Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Propulsion Controls Performance Specification PDF Download
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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 : 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 : 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 : 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 : 17
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Book Description
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).
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 : 27
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Book Description
This specification describes the automatic flight control system (AFCS) and establishes its requirements and testing objectives. Dynamic and static accuracies, as well as a complete description of all the control modes, are included. 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 : 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 : 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:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 812
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Book Description
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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Book Description
This specification establishes the design, construction, performance requirements, and test objectives of the flight instrumentation equipment for the Model 733 supersonic transport. This specification covers the following flight instrumentation equipment: Attitude director indicator; Horizontal situation indicator; Flight director computer; Comparator warning and approach gate monitor; Approach progress annunciator; Radio magnetic indicator; Standby attitude/heading indicator; Radio altimeter; and Radar altitude/vertical speed indicator. 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).
