Spacecraft engineering systems design (57 résultats)

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Hardback or Cased Book. Etat : New. A Systems Engineering Approach to the Design of a Spacecraft Dynamics and Control Testbed. Book.

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Taschenbuch. Etat : Neu. Neuware - A systems engineering team used an innovative process to develop a new frictionless air bearing satellite simulator, SIMSAT II, for AFIT. AFIT faculty provided the design team with initial requirements, including rotating 30 rpm for spin stabilization and a rapid slewing capability about the yaw axis of +/- 45 degrees in 15 seconds from a standing start to a standing stop. The design team developed the Project Vee process model to meet these requirements by combining key system engineering principles of the original Vee model with project management tenets. The Project Vee model decomposed the requirements to produce a complete system design, guided the procurement of components, and performed validation and verification of the system. The design effort resulted in a three-axis, tabletop spherical air bearing configuration. SIMSAT II incorporates the use of fans as an actuating device for rapid slewing capability, a rigid structure for greater stability, and the capability for longer experimental runs. A modular payload platform allows for numerous types of experiments to be conducted onboard the system. SIMSAT II provides AFIT with a new simulator for spacecraft dynamics and control, with both educational and research experimentation possibilities.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.…

Paperback. Etat : New.

Buch. Etat : Neu. Neuware - A systems engineering team used an innovative process to develop a new frictionless air bearing satellite simulator, SIMSAT II, for AFIT. AFIT faculty provided the design team with initial requirements, including rotating 30 rpm for spin stabilization and a rapid slewing capability about the yaw axis of +/- 45 degrees in 15 seconds from a standing start to a standing stop. The design team developed the Project Vee process model to meet these requirements by combining key system engineering principles of the original Vee model with project management tenets. The Project Vee model decomposed the requirements to produce a complete system design, guided the procurement of components, and performed validation and verification of the system. The design effort resulted in a three-axis, tabletop spherical air bearing configuration. SIMSAT II incorporates the use of fans as an actuating device for rapid slewing capability, a rigid structure for greater stability, and the capability for longer experimental runs. A modular payload platform allows for numerous types of experiments to be conducted onboard the system. SIMSAT II provides AFIT with a new simulator for spacecraft dynamics and control, with both educational and research experimentation possibilities.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.…

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Taschenbuch. Etat : Neu. Neuware.

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Gebunden. Etat : New. KlappentextA spacecraft is a machine that is created to fly in the outer space. There are numerous purposes for which spacecrafts are used, such as space colonization, communications, meteorology, navigation, transportation, Earth observ.

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Taschenbuch. Etat : Neu. Neuware - Most aerospace courses teach aerodynamics, structures, propulsion, and orbital mechanics as separate subjects - and leave students to connect them alone.If you have worked through separate courses in fluid mechanics, propulsion, and astrodynamics, you have probably noticed the seams. One text treats wings in depth but skips rockets; another derives orbital transfers but assumes you already understand compressible flow; a third covers structures as an afterthought. The result is a set of methods that never quite fits together - and a nagging sense that the same physics keeps reappearing under different names.This textbook was built to close those gaps. It presents aerospace engineering as one connected discipline, building from the atmosphere upward: the physical environment first, then the fluid mechanics that turn atmospheric properties into forces, then the propulsion that generates thrust, the structures that carry loads, and the spacecraft systems that operate where the atmosphere ends.Inside, you will: - Follow every major result from first principles, with each derivation shown step by step. - See the recurring logic across topics - why a rocket nozzle and a subsonic diffuser obey the same area-velocity relation. - Work through fully solved examples with units tracked at every stage. - Test yourself with end-of-chapter practice problems, each supported by complete answers. - Move confidently between SI and US customary units, both given where practice expects them. - Use appendices of constants, atmosphere tables, airfoil data, and material properties as a standing reference.Coverage spans the standard atmosphere and flight regimes; fluid mechanics and subsonic, finite-wing, and compressible aerodynamics; aircraft performance, stability, and control; air-breathing and rocket propulsion; aerospace structures and structural design; aircraft sizing; two-body orbital mechanics; orbital maneuvers and mission design; spacecraft systems; and re-entry and hypersonic flight.It is written for upper-division undergraduates in aerospace engineering, mechanical engineering students taking aerospace options, and early-career engineers who want a single quantitative reference from atmospheric flight through orbital operations. A background in calculus through ordinary differential equations, physics, statics, and introductory thermodynamics is assumed.Bring the whole discipline together in one volume. Add this comprehensive guide to your shelf and start building a connected understanding of flight, from the runway to orbit.…