Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Air Induction Subsystem Specification written by L. J. Kimer and published by . This book was released on 1966 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the air induction subsystem for the prototype-model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The air induction subystem shall provide the engine with the quantity of air demanded at high-pressure recovery within the flow distortion limits of the engine. Four independent subsystems are required per airplane.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Air Induction Control Subsystem Specification written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 139 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines objectives, criteria and configuration, and establishes requirements for performance, operation, design, test and qualification of the air induction control subsystem (hereinafter called the control subsystem) as applied to the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem is used to provide automatic and manual control of the air induction subsystem, (hereinafter called the inlet). There shall be one independent control subsystem for each of the four inlets. Each control subsystem changes the geometry of an inlet centerbody and operates its bypass louvers and takeoff doors to provide efficient inlet airflow diffusion and high performance inlet-engine airflow match. The subsystems include necessary hydraulic power generation, hydraulic power distribution equipment, and flight deck controls and displays. Power from the airplane electrical system and from each of the engines is required by the subsystem in order to accomplish its intended function. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Fuel Subsystem Specification written by S. E. Lindstrom and published by . This book was released on 1966 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Environmental Control Subsystem Specification written by V. D. Warmbo and published by . This book was released on 1966 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Flight Deck Subsystem Specification written by George G. Burton and published by . This book was released on 1966 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Communications navigation Subsystem Specification written by Howard G. Barton and published by . This book was released on 1966 with total page 395 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Air Induction Subsystem Specification written by L. J. Kimer and published by . This book was released on 1966 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the air induction subsystem for the prototype-model supersonic transport airplane. Differences between the prototype and production airplanes are described. The air induction subsystem shall provide the engine with the quantity of air demanded at high-pressure recovery within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem. The installation of the subsystem is defined by specification D6A10113-1. Four independent subsystems are required per airplane.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Airframe Subsystem Specification written by John Katzinski and published by . This book was released on 1966 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype model supersonic transport airplenes. The airframe subsystem consists of the fuselage, empennage, wing and control surfaces. Discrete differences between the prototype model supersonic transport airplanes and production airplanes are included in Supplement I. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Flight Controls and Hydraulics Subsystem Specification written by E. See and published by . This book was released on 1966 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the flight controls and hydraulic subsystem for the B-2707 supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation commands and furnish hydraulic power to the landing gear subsystem. This subsystem shall consist of primary flight controls, secondary flight controls, automatic flight controls and hydraulic power. (Author).
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Starting Subsystem Specification written by Grant W. Ort and published by . This book was released on 1966 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Landing Gear Subsystem Specification written by T. A. Perara and published by . This book was released on 1966 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the Landing Gear Subsystem for the prototype model supersonic transport airplane. The subsystem defined herein consists of the landing gear structure, shock absorbers, wheels, brakes, tires, brake control, steering, extension and retraction, and position indication and warning.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Flight Deck Subsystem Specification written by George G. Burton and published by . This book was released on 1966 with total page 163 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Ground Support Equipment Requirements Specification written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test, and qualification of the Ground Support Equipment (GSE) required for the B-2707. Included are the general design requirements applicable to all GSE designed for the B-2702, a consolidated list of the GSE arranged by system requirements, and individual specification data for each item of equipment. This combined specification provides requirements planning information and technical data on all of the GSE presently identified. A prime consideration in GSE planning and definition has been to use existing inventory, existing standard, or modified standard GSE whenever possible. The extensive use of equipment in these categories for B-2707 support is indicated on the consolidated list. GSE identification is an output of the system engineering analysis process, which is continuously applied to define and verify the B-2707 support requirements. The specification will be refined and updated throughout the prototype development program to provide a current definition of the GSE requirements for effective and efficient air carrier ground operations.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Airframe Subsystem Specification written by John Katzinski and published by . This book was released on 1966 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Fuel Subsystem Specification written by S. E. Lindstrom and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Aircraft Engine Installation Subsystem Specification written by L. G. Dhoors and published by . This book was released on 1966 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification for the Aircraft Engine Installation Subsystem (AEIS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described. The subsystem provides the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem also provides mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem contains the engine, exhaust and thrust reverser assembly, engine accessories, engine mounting provisions, engine controls, cowling, bleed air ducting, instrumentation plumbing and wiring.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Electrical Power Subsystem Specification written by L. A. Jones and published by . This book was released on 1966 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
