Fundamental Relationships for Ablation and Hyperthermal Heat Transfer

Item

Title
Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
Date
1966
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AFFDL TR 66-25
Corporate Author
Air Force Flight Dynamics Laboratory
Laboratory
Air Force Flight Dynamics Laboratory
Extent
54
Identifier
AD0633677
Access Rights
Distribution of this document is unlimited
Distribution Classification
1
Contract
Laboratory Research - No Contract
DoD Project
1368
DoD Task
136804
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
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.
Report Availability
Full text available
Date Issued
1966-04
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Creator
Achard, Robert T.