Author : A. L. Paxhio
Publisher :
Page : 31 pages
File Size : 31,8 MB
Release : 1966
Category :
ISBN :
This document is a description of the Boeing Company management methods of standardization applied in the design and manufacture of the preproduction prototype supersonic transport. It identifies and provides policy direction for technical and management considerations applicable to the establishment and maintenance of standardization requirements.
Author : R. S. Reimfield
Publisher :
Page : 30 pages
File Size : 38,60 MB
Release : 1966
Category :
ISBN :
This document defines the Boeing SST value engineering plan for the supersonic preproduction prototype development program. It provides policy direction as well as technical and management considerations for the execution and maintenance of an effective program. The value engineering plan will be implemented through use of the following methods: Application of value engineering by employees in performance of application assignments; Formal analysis of design, development, test, tooling, planning, and manufacturing; Informal analyses and recommendations developed through consultation; and Value engineering in conjunction with procurement functions.
Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 167 pages
File Size : 18,88 MB
Release : 1966
Category :
ISBN :
Author : Joseph Harris
Publisher :
Page : 47 pages
File Size : 42,65 MB
Release : 1966
Category :
ISBN :
Author : O. J. Olson
Publisher :
Page : 75 pages
File Size : 45,44 MB
Release : 1966
Category :
ISBN :
Contents: Applicable Documents, Requirements, Quality Assurance Provisions, Additional Data.
Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 9 pages
File Size : 28,22 MB
Release : 1966
Category :
ISBN :
This document presents a design integration matrix applicable to Phase II-C of the Supersonic Transport Program. It shows, by a system of code numbers, what element in the Boeing organization has responsibility and the degree of responsibility for each element in the work breakdown structure. The organizations included are only those that affect, directly or indirectly, the establishment of the design of the SST.
Author : Stanley E. Lindstrom
Publisher :
Page : 37 pages
File Size : 19,36 MB
Release : 1966
Category :
ISBN :
This specification establishes the requirements for performance design, test and qualification of the fuel system as applied to the prototype airplanes. This subsystem will provide for the storage, distribution and management of fuel. (Author).
Author : R. G. Bush
Publisher :
Page : 222 pages
File Size : 13,18 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 : George M. Burton
Publisher :
Page : 76 pages
File Size : 33,30 MB
Release : 1966
Category :
ISBN :
Contents: Requirements; Performance; Subsystem Definition; Design and Construction; Quality Assurance Provisions; Engineering Test and Evaluation; Preliminary Qualification Tests; Formal Qualification/Certification Tests; and Reliability Test and Analysis.
Author : W. H. Burrell
Publisher :
Page : 25 pages
File Size : 33,85 MB
Release : 1966
Category :
ISBN :
Contents: Requirements; Performance; Subststem Definition; Design and Construction; Quality Assurance Provisions; Engineering Test and Evaluation; Preliminary Qualification Tests; Formal Qualification/Certification Tests; Reliability tests and Analyses; Product Performance and Configuration Requirements/Quality Verification Crossreference Index.
