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

Abstract

This specification establishes preliminary performance, design, and construction requirements applicable to the inertial navigation system for the supersonic transport. The requirements will be updated as the ARINC inertial navigation system characteristic is developed. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of the 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
AD0804438

Entities

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Flight Testing
  • Inertial Navigation
  • Inertial Navigation Systems
  • Navigation
  • Prototypes
  • Specifications
  • Supersonic Transport Aircraft
  • Transport Ships

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Inertial Navigation Systems.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow