Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Aircraft Engine Installation Performance Specification PDF Download
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Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Book Description
This specification describes the aircraft engine installation. The essential physical and functional characteristics are noted and the design requirements are specified in some detail. Ground and flight tests which will ensure that the installation is satisfactory are established. The specific engine installation covered is the GE4/J5G. (Author).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Book Description
This specification describes the aircraft engine installation. The essential physical and functional characteristics are noted and the design requirements are specified in some detail. Ground and flight tests which will ensure that the installation is satisfactory are established. The specific engine installation covered is the GE4/J5G. (Author).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
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Book Description
This specification describes the engine inlet anti-icing system and establishes its requirements, and testing objectives. 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 determined after prototype flight testing.
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
This document describes the performance guarantees for the Boeing Model 733-390 powered by General Electric engines, the Model 733-394 powered by Pratt and Whitney engines, and the 733 prototype airplane.
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 45
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Book Description
This specification defines preliminary performance, design, and construction requirements applicable to the air data system for the supersonic transport. The air data system is comprised of the following items: Pitot-static installation, Total temperature probe, Air data computer, Pressure altitude indicator, Airspeed indicator, Mach number indicator, Total temperature indicator, True airspeed indicator, Static air temperature indicator, and Angle-of-attack sensor. 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).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
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Book Description
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).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 21
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Book Description
This specification describes the principal physical and functional characteristics of the control systems necessary to start, set, vary thrust, and stop the General Electric GE4/J5G engine. The design requirements are specified. Ground and flight tests to ensure that the control systems are satisfactory have been established. 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).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
This specification describes and establishes the requirements and testing objectives for the hydraulic power, flight control, and utility actuation systems. 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: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
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Book Description
This specification describes the fuel system and establishes its requirements and testing objectives. System performance requirements established 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).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
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Book Description
This specification describes the environmental control system and establishes its requirements and testing objectives. The system shall comply with Federal Aviation Agency requirements and shall consist of the following major subsystems: Air Conditioning, Windshield Rain Removal, Anti-Icing and Antifogging, and Oxygen. System performance requirements 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: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 21
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Book Description
This specification describes the electric power system and establishes its power quality characteristics, requirements, and testing objectives. 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).
