AIAA-SP-108-2004.pdf
《AIAA-SP-108-2004.pdf》由会员分享,可在线阅读,更多相关《AIAA-SP-108-2004.pdf(24页珍藏版)》请在三一文库上搜索。
1、 Special Project AIAA SP-108-2004 Recommended Design Practices for Conceptual Nuclear Fusion Space Propulsion Systems 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 grant
2、s you a license as follows: The right to download an electronic file of this AIAA standard 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
3、. In addition, the electronic file may not be distributed elsewhere over computer networks or otherwise. The hard copy print may only be distributed to other employees for their internal use within your organization. Copyright American Institute of Aeronautics and Astronautics Provided by IHS under
4、license with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:52:53 MDTNo reproduction or networking permitted without license from IHS -,-,- AIAA SP-108-2004 Special Project Report Recommended Design Practices for Conceptual Nuclear Fusion Space Propulsion Sys
5、tems Sponsored by American Institute of Aeronautics and Astronautics Abstract This document provides recommended design practices for conceptual engineering studies of nuclear fusion space propulsion systems. Discussion and recommendations are included on key topics including design reference missio
6、ns, degree of technological extrapolation and concomitant risk, thoroughness in calculating mass properties (nominal mass properties, weight-growth contingency and propellant margins, and specific impulse), and thoroughness in calculating power generation and usage (power-flow, power contingencies,
7、specific power). Copyright American Institute of Aeronautics and Astronautics Provided by IHS under license with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:52:53 MDTNo reproduction or networking permitted without license from IHS -,-,- AIAA SP-108-2004 ii
8、 Library of Congress Cataloging-in-Publication Data Special project report : recommended design practices for conceptual nuclear fusion space propulsion systems. p. cm. “AIAA SP-108-2004.“ Includes bibliographical references. ISBN 1-56347-751-3 (hardcopy) - ISBN 1-56347-752-1 (electronic) 1. Nuclear
9、 rockets-Research-United States. 2. Controlled fusion-Research-United States. 3. Prototypes, Engineering-Standards-United States. I. Title: Recommended design practices for conceptual nuclear fusion space propulsion systems. II. American Institute of Aeronautics and Astronautics. TL783.5.S66 2004 62
10、9.4753-dc22 2004028601 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 publication may be reproduced in any form, in an electronic retriev
11、al system or otherwise, without prior written permission of the publisher. Printed in the United States of America Copyright American Institute of Aeronautics and Astronautics Provided by IHS under license with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:5
12、2:53 MDTNo reproduction or networking permitted without license from IHS -,-,- AIAA SP-108-2004 iii Contents Foreword . iv 1 Introduction1 1.1 Scope 1 1.2 Purpose.1 1.3 Developments Focusing Attention on Nuclear Fusion Propulsion.1 2 Quantifying Figures of Merit.1 3 Recommended Ground Rules and Prac
13、tices for Credible Conceptual Designs.2 3.1 Design Reference Missions .3 3.2 Degree of Technological Extrapolation and Concomitant Risk4 3.3 Thoroughness in Calculating Mass Properties .6 3.3.1 Nominal Mass Property Template .7 3.3.2 Weight-Growth Contingency and Propellant Margins.10 3.3.3 Specific
14、 Impulse10 3.4 Thoroughness in Calculating Power Generation and Usage .11 3.4.1 Power-Flow .11 3.4.2 Jet Power-Loss and Auxiliary Power Contingencies 12 3.4.3 Specific Power 13 4 Summary.14 5 References14 Figures Figure 1 Relationships Among Example FOMs, Operating Parameters, and Recommendations on
15、 Mission/Vehicle Systems Characteristics2 Figure 2 Sample Generic Power Flow Diagram (all power values in MW “tbd”)12 Tables Table 1 Generic Mass Property Template for Nuclear Fusion Space Propulsion Systems .8 Copyright American Institute of Aeronautics and Astronautics Provided by IHS under licens
16、e with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:52:53 MDTNo reproduction or networking permitted without license from IHS -,-,- AIAA SP-108-2004 iv Foreword To facilitate the improvement and standardization of conceptual designs of nuclear fusion space
17、propulsion systems, Technical Interchange Meetings (TIM) took place in late 1999 and early 2000. The TIMs were broadly represented by the members of the National Aeronautics and Space Administration (NASA), the Department of Energy (DOE) laboratories, academia, and industry professionals active in t
18、he field. The TIMs were led by NASAs Glenn Research Center (GRC). At their conclusion, it was suggested and all agreed that the results of the TIMs should be offered to the appropriate AIAA Technical Committee (TC) to review and codify the recommended design practices into an appropriate AIAA techni
19、cal standard. The AIAA Nuclear and Future Flight Propulsion Technical Committee (NFFPTC) was identified as the most appropriate TC for this task. The NFFPTCs Chairman was approached and agreed to bring the TIMs product to the TC for their consideration. The NFFPTC subsequently formed an ad hoc worki
20、ng group for the expressed purpose of authoring an AIAA standards document to guide the development of higher quality conceptual designs for nuclear fusion space propulsion vehicles. Most of the recommendations stem from the work of the TIMs, with the balance contributed by the AIAA NFFPTC Fusion De
21、sign Working Group. The following participants in the Nuclear Fusion Propulsion Technical Interchange Meetings deserve special mention: Dr. Charles D. Orth DOE LLNL Dr. Peter J. Turchi DOE LANL Mr. Scott A. Carpenter EDEn-Corp Dr. John F. Santarius University of Wisconsin (Madison) Dr. Robert H. Fri
22、sbee NASA JPL Mr. Craig H. Williams Chair, NASA GRC Other contributors to the TIMs included: Dr. George H. Miley University of Illinois (Urbana-Champaign) Dr. Hiromu Momota University of Illinois (Urbana-Champaign) Dr. Jay E. Polk NASA JPL Dr. John Slough University of Washington Dr. Martin Peng DOE
23、 ORNL at PPPL Dr. Brice N. Cassenti United Technologies Mr. Joseph OToole DOE LANL Dr. Michael R. LaPointe Ohio Aerospace Institute at NASA GRC Dr. Frank J. Wessel University of California (Irvine) Ms. Carol Chao University of California (Irvine) Mr. Alex Cheung University of California (Irvine) Ms.
24、 Xia Liu EDEn-Corp Mr. Bryan A. Palaszewski NASA GRC Mr. Leonard A. Dudzinski NASA GRC Copyright American Institute of Aeronautics and Astronautics Provided by IHS under license with AIAA Licensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 04/18/2007 10:52:53 MDTNo reproduction or n
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- AIAA SP 108 2004
链接地址:https://www.31doc.com/p-3732800.html