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

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.

Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1966
Accession Number
AD0827450

Entities

People

  • L. J. Kimer

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Distortion
  • High Pressure
  • Models
  • Production
  • Prototypes
  • Qualifications
  • Recovery
  • Shape
  • Specifications
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics