Launch Vehicle Design Process Description And Training Formulation

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Launch Vehicle Design Process Description and Training Formulation

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 88 pages
File Size : 41,6 Mb
Release : 2018-09-23
Category : Science
ISBN : 1723962651

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Launch Vehicle Design Process Description and Training Formulation by National Aeronautics and Space Adm Nasa Pdf

A primary NASA priority is to reduce the cost and improve the effectiveness of launching payloads into space. As a consequence, significant improvements are being sought in the effectiveness, cost, and schedule of the launch vehicle design process. In order to provide a basis for understanding and improving the current design process, a model has been developed for this complex, interactive process, as reported in the references. This model requires further expansion in some specific design functions. Also, a training course for less-experienced engineers is needed to provide understanding of the process, to provide guidance for its effective implementation, and to provide a basis for major improvements in launch vehicle design process technology. The objective of this activity is to expand the description of the design process to include all pertinent design functions, and to develop a detailed outline of a training course on the design process for launch vehicles for use in educating engineers whose experience with the process has been minimal. Building on a previously-developed partial design process description, parallel sections have been written for the Avionics Design Function, the Materials Design Function, and the Manufacturing Design Function. Upon inclusion of these results, the total process description will be released as a NASA TP. The design function sections herein include descriptions of the design function responsibilities, interfaces, interactive processes, decisions (gates), and tasks. Associated figures include design function planes, gates, and tasks, along with other pertinent graphics. Also included is an expanded discussion of how the design process is divided, or compartmentalized, into manageable parts to achieve efficient and effective design. A detailed outline for an intensive two-day course on the launch vehicle design process has been developed herein, and is available for further expansion. The course is in an interactive lecture/wor

Launch Vehicle Design Process

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 262 pages
File Size : 43,9 Mb
Release : 2018-06-27
Category : Electronic
ISBN : 1721938141

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Launch Vehicle Design Process by National Aeronautics and Space Administration (NASA) Pdf

Engineering design is a challenging activity for any product. Since launch vehicles are highly complex and interconnected and have extreme energy densities, their design represents a challenge of the highest order. The purpose of this document is to delineate and clarify the design process associated with the launch vehicle for space flight transportation. The goal is to define and characterize a baseline for the space transportation design process. This baseline can be used as a basis for improving effectiveness and efficiency of the design process. The baseline characterization is achieved via compartmentalization and technical integration of subsystems, design functions, and discipline functions. First, a global design process overview is provided in order to show responsibility, interactions, and connectivity of overall aspects of the design process. Then design essentials are delineated in order to emphasize necessary features of the design process that are sometimes overlooked. Finally the design process characterization is presented. This is accomplished by considering project technical framework, technical integration, process description (technical integration model, subsystem tree, design/discipline planes, decision gates, and tasks), and the design sequence. Also included in the document are a snapshot relating to process improvements, illustrations of the process, a survey of recommendations from experienced practitioners in aerospace, lessons learned, references, and a bibliography. Blair, J. C. and Ryan, R. S. and Schutzenhofer, L. A. and Humphries, W. R. Marshall Space Flight Center

Design of Rockets and Space Launch Vehicles

Author : Donald L. Edberg,Guillermo Costa,Willie Costa
Publisher : American Institute of Aeronautics and Astronautics Incorporated
Page : 0 pages
File Size : 50,8 Mb
Release : 2020
Category : Launch vehicles (Astronautics)
ISBN : 1624105939

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Design of Rockets and Space Launch Vehicles by Donald L. Edberg,Guillermo Costa,Willie Costa Pdf

With growing interest in space activity and numerous new launchers in development, this book is a timely, comprehensive survey of important concepts and applications. It enhances understanding and provides exposure to practical aspects of design, manufacturing, testing, and engineering associated with these topics.

Multidisciplinary Optimization Branch Experience Using ISIGHT Software

Author : S. L. Padula
Publisher : Unknown
Page : 22 pages
File Size : 48,8 Mb
Release : 1999
Category : Multidisciplinary design optimization
ISBN : NASA:31769000634686

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Multidisciplinary Optimization Branch Experience Using ISIGHT Software by S. L. Padula Pdf

The Multidisciplinary Optimization (MDO) Branch at NASA Langley is investigating frameworks for supporting multidisciplinary analysis and optimization research. A framework provides software and system services to integrate computational tasks and allows the researcher to concentrate more on the application and less on the programming details. A framework also provides a common working environment and a full range of optimization tools, and so increases the productivity of multidisciplinary research teams. Finally, a framework enables staff members to develop applications for use by disciplinary experts in other organizations. This year, the MDO Branch has gained experience with the iSIGHT framework. This paper describes experiences with four aerospace applications, including (1) reusable launch vehicle sizing, (2) aerospike nozzle design, (3) low-noise rotorcraft trajectories, and (4) acoustic liner design. Brief overviews of each problem are provided, including the number and type of disciplinary codes and computation time estimates. In addition, the optimization methods, objective functions, design variables, and constraints are described for each problem. For each case, discussions on the advantages and disadvantages of using the iSIGHT framework are provided as well as notes on the ease of use of various advanced features and suggestions for areas of improvement.

