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Author : Robert Samuel Ryan
Publisher : Unknown
Page : 44 pages
File Size : 42,9 Mb
Release : 1993
Category : Astronautics
ISBN : NASA:31769000446610
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 42 pages
File Size : 49,9 Mb
Release : 2018-07-11
Category : Electronic
ISBN : 1722836075
As emphasis shifts from optimum-performance aerospace systems to least lift-cycle costs, systems designs must seek, adapt, and innovate cost improvement techniques in design through operations. The systems design process of concept, definition, and design was assessed for the types and flow of total quality management techniques that may be applicable in a launch vehicle systems design analysis. Techniques discussed are task ordering, quality leverage, concurrent engineering, Pareto's principle, robustness, quality function deployment, criteria, and others. These cost oriented techniques are as applicable to aerospace systems design analysis as to any large commercial system. Ryan, R. and Verderaime, V. Marshall Space Flight Center ...
Author : Walter Edward Hammond
Publisher : AIAA
Page : 740 pages
File Size : 44,6 Mb
Release : 1999
Category : Astronautics
ISBN : 1600861105
Annotation This practical book gives young professionals all the information they need to know to get started in the space business. It takes you step-by-step through processes for systems engineering and acquisition, design and development, cost analysis, and program planning and analysis. You'll find the systems engineering and design process that applies to all space transportation systems, then the overall system architecture considerations that also apply to all space transportation systems. There is also detailed coverage of space launch vehicles by class, including the current space shuttle, other manned reusable systems, expendable systems, and future systems. A companion CD-ROM contains the Operations Simulation and Analysis Modeling System software.
Author : J. C. Blair
Publisher : Unknown
Page : 264 pages
File Size : 45,7 Mb
Release : 2001
Category : Electronic
ISBN : NASA:31769000451867
Author : Anonim
Publisher : Unknown
Page : 178 pages
File Size : 50,8 Mb
Release : 1994
Category : Engineering
ISBN : NASA:31769000660509
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 236 pages
File Size : 46,5 Mb
Release : 2018-06-27
Category : Electronic
ISBN : 1721928197
This report summaries the key accomplishments of Georgia Tech's Space Systems Design Laboratory (SSDL) under NASA Grant NAG8-1302 from NASA - Marshall Space Flight Center. The report consists of this summary white paper, copies of technical papers written under this grant, and several viewgraph-style presentations. During the course of this grant four main tasks were completed: (1)Simulated Combined-Cycle Rocket Engine Analysis Module (SCCREAM), a computer analysis tool for predicting the performance of various RBCC engine configurations; (2) Hyperion, a single stage to orbit vehicle capable of delivering 25,000 pound payloads to the International Space Station Orbit; (3) Bantam-X Support - a small payload mission; (4) International Trajectory Support for interplanetary human Mars missions. Olds, John R. Marshall Space Flight Center NAG8-1302
Author : Walter Edward Hammond
Publisher : AIAA
Page : 906 pages
File Size : 47,8 Mb
Release : 2001
Category : Astronautics
ISBN : 1600860451
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,
Author : Chong Hun Kim
Publisher : Lulu.com
Page : 676 pages
File Size : 47,5 Mb
Release : 2007
Category : Technology & Engineering
ISBN : 9780615165110
This book is written for aerospace engineers who have completed their BS degree and are interested in the design and analysis of rocket attitude control systems. It introduces a new approach to the design, characterized by its robustness. Current LV attitude control systems are designed based on classical SISO control theory, and they lack robustness. The theory used here truly offers a technique that enables us to design control systems that are reasonably insensitive to math modeling errors and can withstand disturbances such as gust, and in addition it doesn’t need external states estimator, such as Kalman filtering. Extensive simulation results, which demonstrate the effectiveness of this approach, are presented in this book. Basic rocket theory and a concept of H-infinity control system design technique are explained for those who are new in these fields of study.
Author : Anonim
Publisher : Unknown
Page : 1388 pages
File Size : 40,7 Mb
Release : 1971
Category : Government publications
ISBN : OSU:32437010583744
Author : Anonim
Publisher : Unknown
Page : 1060 pages
File Size : 54,7 Mb
Release : 1993-12
Category : Government publications
ISBN : UIUC:30112063914607
Author : Zhang Qingjun,Liu Jie
Publisher : CRC Press
Page : 415 pages
File Size : 49,6 Mb
Release : 2023-10-09
Category : Science
ISBN : 9781000879582
Drawing on practical engineering experience and latest achievements of space technology in China, this title investigates spacecraft system design and introduces several design methods based on the model development process. A well-established space engineering system with spacecraft as the core is integral to spaceflight activities and missions of entering, exploring, developing and utilizing outer space. This book expounds the key phases in the workflow of spacecraft development, including task analysis, overall plan design, external interface, configuration and assembly design and experimental verification. Subsystems that function as the nuclei of spacecraft design and important aspects in the model development process are then examined, such as orbit design, environmental influence factors, reliability design, dynamics analysis, etc. In addition, it also discusses the digital environment and methods to improve the efficiency of system design. The title will appeal to researchers, students, and especially professionals interested in spacecraft system design and space engineering.
Author : Anonim
Publisher : Unknown
Page : 700 pages
File Size : 48,7 Mb
Release : 1995
Category : Aeronautics
ISBN : UOM:39015038704915
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : N.V. Kadam
Publisher : Allied Publishers
Page : 380 pages
File Size : 54,5 Mb
Release : 2009-06-15
Category : Technology & Engineering
ISBN : 9789387997813
This book gives in a concise and easy to understand form the various aspects of Practical Design of Flight Control Systems for Launch Vehicles and Missiles. It covers almost every aspect of Flight Control System Design which a designer would like to know, such as mission considerations, control requirements for various segments of the flight trajectory and different types of control effectors. It further gives generalized equations of motion with a novel method of incorporating structural flexibility and propellant sloshing which does not require rederivation, and very easy and common sense approach to deriving slosh and gimballed engine dynamic equations. Subsequently it gives the control system configurations, power plant sizing, loop design for linearised system and detailed analysis and design of on-off reaction control systems. It also covers various software features which are necessary for actual implementation of the design in flight missions, robustness features to avoid malfunctioning in some circumstances, design validation aspects including end-to-end sign checks and describes some flight experiences which called for design updates. The book is unique for its strong practical flavour and is directly useful to the working engineers in the field and post graduate students in Aerospace Engineering.
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 2300 pages
File Size : 44,5 Mb
Release : 1967
Category : Aeronautics
ISBN : STANFORD:36105113793777
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 2084 pages
File Size : 42,6 Mb
Release : 1967
Category : Aeronautics
ISBN : RUTGERS:39030031129879
