Space Vehicle Design

Author: Michael Douglas Griffin
Editor: AIAA
ISBN: 9781600861123
File Size: 37,25 MB
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Nasa Space Vehicle Design Criteria Environment

Author: Goddard Space Flight Center
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ISBN:
File Size: 45,21 MB
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Nasa Space Vehicle Design Criteria Volume 3 Structures Part B Loads And Structural Dynamics Chapter 1 General Criteria Section 1 Flutter Buzz And Divergence

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File Size: 20,36 MB
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Launch Vehicle Design Process Characterization Technical Integration And Lessons Learned

Author: J. C. Blair
Editor:
ISBN:
File Size: 75,17 MB
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The Influential Aspects Of Atmospheric Disturbances On Space Vehicle Design Using Statistical Approaches For Analysis

Author: Robert S. Ryan
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ISBN:
File Size: 19,36 MB
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Nasa Space Vehicle Design Criteria Guidance And Control Entry Vehicle Control

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File Size: 78,69 MB
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Nasa Space Vehicle Design Criteria Prelaunch Ground Wind Loads

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File Size: 50,78 MB
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Information Flow In The Launch Vehicle Design Analysis Process

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File Size: 57,69 MB
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Compartment Venting Space Vehicle Design Criteria

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File Size: 33,42 MB
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Solid Rocket Motor Igniters Nasa Space Vehicle Design Criteria Chemical Propulsion

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File Size: 30,39 MB
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Nasa Space Vehicle Design Criteria Environment Meteorid Environment Model 1969 Near Earth To Lunar Surface

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File Size: 69,17 MB
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Nasa Space Vehicle Design Criteria Structures Propellant Slosh Loads

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File Size: 59,43 MB
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Elements Of Spacecraft Design

Author: Charles D. Brown
Editor: AIAA
ISBN: 9781600860515
File Size: 47,20 MB
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Annotation This text discusses the conceptual stages of mission design, systems engineering, and orbital mechanics, providing a basis for understanding the design process for different components and functions of a spacecraft. Coverage includes propulsion and power systems, structures, attitude control, thermal control, command and data systems, and telecommunications. Worked examples and exercises are included, in addition to appendices on acronyms and abbreviations and spacecraft design data. The book can be used for self-study or for a course in spacecraft design. Brown directed the team that produced the Magellan spacecraft, and has taught spacecraft design at the University of Colorado. Annotation c. Book News, Inc., Portland, OR (booknews.com).

Analysis And Design Of Space Vehicle Flight Control Systems Volume 16 Abort

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File Size: 73,38 MB
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Nasa Space Vehicle Design Criteria Volume 3 Structures Part B Loads And Structural Dynamics Chapter 3 Launch And Exit Section 2 Local Steady Aerodynamic Loads

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File Size: 35,84 MB
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Space Radiation Protection Space Vehicle Design Criteria

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File Size: 21,32 MB
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Space Launch Vehicle Design

Author: EDBERG. COSTA
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ISBN: 9781624105937
File Size: 50,53 MB
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Spacecraft Aerodynamic Torques Space Vehicle Design Criteria Guidance And Control

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File Size: 39,73 MB
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Space Launch Vehicle Design

Author: David Woodward
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File Size: 22,56 MB
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Engineering design can be broken down into three phases: conceptual design, preliminary design, and detailed design. During the conceptual design phase, several potential configurations are studied towards the identification of the baseline vehicle. Although the least amount of detail is known about the design during the early conceptual design phase, the decisions made during this phase lock in major features effecting life-cycle cost and overall product success. As the next big space race begins, it is critically important to have a readily available tool for launch vehicle designers that is intuitive to use, easy to modify, cost effective, and provides correct results. This thesis details the creation of such a tool for use during the early conceptual design phase by analyzing existing launch vehicle design software and literature in order to adopt a best-practice approach to launch vehicle sizing. In addition to correctly sizing the vehicle calculating the initial parameters, the tool also determines the vehicle's basic geometric information and runs an ascent-to-orbit trajectory simulation to verify the design's validity. The tool is capable of sizing fully expendable space launch vehicles, fully expendable vehicles whose final stage is to be used for both ascent-to-orbit and additional orbital maneuvering after reaching the parking orbit, and vehicles whose first stage performs a self-recovery through the boostback and vertical landing method.

Space Vehicle Mechanisms

Author: Peter L. Conley
Editor: John Wiley & Sons
ISBN: 9780471121411
File Size: 64,91 MB
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The first comprehensive reference on the design, analysis, and application of space vehicle mechanisms Space Vehicle Mechanisms: Elements of Successful Design brings together accumulated industry experience in the design, analysis, and application of the mechanical systems used during space flight. More than thirty experts from a variety of related specialties and subspecialties share their insights, technical expertise, and in-depth knowledge on an enormous variety of topics, including: * Stainless steel, beryllium, and other widely used materials * Bearings * Lubricants and component lubrication * Release devices * Motors * Optical encoders * Resolvers * Signal and power transfer devices * Deployment devices * Thermal design * Radiation and survivability * Electrical interfaces * Reliability Space Vehicle Mechanisms is an indispensable resource for engineers involved in the design and analysis of mechanical assemblies used in space flight, and a valuable reference for space systems engineers, mission planners, and control systems engineers. It is also an excellent text for upper-level undergraduate and graduate-level courses in astronautical and mechanical engineering. Space Vehicle Mechanisms: Elements of Successful Design brings together accumulated industry experience in the design, analysis, and application of the mechanical systems used during space flight. More than thirty experts from a variety of related specialties and subspecialties share their insights, technical expertise, and in-depth knowledge on an enormous variety of topics, including: