<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="6.x">Drupal-Biblio</source-app><ref-type>47</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Wright, R L</style></author><author><style face="normal" font="default" size="100%">Detyder, D D</style></author><author><style face="normal" font="default" size="100%">Ferebee, M J</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1622. Conceptual Spacecraft Systems Design and Synthesis</style></title><secondary-title><style face="normal" font="default" size="100%">43rd Annual Conference, Atlanta, Georgia, May 21-23</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">18. Weight Engineering - Spacecraft Design</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1984</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/21/84</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">http://www.sawe.org/store/product_info.php?products_id=44009</style></url></web-urls></urls><publisher><style face="normal" font="default" size="100%">Society of Allied Weight Engineers, Inc.</style></publisher><pub-location><style face="normal" font="default" size="100%">Atlanta, Georgia</style></pub-location><pages><style face="normal" font="default" size="100%">31</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">An interactive systems design and synthesis is performed on future spacecraft concepts using the Interactive Design and Evaluation of Advanced Systems (IDEAS) computer-aided design and analysis system. The capabilities and advantages of the systems-oriented interactive computer-aided design and analysis system are described. The synthesis of both large antenna and space station concepts, and space station evolutionary growth designs is demonstrated The IDEAS program provides the user with both an interactive graphics and an interactive computing capability which consists of over 40 multidisciplinary synthesis and analysis modules. Thus, the user can create, analyze, and conduct parametric studies and modify Earth-orbiting spacecraft designs (space stations, large antennas or platforms, and technologically advanced spacecraft) at an interactive terminal with relative ease. The IDEAS approach is useful during the conceptual design phase of advanced space missions when a multiplicity of parameters and concepts must be analyzed and evaluated in a cost-effective and timely manner. </style></abstract><work-type><style face="normal" font="default" size="100%">18. WEIGHT ENGINEERING - SPACECRAFT DESIGN</style></work-type><accession-num><style face="normal" font="default" size="100%">1622</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $19.53. Members may download this paper for free. &lt;a href=&quot;http://www.sawe.org/dms&quot;&gt;Click here&lt;/a&gt;. (Login Required. See SAWE &lt;a href=&quot;http://www.sawe.org/faq&quot;&gt;Frequently Asked Questions&lt;/a&gt;.)</style></custom1><custom3><style face="normal" font="default" size="100%">19.53</style></custom3></record></records></xml>