SAE AIR1603-1993 PDF

Scope: This document provides a brief description of the auxiliary power equipment that is available with enough description and pertinent comments to enable an engineer to make logical preliminary selection of the appropriate equipment for advanced military aircraft programs. The information has been kept as brief as possible to include the maximum amount of equipment in a relatively short document. It is not intended to replace textbook design analysis or detailed information available from the equipment suppliers. The document describes auxiliary power equipment. Auxiliary power is defined as follows: those elements of secondary power (defined as all aircraft nonpropulsive power generation and transmission) related to main engine bleed air and shaft power extraction or power generation separate from the main engines. Included are engine bleed air systems, remote engine driven gearboxes, engine starting systems, auxiliary power units, and emergency power systems. Additional definitions may be found in ARP906A which is the source of this definition. Some closely related systems which are not discussed in detail, include thermal management, environmental control, electrical, and hydraulic systems.

SAE AIR1603-1993 Referenced Document

SAE AIR1174 INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS
SAE AIR1467A-1989 Gas Energy Limited Starting Systems
SAE AIR781-1962 Guide for Determining Engine Starter Drive Torque Requirements
SAE AIR944 PNEUMATIC POWER SUPPLIES FOR STARTING AIRCRAFT
SAE ARP906 GLOSSARY, AIRCRAFT ENGINE STARTING SYSTEMS
SAE ARP949 TURBINE ENGINE STARTING SYSTEM DESIGN REQUIREMENTS*， 1994-09-01 Update
SAE AS1606-1992 Gas Turbine Starter (Jet Fuel Starter) Specification
SAE AS943 STARTER, PNEUMATIC, AIRCRAFT ENGINE, GENERAL SPECIFICATION FOR

1993 SAE AIR1603-1993 Auxiliary Power System Considerations for Advanced Military Aircraft