Commerce Business Daily

Author : Anonim
Publisher : Unknown
Page : 1612 pages
File Size : 54,7 Mb
Release : 1999
Category : Government purchasing
ISBN : NYPL:33433063171130

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Commerce Business Daily by Anonim Pdf

Information Flow in the Launch Vehicle Design/Analysis Process

Author : National Aeronautics and Space Adm Nasa
Publisher : Unknown
Page : 56 pages
File Size : 44,5 Mb
Release : 2018-09-20
Category : Electronic
ISBN : 1723852198

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Information Flow in the Launch Vehicle Design/Analysis Process by National Aeronautics and Space Adm Nasa Pdf

This paper describes the results of a team effort aimed at defining the information flow between disciplines at the Marshall Space Flight Center (MSFC) engaged in the design of space launch vehicles. The information flow is modeled at a first level and is described using three types of templates: an N x N diagram, discipline flow diagrams, and discipline task descriptions. It is intended to provide engineers with an understanding of the connections between what they do and where it fits in the overall design process of the project. It is also intended to provide design managers with a better understanding of information flow in the launch vehicle design cycle.Humphries, W. R., Sr. and Holland, W. and Bishop, R.Marshall Space Flight CenterINFORMATION FLOW; DESIGN ANALYSIS; LAUNCH VEHICLES; OPTIMIZATION; SPACECRAFT LAUNCHING; SPACE TRANSPORTATION...

Scientific and Technical Aerospace Reports

Author : Anonim
Publisher : Unknown
Page : 464 pages
File Size : 51,7 Mb
Release : 1995
Category : Aeronautics
ISBN : MINN:30000011064593

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Scientific and Technical Aerospace Reports by Anonim Pdf

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.

NASA Conference Publication

Author : Anonim
Publisher : Unknown
Page : 418 pages
File Size : 45,8 Mb
Release : 1990
Category : Aeronautics
ISBN : UOM:39015022348364

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NASA Conference Publication by Anonim Pdf

Ensuring the Safety of Human Spaceflight

Author : United States. Congress. House. Committee on Science and Technology (2007). Subcommittee on Space and Aeronautics
Publisher : Unknown
Page : 144 pages
File Size : 47,8 Mb
Release : 2010
Category : Science
ISBN : UCSD:31822037823788

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Ensuring the Safety of Human Spaceflight by United States. Congress. House. Committee on Science and Technology (2007). Subcommittee on Space and Aeronautics Pdf

Launch Vehicle Design and Optimization Methods and Priority for the Advanced Engineering Environment

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 36 pages
File Size : 54,9 Mb
Release : 2018-06-03
Category : Electronic
ISBN : 1720610215

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Launch Vehicle Design and Optimization Methods and Priority for the Advanced Engineering Environment by National Aeronautics and Space Administration (NASA) Pdf

NASA's Advanced Engineering Environment (AEE) is a research and development program that will improve collaboration among design engineers for launch vehicle conceptual design and provide the infrastructure (methods and framework) necessary to enable that environment. In this paper, three major technical challenges facing the AEE program are identified, and three specific design problems are selected to demonstrate how advanced methods can improve current design activities. References are made to studies that demonstrate these design problems and methods, and these studies will provide the detailed information and check cases to support incorporation of these methods into the AEE. This paper provides background and terminology for discussing the launch vehicle conceptual design problem so that the diverse AEE user community can participate in prioritizing the AEE development effort.Rowell, Lawrence F. and Korte, John J.Langley Research CenterLAUNCH VEHICLES; SYSTEMS ENGINEERING; DESIGN OPTIMIZATION; SPACE TRANSPORTATION SYSTEM; RESEARCH AND DEVELOPMENT; MATHEMATICAL MODELS; STOCHASTIC PROCESSES; GENETIC ALGORITHMS; EXPERIMENT DESIGN; CONFIGURATION MANAGEMENT