Author : R. G. Bush
Publisher :
Page : 309 pages
File Size : 37,17 MB
Release : 1966
Category :
ISBN :
Contents: General Airplane Description; General Requirements; General Airplane Characteristics; Airframe Structures; Propulsion; Flight Deck Accommodations; Flight Controls; Hydraulic Power System; Electric Power System; Electronics; Passenger and Cargo Provisions; Environmental Control; Maintainability, and Standard Parts, Interchangeability, and Replaceability.
Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 152 pages
File Size : 17,88 MB
Release : 1966
Category :
ISBN :
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.
Author : Lewis H. Gray
Publisher :
Page : 29 pages
File Size : 26,95 MB
Release : 1966
Category :
ISBN :
This specification establishes the performance, design, test, and qualification requirements for the flight simulator of Boeing Model 2707 production airplane (B-2707). The simulator will be used for training flight crews in both ground and flight operations.
Author : Lewis H. Gray
Publisher :
Page : 38 pages
File Size : 27,31 MB
Release : 1966
Category :
ISBN :
Author : George G. Burton
Publisher :
Page : 126 pages
File Size : 32,94 MB
Release : 1966
Category :
ISBN :
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 : Howard G. Barton
Publisher :
Page : 395 pages
File Size : 39,10 MB
Release : 1966
Category :
ISBN :
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 :
Page : 47 pages
File Size : 33,89 MB
Release : 1966
Category :
ISBN :
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 : Eugene A. Liekhus
Publisher :
Page : 63 pages
File Size : 12,20 MB
Release : 1966
Category :
ISBN :
Author : A. Gay
Publisher :
Page : 119 pages
File Size : 40,46 MB
Release : 1966
Category :
ISBN :
This document describes the land, buildings, and equipment facilities resources required for all phases of the projected B-2707 Program.
Author : Paul E. Johnson
Publisher :
Page : 70 pages
File Size : 29,42 MB
Release : 1966
Category :
ISBN :
This specification establishes the requirements for the performance and method of calculation for the B-2707 (PW) propulsion system. The Pratt + Whitney Aircraft JTF17A-21B engine performance data is the primary data for the production propulsion performance specification. Supplement 1 of this specification defines the prototype propulsion performance and method of calculation by showing the specific differences between the production and the prototype engines.
