COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT) AIR INDUCTION SYSTEM PERFORMANCE SPECIFICATION.

Abstract

The specification describes and establishes the requirements and testing objectives for the air induction (inlet) system. Performance requirements established herein are design objectives to be applied to prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1965
Accession Number
AD0804452

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Fixed Wing Aircraft
  • Flight Testing
  • Induction Systems
  • Jet Aircraft
  • Production
  • Prototypes
  • Specifications
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow