Accession Number:

AD0804413

Title:

COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT. ENGINE INLET ANTI-ICING PERFORMANCE SPECIFICATION.

Descriptive Note:

Complete revision.

Corporate Author:

BOEING CO RENTON WA

Personal Author(s):

Report Date:

1965-11-15

Pagination or Media Count:

13.0

Abstract:

This specification describes the engine inlet anti-icing system and establishes its requirements, and testing objectives. 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 determined after prototype flight testing.

Subject Categories:

  • Civilian Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE