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Systems Design Analysis Applied to Launch Vehicle Configuration

Systems Design Analysis Applied to Launch Vehicle Configuration PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722836078
Category :
Languages : en
Pages : 42

Book Description
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 ...

Systems Design Analysis Applied to Launch Vehicle Configuration

Systems Design Analysis Applied to Launch Vehicle Configuration PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722836078
Category :
Languages : en
Pages : 42

Book Description
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 ...

Systems Design Analysis Applied to Launch Vehicle Configuration

Systems Design Analysis Applied to Launch Vehicle Configuration PDF Author: Robert Samuel Ryan
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 44

Book Description


System Design Analysis Applied to Launch Vehicle Configuration

System Design Analysis Applied to Launch Vehicle Configuration PDF Author: R. Ryan
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Book Description


Space Transportation

Space Transportation PDF Author: Walter Edward Hammond
Publisher: AIAA
ISBN: 9781600861109
Category : Astronautics
Languages : en
Pages : 740

Book Description
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.

Information Flow in the Launch Vehicle Design/Analysis Process

Information Flow in the Launch Vehicle Design/Analysis Process PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 62

Book Description


Design Methodologies for Space Transportation Systems

Design Methodologies for Space Transportation Systems PDF Author: Walter Edward Hammond
Publisher: AIAA
ISBN: 9781600860454
Category : Astronautics
Languages : en
Pages : 906

Book Description
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 System Design

Spacecraft System Design PDF Author: Zhang Qingjun
Publisher: CRC Press
ISBN: 1000879585
Category : Science
Languages : en
Pages : 415

Book Description
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.

Launch Vehicle Design Process: Characterization, Technical Integration, and Lessons Learned

Launch Vehicle Design Process: Characterization, Technical Integration, and Lessons Learned PDF Author: J. C. Blair
Publisher:
ISBN:
Category :
Languages : en
Pages : 264

Book Description


Launch Vehicle Systems Analysis

Launch Vehicle Systems Analysis PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721928194
Category :
Languages : en
Pages : 236

Book Description
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

Launch Vehicle Systems Design Analysis

Launch Vehicle Systems Design Analysis PDF Author: Robert Ryan
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description