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Title
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Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
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Date
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1966
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Index Abstract
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Coming Soon
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Photo Quality
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Not Needed
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Report Number
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AFFDL TR 66-25
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Corporate Author
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Air Force Flight Dynamics Laboratory
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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54
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Identifier
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AD0633677
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Access Rights
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Distribution of this document is unlimited
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Distribution Classification
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1
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Contract
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Laboratory Research - No Contract
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DoD Project
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1368
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DoD Task
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136804
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Abstract
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A qualitative review of fundamental relationships involved in ablation engineering and aerodynamic heating is presented. This document is written for rapid reading with the primary purpose of introducing the technical area to engineers, scientists, and management personnel associated with but not intimately working in hypervelocity thermal protection.
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Report Availability
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Full text available
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Date Issued
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1966-04
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Provenance
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource
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Creator
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Achard, Robert T.