COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT. ENVIRONMENTAL CONTROL SYSTEM PERFORMANCE SPECIFICATION.

Abstract

This specification describes the environmental control system and establishes its requirements and testing objectives. The system shall comply with Federal Aviation Agency requirements and shall consist of the following major subsystems: Air Conditioning, Windshield Rain Removal, Anti-Icing and Antifogging, and Oxygen. System performance requirements are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing.

Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1965
Accession Number
AD0804421

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

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

Fields of Study

  • Physics

Readers

  • Software Engineering
  • Surface Coatings Technology.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow