AIAA-S-096-2004.pdf
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1、Standard ANSI/AIAA S-096-2004 AIAA standards are copyrighted by the American Institute of Aeronautics and Astronautics (AIAA), 1801 Alexander Bell Drive, Reston, VA 20191-4344 USA. All rights reserved. AIAA grants you a license as follows: The right to download an electronic file of this AIAA standa
2、rd for temporary storage on one computer for purposes of viewing, and/or printing one copy of the AIAA standard for individual use. Neither the electronic file nor the hard copy print may be reproduced in any way. In addition, the electronic file may not be distributed elsewhere over computer networ
3、ks or otherwise. The hard copy print may only be distributed to other employees for their internal use within your organization. Space Systems Flywheel Rotor Assemblies Copyright American Institute of Aeronautics and Astronautics Provided by IHS under license with AIAA Licensee=IHS Employees/1111111
4、001, User=Wing, Bernie Not for Resale, 04/18/2007 10:00:18 MDTNo reproduction or networking permitted without license from IHS -,-,- ANSI/AIAA S-096-2004 American National Standard Space Systems Flywheel Rotor Assemblies Sponsored by American Institute of Aeronautics and Astronautics Approved 30 Nov
5、ember 2004 American National Standards Institute Abstract This standard establishes baseline requirements for the design, fabrication, test, inspection, storage, and transportation of a flywheel rotor assembly used in a spaceflight flywheel system for energy storage and/or attitude control. These re
6、quirements when implemented on a particular system will assure a high level of confidence in achieving safe and reliable operation. Copyright American Institute of Aeronautics and Astronautics Provided by IHS under license with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale
7、, 04/18/2007 10:00:18 MDTNo reproduction or networking permitted without license from IHS -,-,- ANSI/AIAA S-096-2004 ii Approval of an American National Standard requires verification by ANSI that the requirements for due process, consensus, and other criteria have been met by the standards develope
8、r. Consensus is established when, in the judgment of the ANSI Board of Standards Review, substantial agreement has been reached by directly and materially affected interests. Substantial agreement means much more than a simple majority, but not necessarily unanimity. Consensus requires that all view
9、s and objections be considered, and that a concerted effort be made toward their resolution. The use of American National Standards is completely voluntary; their existence does not in any respect preclude anyone, whether he has approved the standards or not, from manufacturing, marketing, purchasin
10、g, or using products, processes, or procedures not conforming to the standards. The American National Standards Institute does not develop standards and will in no circumstances give an interpretation of any American National Standard. Moreover, no person shall have the right or authority to issue a
11、n interpretation of an American National Standard in the name of the American National Standards Institute. Requests for interpretations should be addressed to the secretariat or sponsor whose name appears on the title page of this standard. CAUTION NOTICE: This American National Standard may be rev
12、ised or withdrawn at any time. The procedures of the American National Standards Institute require that action be taken to affirm, revise, or withdraw this standard no later than five years from the date of approval. Purchasers of American National Standards may receive current information on all st
13、andards by calling or writing the American National Standards Institute. Library of Congress Cataloging-in-Publication Data American national standard space systems : flywheel rotor assemblies / sponsored by American Institute of Aeronautics and Astronautics. p. cm. ISBN 1-56347-741-6 (hardcopy) - I
14、SBN 1-56347-742-4 (electronic) 1. Space vehicles-Attitude control systems-Equipment and supplies-Standards-United States. 2. Space vehicles-Auxiliary power supply-Equipment and supplies-Standards-United States. 3. Flywheels-Standards- United States. 4. Rotors-Standards-United States. I. American Ins
15、titute of Aeronautics and Astronautics. TL3260.A45 2004 629.474-dc22 2004027019 Published by American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Reston, VA 20191 Copyright 2004 American Institute of Aeronautics and Astronautics All rights reserved No part of this publicatio
16、n may be reproduced in any form, in an electronic retrieval system or otherwise, without prior written permission of the publisher. Printed in the United States of America American National Standard Copyright American Institute of Aeronautics and Astronautics Provided by IHS under license with AIAA
17、Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:00:18 MDTNo reproduction or networking permitted without license from IHS -,-,- ANSI/AIAA S-096-2004 iii Contents Foreword v 1 Scope 1 2 Applicable Documents1 3 Vocabulary 1 3.1 Abbreviations and Acronyms .1 3.2 Terms
18、 and Definitions.2 4 General Requirements .5 4.1 Design Requirements.5 4.1.1 System Analysis5 4.1.2 Loads, Speeds and Environments.6 4.1.3 Strength.6 4.1.4 Static Stiffness 6 4.1.5 Rotor Dynamics 6 4.1.6 Thermal .7 4.1.7 Static Strength Margin of Safety 7 4.1.8 Fracture Control*.7 4.1.9 Fatigue Life
19、8 4.1.10 Time Dependent Behavior8 4.1.11 Stress-Rupture Life.8 4.1.12 Corrosion and Stress Corrosion Control and Prevention .8 4.1.13 Outgassing8 4.2 Materials Requirements9 4.2.1 Metallic Materials9 4.2.2 Composite Materials.9 4.2.3 Ceramic Materials.10 4.2.4 Polymeric Materials 11 4.3 Fabrication
20、and Process Control11 4.4 Quality Assurance.12 4.4.1 Inspection Plan .12 4.4.2 Inspection Techniques12 4.4.3 Inspection Data.12 4.4.4 Traceability* 12 4.5 Repair and Refurbishment .13 4.6 Storage Requirements13 4.7 Transportation Requirements.13 Copyright American Institute of Aeronautics and Astron
21、autics Provided by IHS under license with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:00:18 MDTNo reproduction or networking permitted without license from IHS -,-,- ANSI/AIAA S-096-2004 iv 5 Verification Requirements 13 5.1 Design Requirements Verificatio
22、n13 5.1.1 System Analysis Verification13 5.1.2 Loads, Speeds and Environments Verification .14 5.1.3 Strength Verification .14 5.1.4 Static Stiffness Verification.14 5.1.5 Rotor Dynamics Verification.14 5.1.6 Thermal Verification15 5.1.7 Static Strength MoS Verification 15 5.1.8 Fracture Control Ver
23、ification*.16 5.1.9 Fatigue Life Verification17 5.1.10 Time Dependent Behavior Verification17 5.1.11 Stress-Rupture Life Verification .17 5.1.12 Corrosion and Stress Corrosion Control and Prevention Verification17 5.1.13 Outgassing Verification.17 5.2 Acceptance Tests.17 5.2.1 Inspection18 5.2.2 Pro
24、of Spin Test .18 5.2.3 Modal Test.18 5.3 Qualification Tests 18 5.3.1 Inspection19 5.3.2 Proof Spin Test .19 5.3.3 Thermal Vacuum Tests 19 5.3.4 Vibration and Shock Tests .19 5.3.5 Damage Tolerance (Safe-Life) Test*.19 5.3.6 Modal Test.19 5.3.7 Ultimate Load Test19 Tables Table 1 Design Requirements
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- AIAA 096 2004
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