panel Concepts
Author: John T. Dorsey
Publisher:
ISBN:
Category : Brakes
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Brakes
Languages : en
Pages : 36
Book Description
Structural Performance of Two Aerobrake Hexagonal Heat Shield Panel Concepts
Author: John T. Dorsey
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Structural Performance of Two Aerobrake Hexagonal Heat Shield Panel Concepts
Author: National Aeronautics and Space Adm Nasa
Publisher:
ISBN: 9781728937212
Category :
Languages : en
Pages : 34
Book Description
Structural sizing and performance are presented for two structural concepts for an aerobrake hexagonal heat shield panel. One concept features a sandwich construction with an aluminum honeycomb core and thin quasi-isotropic graphite-epoxy face sheets. The other concept features a skin-rib isogrid construction with thin quasi-isotropic graphite-epoxy skins and graphite-epoxy ribs oriented at 0, ]60, and -60 degs along the panel. Linear static, linear bifurcation buckling, and nonlinear static analyses were performed to compare the structural performance of the two panel concepts and assess their feasibility for a lunar transfer vehicle aerobrake application. Dorsey, John T. and Dyess, James W. Langley Research Center RTOP 506-43-41-02...
Publisher:
ISBN: 9781728937212
Category :
Languages : en
Pages : 34
Book Description
Structural sizing and performance are presented for two structural concepts for an aerobrake hexagonal heat shield panel. One concept features a sandwich construction with an aluminum honeycomb core and thin quasi-isotropic graphite-epoxy face sheets. The other concept features a skin-rib isogrid construction with thin quasi-isotropic graphite-epoxy skins and graphite-epoxy ribs oriented at 0, ]60, and -60 degs along the panel. Linear static, linear bifurcation buckling, and nonlinear static analyses were performed to compare the structural performance of the two panel concepts and assess their feasibility for a lunar transfer vehicle aerobrake application. Dorsey, John T. and Dyess, James W. Langley Research Center RTOP 506-43-41-02...
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 212
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1194
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1194
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1644
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1644
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938
Book Description
Minimum Accommodation for Aerobrake Assembly. Phase 2: Structural Concepts for a Lunar Transfer Vehicle Aerobrake which Can be Assembled on Orbit
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
The 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum: 93-1370 - 93-1445
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 700
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 700
Book Description