Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 167 pages
File Size : 34,71 MB
Release : 1966
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ISBN :
Author : Joseph Harris
Publisher :
Page : 47 pages
File Size : 16,49 MB
Release : 1966
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Author : W. H. Burrell
Publisher :
Page : 25 pages
File Size : 41,98 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.
Author : Stanley E. Lindstrom
Publisher :
Page : 37 pages
File Size : 12,74 MB
Release : 1966
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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 : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 33 pages
File Size : 32,6 MB
Release : 1966
Category :
ISBN :
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.
Author : George M. Burton
Publisher :
Page : 76 pages
File Size : 35,64 MB
Release : 1966
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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 : O. J. Olson
Publisher :
Page : 75 pages
File Size : 47,63 MB
Release : 1966
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ISBN :
Contents: Applicable Documents, Requirements, Quality Assurance Provisions, Additional Data.
Author : R. E. Ensley
Publisher :
Page : 21 pages
File Size : 22,12 MB
Release : 1966
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ISBN :
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).
Author : L. A. Hulsman
Publisher :
Page : 52 pages
File Size : 18,73 MB
Release : 1966
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ISBN :
This specification establishes the requirements for performance, design, test and qualification of the Flight Controls and Hydraulics Subsystem, as applied to the prototype preproduction airplanes. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation system commands and furnish hydraulic power to the Landing Gear Subsystem, D6A10108-1. The subsystem shall consist of Primary Flight Controls, Secondary Flight Controls, Automatic Flight Controls and Hydraulic Power. (Author).
Author : Paul E. Johnson
Publisher :
Page : 54 pages
File Size : 24,15 MB
Release : 1966
Category :
ISBN :
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.
