Tentative Airworthiness Standards for Supersonic Transports, November 1, 1965 PDF Download
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Author: United States. Flight Standards Service
Publisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 210
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Book Description
Author: United States. Flight Standards Service
Publisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 210
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Book Description
Author: Richard H. Sawyer
Publisher:
ISBN:
Category : Air traffic control
Languages : en
Pages : 98
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Book Description
Author: Milton D. McLaughlin
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 44
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 554
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Book Description
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 826
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1076
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Book Description
Author: Planning Research Corporation
Publisher:
ISBN:
Category : Air traffic control
Languages : en
Pages : 238
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Book Description
Author: Robert G. Thomson
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 44
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Book Description
Author: C. Thomas Snyder
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 84
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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.
