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

Abstract

This specification describes the system and establishes the testing requirements for the air induction hydraulic and control system. In the remainder of this document, the air induction system will be referred to as inlet system. 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 established after prototype flight testing. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1965
Accession Number
AD0804449

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

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

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow