Accession Number : AD0804438

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

Descriptive Note : Complete revision.

Corporate Author : BOEING CO RENTON WA

Report Date : 15 NOV 1965

Pagination or Media Count : 18

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)

Descriptors :   *INERTIAL NAVIGATION, INSTRUMENTATION, SPECIFICATIONS, JET TRANSPORT AIRCRAFT, DIGITAL COMPUTERS, PERFORMANCE(ENGINEERING), DISPLAY SYSTEMS, MAINTAINABILITY, ENVIRONMENTAL TESTS, INTERFACES, MEASUREMENT, ADAPTERS, CONTROL SYSTEMS, POWER.

Subject Categories : Air Navigation and Guidance
      Military Aircraft Operations
      Civilian Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE