Surface Characterization of Candidate Metallic TPS for RLV

Surface Characterization of Candidate Metallic TPS for RLV PDF Author: David A. Stewart
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ISBN:
Category :
Languages : en
Pages :

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Surface Characterization of Candidate Metallic TPS for RLV

Surface Characterization of Candidate Metallic TPS for RLV PDF Author: David A. Stewart
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Surface Catalysis and Characterization of Proposed Candidate Tps for Access-To-Space Vehicles

Surface Catalysis and Characterization of Proposed Candidate Tps for Access-To-Space Vehicles PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722792640
Category :
Languages : en
Pages : 62

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Surface properties have been obtained on several classes of thermal protection systems (TPS) using data from both side-arm-reactor and arc-jet facilities. Thermochemical stability, optical properties, and coefficients for atom recombination were determined for candidate TPS proposed for single-stage-to-orbit vehicles. The systems included rigid fibrous insulations, blankets, reinforced carbon carbon, and metals. Test techniques, theories used to define arc-jet and side-arm-reactor flow, and material surface properties are described. Total hemispherical emittance and atom recombination coefficients for each candidate TPS are summarized in the form of polynomial and Arrhenius expressions. Stewart, David A. Ames Research Center...

33rd Thermophysics Conference

33rd Thermophysics Conference PDF Author:
Publisher:
ISBN:
Category : Thermodynamics
Languages : en
Pages : 418

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International Aerospace Abstracts

International Aerospace Abstracts PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 974

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Surface Catalysis and Characterization of Proposed Candidate TPS for Access-to-Space Vehicles

Surface Catalysis and Characterization of Proposed Candidate TPS for Access-to-Space Vehicles PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 66

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Development of Metallic Thermal Protection Systems for the Reusable Launch Vehicle

Development of Metallic Thermal Protection Systems for the Reusable Launch Vehicle PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Characterization of Metal and Polymer Surfaces

Characterization of Metal and Polymer Surfaces PDF Author: Lieng-Huang Lee
Publisher:
ISBN:
Category : Metals
Languages : en
Pages :

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Reusable Launch Vehicle

Reusable Launch Vehicle PDF Author: National Research Council
Publisher: National Academies Press
ISBN: 0309175860
Category : Science
Languages : en
Pages : 98

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The key to opening the use of space to private enterprise and to broader public uses lies in reducing the cost of the transportation to space. More routine, affordable access to space will entail aircraft-like quick turnaround and reliable operations. Currently, the space Shuttle is the only reusable launch vehicle, and even parts of it are expendable while other parts require frequent and extensive refurbishment. NASA's highest priority new activity, the Reusable Launch Vehicle program, is directed toward developing technologies to enable a new generation of space launchers, perhaps but not necessarily with single stage to orbit capability. This book assesses whether the technology development, test and analysis programs in propulsion and materials-related technologies are properly constituted to provide the information required to support a December 1996 decision to build the X-33, a technology demonstrator vehicle; and suggest, as appropriate, necessary changes in these programs to ensure that they will support vehicle feasibility goals.

Reusable Launch Vehicle

Reusable Launch Vehicle PDF Author: Committee on Reusable Launch Vehicle Technology and Test Program
Publisher: National Academies Press
ISBN: 0309588960
Category : Science
Languages : en
Pages : 99

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Book Description
The key to opening the use of space to private enterprise and to broader public uses lies in reducing the cost of the transportation to space. More routine, affordable access to space will entail aircraft-like quick turnaround and reliable operations. Currently, the space Shuttle is the only reusable launch vehicle, and even parts of it are expendable while other parts require frequent and extensive refurbishment. NASA's highest priority new activity, the Reusable Launch Vehicle program, is directed toward developing technologies to enable a new generation of space launchers, perhaps but not necessarily with single stage to orbit capability. This book assesses whether the technology development, test and analysis programs in propulsion and materials-related technologies are properly constituted to provide the information required to support a December 1996 decision to build the X-33, a technology demonstrator vehicle; and suggest, as appropriate, necessary changes in these programs to ensure that they will support vehicle feasibility goals.

Implementation Plan for the NASA Center of Excellence for Structures and Materials

Implementation Plan for the NASA Center of Excellence for Structures and Materials PDF Author: Charles E. Harris
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 122

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