Accession Number : AD0804449

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

Corporate Author : BOEING CO RENTON WA

Report Date : 15 NOV 1965

Pagination or Media Count : 17

Abstract : This specification describes the system and establishes the testing requirements for the air induction hydraulic and control system. In the remainder of this document, the air induction system will be referred to as inlet system. 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)

Descriptors :   *TURBOJET INLETS), (*HYDRAULIC EQUIPMENT, CONTROL SYSTEMS, CONTROL PANELS, PERFORMANCE(ENGINEERING).

Subject Categories : Hydraulic and Pneumatic Equipment
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE