Author : O. J. Olson
Publisher :
Page : 75 pages
File Size : 35,28 MB
Release : 1966
Category :
ISBN :
Contents: Applicable Documents, Requirements, Quality Assurance Provisions, Additional Data.
Author : R. G. Bush
Publisher :
Page : 222 pages
File Size : 35,63 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 :
Publisher :
Page : 812 pages
File Size : 11,90 MB
Release :
Category : Science
ISBN :
Author : E. J. Overmyer
Publisher :
Page : 41 pages
File Size : 22,8 MB
Release : 1966
Category :
ISBN :
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).
Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 33 pages
File Size : 34,72 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 : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher :
Page : 167 pages
File Size : 25,56 MB
Release : 1966
Category :
ISBN :
Author : Joseph Harris
Publisher :
Page : 47 pages
File Size : 11,19 MB
Release : 1966
Category :
ISBN :
Author : Stanley E. Lindstrom
Publisher :
Page : 37 pages
File Size : 49,58 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 : George M. Burton
Publisher :
Page : 76 pages
File Size : 44,34 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 : O. J. Olson
Publisher :
Page : 64 pages
File Size : 44,50 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 passenger and cargo accommodations subsystem (hereinafter called the P and CAS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in the supplement. The P and CAS consists of passenger-cabin furnishings and equipment, cargo provisions, and airplane exterior decorative markings.
