Supersonic Transport Development Program. Phase Iii. Boeing Model 2707. Starting Subsystem Specification PDF Download
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Author: Grant W. Ort
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
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Book Description
This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test and qualification of the starting subsystem (SS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The SS provides for starting and windmill braking of the engine, drives the accessory drive subsystem (ADS) and its attached accessories in the engine disconnect mode, and supplies ground source or engine bleed air to the environmental control subsystem (ECS).
Author: Grant W. Ort
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
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Book Description
This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test and qualification of the starting subsystem (SS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The SS provides for starting and windmill braking of the engine, drives the accessory drive subsystem (ADS) and its attached accessories in the engine disconnect mode, and supplies ground source or engine bleed air to the environmental control subsystem (ECS).
Author: George G. Burton
Publisher:
ISBN:
Category :
Languages : en
Pages : 163
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Author: John Katzinski
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
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Book Description
This specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype model supersonic transport airplanes. The airframe subsystem consists of the fuselage, empennage, wing and control surfaces.
Author: George G. Burton
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Book Description
This specification defines the objectives, criteria and configuration and establishes the requirements for performance, design, test, and qualification of the flight deck subsystem as applicable to the prototype supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. (Author).
Author: S. E. Lindstrom
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
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Book Description
This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the fuel subsystem for the prototype model supersonic transport airplane. This subsystem provides for the storage, distribution and management of fuel.
Author: Howard G. Barton
Publisher:
ISBN:
Category :
Languages : en
Pages : 395
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Book Description
This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the navigation and communication subsystem for the prototype model supersonic transport airplane. (Author).
Author: S. E. Lindstrom
Publisher:
ISBN:
Category :
Languages : en
Pages : 50
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Book Description
This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the fuel subsystem for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem provides for the storage, distribution and management of fuel. (Author).
Author: L. A. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 75
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Book Description
This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the primary ac, primary dc and standby electrical power systems for the prototype model supersonic transport airplane. Differences between the prototype and production electrical power subsystems are described in Supplement I. It covers the generation, conversion, control, protection, energy storage, monitoring, and distribution of electric power to all equipment that requires such power for proper functioning of the airplane. The primary ac electric power source of the airplane requires a mechanical power input from the accessory drive defined by specification D6A10089-1. Performance of the electric utilization equipment associated with other aircraft subsystems is defined in those subsystem specifications. Performance of the lighting subsystem is defined in Part II of this specification.
Author: Howard G. Barton
Publisher:
ISBN:
Category :
Languages : en
Pages : 399
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Book Description
This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the communications/navigation/radar subsystem for the prototype model supersonic transport airplane.
Author: V. D. Warmbo
Publisher:
ISBN:
Category :
Languages : en
Pages : 66
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Book Description
