Accession Number:

AD0827450

Title:

SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III. BOEING MODEL 2707. AIR INDUCTION SUBSYSTEM SPECIFICATION,

Descriptive Note:

Corporate Author:

BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV

Personal Author(s):

Report Date:

1966-12-31

Pagination or Media Count:

79.0

Abstract:

This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the air induction subsystem for the prototype-model supersonic transport airplane. Differences between the prototype and production airplanes are described. The air induction subsystem shall provide the engine with the quantity of air demanded at high-pressure recovery within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem. The installation of the subsystem is defined by specification D6A10113-1. Four independent subsystems are required per airplane.

Subject Categories:

  • Civilian Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE