Author: United States. Flight Standards ServicePublisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 210
Book Description
Tentative Airworthiness Standards for Supersonic Transports, November 1, 1965
Author: United States. Flight Standards ServicePublisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 210
Book Description
Simulation Studies of the Supersonic Transport in Future Air Traffic Control Systems
Author: Richard H. SawyerPublisher:
ISBN:
Category : Air traffic control
Languages : en
Pages : 98
Book Description
Simulator Investigation of Maneuver Speed Increases of an SST Configuration in Relation to Speed Margins
Author: Milton D. McLaughlinPublisher:
ISBN:
Category : Air speed
Languages : en
Pages : 44
Book Description
NASA Technical Note
Author: NASA Technical Paper
Author: NASA Technical Memorandum
Author: Monthly Catalog of United States Government Publications
Author: Economic Implications of a United States Supersonic Transport Aircraft Upon Airports and Enroute Support Services
Author: Planning Research CorporationPublisher:
ISBN:
Category : Air traffic control
Languages : en
Pages : 238
Book Description
An Analytical Evaluation of the Denting of Airplane Surfaces by Hail
Author: Robert G. ThomsonPublisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 44
Book Description
Takeoff Certification Considerations for Large Subsonic and Supersonic Transport Airplanes Using the Ames Flight Simulator for Advanced Aircraft
Author: C. Thomas SnyderPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 84
Book Description
Data for use in development of takeoff airworthiness standards for new aircraft designs such as the supersonic transport (SST) and the large wide-body subsonic jet transport are provided. An advanced motion simulator was used to compare the performance and handling characteristics of three representative large jet transports during specific flight certification tasks. Existing regulatory constraints and methods for determining rotation speed were reviewed, and the effects on takeoff performance of variations in rotation speed, pitch attitude, and pitch attitude rate during the rotation maneuver were analyzed. A limited quantity of refused takeoff information was obtained. The aerodynamics, wing loading, and thrust-to-weight ratio of the subject SST resulted in takeoff speeds limited by climb (rather than lift-off) considerations. Take-off speeds based on U.S. subsonic transport requirements were found unacceptable because of the criticality of rotation-abuse effects on one-engine-inoperative climb performance. Adequate safety margin was provided by takeoff speeds based on proposed Anglo-French supersonic transport (TSS) criteria, with the limiting criterion being that takeoff safety speed be at least 1.15 times the one-engine-inoperative zero-rate-of-climb speed. Various observations related to SST certification are presented.