Download or read book Supersonic Transport Program Phase Ii c Report Standardization Plan Sst Boeing Model B 2707 written by A. L. Paxhio and published by . This book was released on 1966 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Program Phase Ii c Report Value Engineering Plan Sst Boeing Model 2707 written by R. S. Reimfield and published by . This book was released on 1966 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Program Phase Ii c Report Communications navigation Subsystem Specification Sst Boeing Model 2707 written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 167 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Program Phase Ii c Report Electrical Power Subsystem Specification Sst Boeing Model 2707 written by Joseph Harris and published by . This book was released on 1966 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Program Phase Ii c Report Passenger and Cargo Accommodations Subsystem Specification Sst Boeing Model 2707 written by O. J. Olson and published by . This book was released on 1966 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Applicable Documents, Requirements, Quality Assurance Provisions, Additional Data.
Download or read book Supersonic Transport Program Phase Ii c Report Design Integration Matrix Sst Boeing Model 2707 written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Program Phase Ii c Report Fuel Subsystem Specification Sst Boeing Model 2707 written by Stanley E. Lindstrom and published by . This book was released on 1966 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Supersonic Transport Program Phase Ii c Report Model Specification Sst Boeing Model 2707 written by R. G. Bush and published by . This book was released on 1966 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Program Phase Ii c Report Airframe Subsystem Specification Sst Boeing Model 2707 written by John Katzinski and published by . This book was released on 1966 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: This subsystem specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype airplanes. Discrete differences between the prototype and production airplanes are included in Supplement 1. (Author).
Download or read book Supersonic Transport Program Phase Ii c Report Flight Deck Subsystem Specification Sst Boeing Model 2707 written by George M. Burton and published by . This book was released on 1966 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Program Phase Ii c Report Aircraft Integrated Data System Subsystem Specification Sst Boeing Model 2707 written by W. H. Burrell and published by . This book was released on 1966 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Program Phase Ii c Report Starting Subsystem Specification Sst Boeing Model 2707 written by G. W. Ort and published by . This book was released on 1966 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test, and qualification of the Starting Subsystem (hereinafter called the SS) as applied to the prototype airplanes. The SS consists of the controls, ducting, and equipment necessary to convert pneumatic power from either a ground or engine bleed air source to shaft power input to the Accessory Drive Subsystem (ADS). The shaft power shall be used to drive the ADS.
Download or read book Supersonic Transport Program Phase Ii c Report Accessory Drive Subsystem Specification Sst Boeing Model 2707 written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Requirements; Performance; Subsystem Definition; Design and Construction; Quality Assurance Provisions; Engineering Test and Evaluation; Preliminary Qualification Test; Formal Qualification Tests; Reliability Test and Analysis; and Product Performance and Configuration Requirements/Quality Verification Cross Reference Index.
Download or read book Supersonic Transport Program Phase Ii c Report Propulsion Subsystem Specification General Electric Sst Boeing Model 2707 written by Paul E. Johnson and published by . This book was released on 1966 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for the performance, test and qualification of the B-2707 (G.E.) propulsion subsystem. The General Electric GE4/J5G engine performance data is the primary data for the propulsion subsystem performance specification. Subsystem performance requirements established herein are design objectives for the prototype airplane. Application of these requirements to production airplane design will be established after prototype flight testing and evaluation.
Download or read book Supersonic Transport Program Phase Ii c Report Environmental Control Subsystem Specification Sst Boeing Model 2707 written by E. J. Overmyer and published by . This book was released on 1966 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test and qualification of the environmental control subsystem (hereinafter called the ECS), as applied to the prototype airplanes. The ECS consists of air source equipment, air conditioning equipment, cabin temperature and cabin pressure control equipment, and the air distribution system. The ECS shall provide a comfortable and safe environment for the crew and passengers, and shall provide the required cooling for the airplane equipment and cargo areas. (Author).
Download or read book Supersonic Transport Program Phase Ii c Report Propulsion Subsystem Specification Pratt and Whitney Aircraft Sst Boeing Model 2707 written by Paul E. Johnson and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for the performance, test and qualification of the B-2707 (P and W) propulsion subsystem. The Pratt and Whitney JTF17A-20B engine performance data is the primary data for the propulsion subsystem performance specification. Subsystem performance requirements established herein are design objectives for the prototype airplane. Application of these requirements to production airplane design will be established after prototype flight testing and evaluation.
Download or read book Supersonic Transport Program Phase Ii c Report Air Induction Subsystem Specification Sst Boeing Model 2707 written by R. E. Ensley and published by . This book was released on 1966 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test and qualification of the Air Induction Subsystem. This subsystem shall provide the engine with the quantity of air demanded within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem, and provides for high pressure recovery within the flow. The installation of the subsystem is defined by the Aircraft Engine Installation Subsystem Specification (D6A10113-1).
