SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III. BOEING MODEL 2707. ENGINE INLET ANTI-ICING SUBSYSTEM SPECIFICATION,

Abstract

This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the Inlet Anti-icing Subsystem (hereinafter called IAIS), for the prototype model supersonic transport airplane. Differences between the prototype and the production airplanes are described.

Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1966
Accession Number
AD0827602

Entities

People

  • J. N. R. Hall

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Fixed Wing Aircraft
  • Jet Aircraft
  • Models
  • Production
  • Prototypes
  • Qualifications
  • Specifications
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering

Technology Areas

  • Hypersonics