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)
Commercial Supersonic Transport Program. Phase II-C. Interim Aircraft Performance Assessment Report. Air Induction Control System Performance Specification
1965
17 pages
Report
Keine Angabe
Englisch