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 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 Aircraft Engine Installation 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 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test and qualification for the Aircraft engine Installation Subsystem. The subsystem is used to provide the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem is also used to provide mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem requires fuel, air flow, electrical and airframe support and control inputs for its operation. These are provided by the airframe fuel, air inlet, air inlet control, electrical, flight control, and airframe structure subsystems.
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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).
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 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 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 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 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 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 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 Development Program Phase Iii Proposal Boeing Model 2707 Propulsion Performance Specification general Electric written by Paul E. Johnson and published by . This book was released on 1966 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for the performance and method of calculation for the B-2707 (PW) propulsion system. The Pratt + Whitney Aircraft JTF17A-21B engine performance data is the primary data for the production propulsion performance specification. Supplement 1 of this specification defines the prototype propulsion performance and method of calculation by showing the specific differences between the production and the prototype engines.
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 Landing Gear 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; Desing and Construction; Quality Assurance Provisions; Engineering Test and Evaluation; Preliminary Qualification Tests; Formal Qualification; Reliability Test and Analyses; and Product Performance and Configuration Requirements/Quality Verification Cross-Reference Index.
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).
