首页> 美国政府科技报告 >Preliminary Design of an Auxiliary Power Unit for the Space Shuttle. Volume 3 Details of System Analysis, Engineering, and Design for Selected System
【24h】

Preliminary Design of an Auxiliary Power Unit for the Space Shuttle. Volume 3 Details of System Analysis, Engineering, and Design for Selected System

机译:航天飞机辅助动力装置的初步设计。第3卷所选系统的系统分析,工程和设计细节

获取原文

摘要

Numerous candidate APU concepts, each meeting the space shuttle APU problem statement are considered. Evaluation of these concepts indicates that the optimum concept is a hydrogen-oxygen APU incorporating a recuperator to utilize the exhaust energy and using the cycle hydrogen flow as a means of cooling the component heat loads. (Author)

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号