SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III. BOEING MODEL 2707. STARTING SUBSYSTEM SPECIFICATION

This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test and qualification of the starting subsystem (SS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes ar...

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Bibliographic Details
Main Author: Ort, Grant W
Format: Report
Language:English
Subjects:
AIR TURBINES
AVIATION SAFETY
BOEING 2707 AIRCRAFT
Civilian Aircraft
Combustion and Ignition
COMMERCIAL AIRCRAFT
CONTROL SYSTEMS
ENGINE STARTERS
IGNITION SYSTEMS
INSTRUMENTATION
Jet and Gas Turbine Engines
JET TRANSPORT AIRCRAFT
MAINTAINABILITY
MAINTENANCE
PNEUMATIC EQUIPMENT
RESTARTING
SPECIFICATIONS
STARTING
SUPERSONIC AIRCRAFT
SUPERSONIC TRANSPORTS
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Summary:This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test and qualification of the starting subsystem (SS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The SS provides for starting and windmill braking of the engine, drives the accessory drive subsystem (ADS) and its attached accessories in the engine disconnect mode, and supplies ground source or engine bleed air to the environmental control subsystem (ECS). Partial revision of Rept. no. D6A10490-1.