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
Structural Performance of Two Aerobrake Hexagonal Heat Shield Panel Concepts
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722809362
Category :
Languages : en
Pages : 32
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: Createspace Independent Publishing Platform
ISBN: 9781722809362
Category :
Languages : en
Pages : 32
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
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