Accession Number : AD0804452

Title :   COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT) AIR INDUCTION SYSTEM PERFORMANCE SPECIFICATION.

Corporate Author : BOEING CO RENTON WA

Report Date : 15 NOV 1965

Pagination or Media Count : 15

Abstract : The specification describes and establishes the requirements and testing objectives for the air induction (inlet) system. Performance requirements established herein are design objectives to be applied to prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author)

Descriptors :   (*TURBOJET INLETS, VARIABLE AREA NOZZLES), PERFORMANCE(ENGINEERING), RELIABILITY, PRESSURE.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE