Accession Number:

AD0804442

Title:

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

Corporate Author:

BOEING CO RENTON WA

Report Date:

1965-11-15

Abstract:

This specification defines preliminary performance, design, and construction requirements applicable to the air data system for the supersonic transport. The air data system is comprised of the following items Pitot-static installation, Total temperature probe, Air data computer, Pressure altitude indicator, Airspeed indicator, Mach number indicator, Total temperature indicator, True airspeed indicator, Static air temperature indicator, and Angle-of-attack sensor. 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

Descriptive Note:

Complete revision.

Pages:

0045

Identifiers:

Communities Of Interest:

Contract Number:

FA-SS-66-5

File Size:

0.00MB

Full text not available:

Request assistance