SAE AIR 1667 : 2013

Table of Contents

1. SCOPE
2. REFERENCES
3. ELECTROTHERMAL ICE PROTECTION SYSTEMS
4. DESIGN CONSIDERATIONS
5. TEST CONSIDERATIONS
6. NOTES
APPENDIX A - OTHER ICE PROTECTION CONCEPTS
APPENDIX B - RATE OF ICE COLLECTION
APPENDIX C - SURFACE EQUILIBRIUM (DATUM)
             TEMPERATURE MODEL

Abstract

Summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection systems.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	AC-9C