Author : R. G. Bush
Publisher :
Page : 222 pages
File Size : 21,95 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 : 167 pages
File Size : 46,69 MB
Release : 1966
Category :
ISBN :
Author : Joseph Harris
Publisher :
Page : 47 pages
File Size : 41,51 MB
Release : 1966
Category :
ISBN :
Author : Stanley E. Lindstrom
Publisher :
Page : 37 pages
File Size : 29,91 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 : O. J. Olson
Publisher :
Page : 75 pages
File Size : 29,66 MB
Release : 1966
Category :
ISBN :
Contents: Applicable Documents, Requirements, Quality Assurance Provisions, Additional Data.
Author : John Katzinski
Publisher :
Page : 78 pages
File Size : 31,90 MB
Release : 1966
Category :
ISBN :
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).
Author : Paul E. Johnson
Publisher :
Page : 54 pages
File Size : 50,21 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.
Author : George M. Burton
Publisher :
Page : 76 pages
File Size : 41,99 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 : R. E. Ensley
Publisher :
Page : 21 pages
File Size : 36,87 MB
Release : 1966
Category :
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 : W. H. Burrell
Publisher :
Page : 25 pages
File Size : 19,15 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.
