COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT. FLIGHT INSTRUMENTATION PERFORMANCE SPECIFICATION.

Abstract

This specification establishes the design, construction, performance requirements, and test objectives of the flight instrumentation equipment for the Model 733 supersonic transport. This specification covers the following flight instrumentation equipment: Attitude director indicator; Horizontal situation indicator; Flight director computer; Comparator warning and approach gate monitor; Approach progress annunciator; Radio magnetic indicator; Standby attitude/heading indicator; Radio altimeter; and Radar altitude/vertical speed indicator. 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
AD0804441

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airplanes
  • Altimeters
  • Altitude
  • Flight Instruments
  • Flight Testing
  • Heading Indicators
  • Horizontal Situation Indicators
  • Indicators
  • Instrumentation
  • Radar Altimeters
  • Radio Altimeters
  • Supersonic Transport Aircraft
  • Telemetry Equipment
  • Vertical Speed Indicators

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Geodesy
  • Software Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow