Flight Separation Mechanisms Space Vehicle Design Criteria

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Integrated Design for Space Transportation System

B.N. Suresh,K. Sivan
Integrated Design for Space Transportation System Book PDF

Author : B.N. Suresh,K. Sivan
Publisher : Springer
Page : 761 pages
File Size : 43,9 Mb
Release : 2015-11-20
Category : Technology & Engineering
ISBN : 9788132225324

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Integrated Design for Space Transportation System by B.N. Suresh,K. Sivan Pdf

The book addresses the overall integrated design aspects of a space transportation system involving several disciplines like propulsion, vehicle structures, aerodynamics, flight mechanics, navigation, guidance and control systems, stage auxiliary systems, thermal systems etc. and discusses the system approach for design, trade off analysis, system life cycle considerations, important aspects in mission management, the risk assessment, etc. There are several books authored to describe the design aspects of various areas, viz., propulsion, aerodynamics, structures, control, etc., but there is no book which presents space transportation system (STS) design in an integrated manner. This book attempts to fill this gap by addressing systems approach for STS design, highlighting the integrated design aspects, interactions between various subsystems and interdependencies. The main focus is towards the complex integrated design to arrive at an optimum, robust and cost effective space transportation system. The orbital mechanics of satellites including different coordinate frames, orbital perturbations and orbital transfers are explained. For launching the satellites to meet specific mission requirements, viz., payload/orbit, design considerations, giving step by step procedure are briefed. The selection methodology for launch vehicle configuration, its optimum staging and the factors which influence the vehicle performance are summarized. The influence of external, internal and dynamic operating environments experienced by the vehicle subsystems and the remedial measures needed are highlighted. The mission design strategies and their influence on the vehicle design process are elaborated. The various critical aspects of STS subsystems like flight mechanics, propulsion, structures and materials, thermal systems, stage auxiliary systems, navigation, guidance and control and the interdependencies and interactions between them are covered. The design guidelines, complexity of the flight environment and the reentry dynamics for the reentry missions are included. The book is not targeted as a design tool for any particular discipline or subsystem. Some of the design related equations or expressions are not attempted to derive from the first principle as this is beyond the scope of this book. However, the important analytical expressions, graphs and sketches which are essential to provide in-depth understanding for the design process as well as to understand the interactions between different subsystems are appropriately included.

Space Shuttle Separation Mechanisms

Anonim
Space Shuttle Separation Mechanisms Book PDF

Author : Anonim
Publisher : Unknown
Page : 30 pages
File Size : 51,7 Mb
Release : 1978
Category : Electronic
ISBN : NASA:31769000537855

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Space Shuttle Separation Mechanisms by Anonim Pdf

Vanguard I Satellite Structure and Separation Mechanism

John T. Shea,Robert C. Baumann
Vanguard I Satellite Structure and Separation Mechanism Book PDF

Author : John T. Shea,Robert C. Baumann
Publisher : Unknown
Page : 22 pages
File Size : 42,6 Mb
Release : 1961
Category : Project Vanguard
ISBN : UIUC:30112106638064

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Vanguard I Satellite Structure and Separation Mechanism by John T. Shea,Robert C. Baumann Pdf

A reevaluation of the Vanguard program objectives in January 1957 resulted in the production of the Vanguard I Satellite, a 6.44-inch-diameter, 3.25-pound sphere with six equally spaced solar cell clusters and six equally spaced antennas mounted on its surface. Experiment requirements necessitated the development of a mechanism to separate the satellite from the third-stage rocket. On the basis of the existing standard separation mechanism, a strap pull-pin girth-ring arrangement was developed. Both the satellite and the separation mechanism were fully tested prior to flight. Successful orbiting and flight operation proved the adequacy of the design.

Design Methodologies for Space Transportation Systems

Walter Edward Hammond
Design Methodologies for Space Transportation Systems Book PDF

Author : Walter Edward Hammond
Publisher : AIAA
Page : 906 pages
File Size : 49,6 Mb
Release : 2001
Category : Astronautics
ISBN : 1600860451

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Design Methodologies for Space Transportation Systems by Walter Edward Hammond Pdf

Annotation "Design Methodologies for Space Transportation Systems is a sequel to the author's earlier text, "Space Transportation: A Systems Approach to Analysis and Design. Both texts represent the most comprehensive exposition of the existing knowledge and practice in the design and project management of space transportation systems, and they reflect a wealth of experience by the author with the design and management of space systems. The text discusses new conceptual changes in the design philosophy away from multistage expendable vehicles to winged, reusable launch vehicles and presents an overview of the systems engineering and vehicle design process as well as systems trades and analysis. Individual chapters are devoted to specific disciplines such as aerodynamics, aerothermal analysis, structures, materials, propulsion, flight mechanics and trajectories, avionics and computers, and control systems. The final chapters deal with human factors, payload, launch and mission operations, safety, and mission assurance. The two texts by the author provide a valuable source of information for the space transportation community of designers, operators, and managers. A companion CD-ROM succinctly packages some oversized figures and tables, resources for systems engineering and launch ranges, and a compendium of software programs. The computer programs include the USAF AIRPLANE AND MISSILE DATCOM CODES (with extensive documentation); COSTMODL for software costing; OPGUID launch vehicle trajectory generator; SUPERFLO-a series of 11 programs intended for solving compressible flow problems in ducts and pipes found in industrial facilities; and a wealth of Microsoft Excel spreadsheet programs covering thedisciplines of statistics, vehicle trajectories, propulsion performance, math utilities,

Spacecraft Thermal Control

Robert G Lyle
Spacecraft Thermal Control Book PDF

Author : Robert G Lyle
Publisher : Unknown
Page : 60 pages
File Size : 40,9 Mb
Release : 1973
Category : Space cabin atmospheres
ISBN : CORNELL:31924004466078

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Spacecraft Thermal Control by Robert G Lyle Pdf