USE OF STRUCTURAL CARBON HEAT SINK BRAKES ON AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

15-11-2016

Publisher

SAE International

RATIONALE
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS

The purpose of this document is to relate areas where carbon brake technology may differ from traditional steel brake technology in design and performance.

Committee	A-5A
DocumentType	Standard
Pages	8
PublisherName	SAE International
Status	Current
Supersedes	SAE AIR 1934 : 1996

SAE ARP 5632 : 2016

ROTORCRAFT: APPLICATION OF EXISTING AIRCRAFT DESIGNED TIRES, WHEELS AND BRAKES

SAE ARP 1493 : 2013	WHEEL AND BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT
MIL-B-8584 Revision C:1970	BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
SAE AIR 4762 : 2016	COMPILATION OF FREEZING BRAKE EXPERIENCE AND POTENTIAL DESIGNS AND OPERATING PROCEDURES TO PREVENT ITS OCCURRENCE
MIL-W-5013 Revision L:1991	WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR

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SAE AIR 1934 : 2016

USE OF STRUCTURAL CARBON HEAT SINK BRAKES ON AIRCRAFT

Table of Contents

Abstract

General Product Information

Standards Referenced By This Book

Standards Referencing This Book

Category

Subcategory