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Standard

THERMAL ANTI-ICING EQUIPMENT, WING AND EMPENNAGE

1997-08-01
HISTORICAL
AS18607
This specification covers the general requirements for the design, installation, and performance of thermal anti-icing equipment for the wings and empennage surfaces in aircraft.
Standard

SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection

2016-08-29
CURRENT
AIR1168/4B
This section presents the basic equations for computing ice protection requirements for nontransparent and transparent surfaces and for fog and frost protection of windshields. Simplified graphical presentations suitable for preliminary design and a description of various types of ice, fog, frost, and rain protection systems are also presented.
Standard

SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection

2014-01-14
HISTORICAL
AIR1168/4A
This section presents the basic equations for computing ice protection requirements for nontransparent and transparent surfaces and for fog and frost protection of windshields. Simplified graphical presentations suitable for preliminary design and a description of various types of ice, fog, frost, and rain protection systems are also presented.
Standard

Ice, Rain, Fog, and Frost Protection

1989-07-01
HISTORICAL
AIR1168/4
This section presents the basic equations for computing ice protection requirements for nontransparent and transparent surfaces and for fog and frost protection of windshields. Simplified graphical presentations suitable for preliminary design, and a description of various types of ice, fog, frost, and rain protection systems are also presented.
Standard

ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS

1989-10-01
HISTORICAL
AIR1667
This Aerospace Information Report (AIR) identifies and summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection. Although various concepts of ice protection are mentioned in this report, the text is limited generally to those factors associated with design and substantiation of cyclic electrothermal ice protection systems as applicable to the protection of helicopter rotor blades. Other systems are described briefly in Appendix A. Applications consider main rotor blades, conventional tail rotor blades, and other types of antitorque devices. The information contained in this report is also limited to the identification of factors that should be considered and why the factor is important. Specific design, analysis and test methodologies are not included. For additional information refer to the references in Section 7.
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