Supersonic Transport Development Program. Phase 3. Boeing Model 2707. Aircraft Engine Installation Subsystem Specification

Abstract

This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification for the Aircraft Engine Installation Subsystem (AEIS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described. The subsystem provides the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem also provides mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem contains the engine, exhaust and thrust reverser assembly, engine accessories, engine mounting provisions, engine controls, cowling, bleed air ducting, instrumentation plumbing and wiring.

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Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1966
Accession Number
AD0827436

Entities

People

  • L. G. Dhoors

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircraft Engines
  • Aircrafts
  • Airframes
  • Control Knobs
  • Control Systems
  • Detectors
  • Engineering
  • Failure Mode And Effect Analysis
  • Fuel Systems
  • Ignition
  • Ignition Systems
  • Propulsion Systems
  • Supersonic Transport Aircraft
  • Test And Evaluation
  • Test Methods
  • Thrust Reversal

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering

Technology Areas

  • Hypersonics