Supersonic Transport Program. Phase II-C Report. Aircraft Engine Installation. Subsystem Specification. SST Boeing Model 2707

Abstract

This specification establishes the requirements for performance, design, test and qualification for the Aircraft engine Installation Subsystem. The subsystem is used to provide the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem is also used to provide mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem requires fuel, air flow, electrical and airframe support and control inputs for its operation. These are provided by the airframe fuel, air inlet, air inlet control, electrical, flight control, and airframe structure subsystems.

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Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1966
Accession Number
AD0805654

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Airframes
  • Control Systems
  • Detection
  • Detectors
  • Engine Mounts
  • Engineering
  • Exhaust Nozzles
  • Fire Extinguishers
  • Fire Protection
  • Fuel Systems
  • Governments
  • Horizontal Stabilizers
  • Ignition
  • Ignition Systems
  • Jet Aircraft
  • Safety
  • Supersonic Transport Aircraft
  • Test And Evaluation
  • Test Methods

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerospace Test and Evaluation
  • Combustion and Flow Dynamics.
  • Robotics and Automation.

Technology Areas

  • Hypersonics