COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT. ENGINE INLET ANTI-ICING PERFORMANCE SPECIFICATION.

Abstract

This specification describes the engine inlet anti-icing system and establishes its requirements, and testing objectives. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be determined after prototype flight testing.

Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1965
Accession Number
AD0804413

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

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

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow