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Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Airframe/engine Business Agreement (general Electric).

Author : W. T. Parish

Publisher :

Page : 21 pages

File Size : 18,23 MB

Release : 1966

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Book Description

Contents: Supersonic Transport Aircraft System Responsibility Agreement; Engine deficiencies; System Deficiencies; Correction of System Deficiencies; Additional Applicability; Changes; Data; Ancillary Agreements; and Duration of Agreements and Admendments, Business Agreements; Working relationships; Product support requirements; Transportation; Hardware requirements. Business Agreements including: Working Relationships; Product Support Requirements; Transportation; Hardware Requirements.





Supersonic Transport Development Program. Phase 3 Proposal. Boeing Model 2707. Volume 2-14. Propulsion Report - Part C. Engine Evaluation

Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.

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Page : 117 pages

File Size : 41,90 MB

Release : 1966

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Book Description

Throughout Phase II-C, as in earlier phases of the SST Program, The Boeing Company has maintained a program of design analysis and performance evaluation, with the coordinated participation of both engine contractors. As a result, the General Electric GE4/J5P powered B-2707 (GE) and the Pratt and Whitney Aircraft JFT17A-21B powered B-2707 (P and WA) airplanes are very competitive in terms of overall airplane performance criteria, and either would make an outstanding airline airplaned. The purpose of this document is to report the technical evaluation of the two engines. Considerations in this evaluation include engine/airplane matching and performance, engine design, installation compatibility, development plan, development risk, and growth potential.



Supersonic Transport Development Program. Boeing Model 2707. Phase Iii Contract. Exhibit A. Statement of Work

Author : BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.

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Page : 39 pages

File Size : 16,9 MB

Release : 1966

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Book Description

Contents: Introduction; Program Requirements; SST Program Milestones; Contract Performance Criteria; System Integration - General; Product Assurance - General; Airframe Structures - General; Airframe Subsystem - General; Propulsion System - General; System Tests - General; Product Support - General; and Product Management - General.



Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. B-2707 Model Specification

Author : R. G. Bush

Publisher :

Page : 309 pages

File Size : 11,58 MB

Release : 1966

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Book Description

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.



Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-12. Propulsion Report-part A. Engine Inlet and Controls

Author : BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.

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Page : 308 pages

File Size : 29,57 MB

Release : 1966

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Book Description

This document includes the summary and three major sections of the propulsion report describing the engines, supersonic inlet, and the propulsion control systems. Studies conducted during Phase II C have resulted in significant improvements to the Boeing Model 2707 propulsion system. Optimum sized engines with improved thrust and fuel consumption characteristics are available from General Electric and Pratt and Whitney Aircraft. The four separate and interchangeable propulsion pods are mounted below the lower surface of the horizontal stabilizer at such a position that the engine exhaust will not impinge on any part of the airplane. The pod location and shape provides optimum lift effect on the airplane.



SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE 3. BOEING MODEL 2707. MODEL SPECIFICATION.

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Page : 298 pages

File Size : 42,15 MB

Release : 1966

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Book Description

This specification defines the Boeing Model 2707-100 Intercontinental Supersonic Transport powered by four engines manufactured by General Electric or Pratt and Whitney Aircraft, and is designated 2707 (GE) or 2707 (P and W), respectively. Differences associated with the use of either type of engines are also noted herein. This specification is submitted in compliance with Part 1A of Exhibit 3B of the Federal Aviation Administration's Request for Proposal for Phase 3 of the Supersonic Transport Development Program. The production configurations described herein are the basic intercontinental airline models. This specification has been arranged in a typical commercial format.





Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Government Furnished Property and Services

Author : L. H Cargol (Sr)

Publisher :

Page : 7 pages

File Size : 32,13 MB

Release : 1966

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Book Description

This document is prepared pursuant to the provisions of the Boeing Phase III Supersonic Transport Development Contract with the FAA, which provides that the government shall furnish to the contractor, for use in the performance of this contract, certain identified government property and services. Government-owned property and services required to support this contract are identified in this document. In addition to the government property identified, the contractor will require support for this property, which will include but not be limited to data, drawings, documents, equipment, spares, assistance and services.



Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-7. Airframe Design Report. Part C. Design Criteria Loads. Aerodynamic Heating Flutter

Author : D. R. Donaldson

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Page : 138 pages

File Size : 48,77 MB

Release : 1966

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Book Description

This report presents the Boeing proposal for structural design loads and environment on the B-2707 commercial supersonic transport. Information on Phase III planning is included to define an efficient program necessary for first flight of the B-2707 prototype. Flight and ground loads criteria, flutter and vibration criteria, and structural design criteria are presented. The design loads and methods of analysis together with load validation data are presented in Sec. 3.0. The effects of these loads on ride comfort of the passengers and crew are also included. Structural temperature analyses that define the effects of aerodynamic and engine-induced heating on all major structure are presented in Sec. 4.0.