首页> 外文OA文献 >Attitudes of the Antarctic Sounding Rocket Vehicles
【2h】

Attitudes of the Antarctic Sounding Rocket Vehicles

机译:南极探空火箭车辆的态度

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

The attitudes of the 12 sounding rockets which were launched at Syowa Station in Antarctica from May 1972 to August 1973 were determined by geomagnetic aspect sensors. The attitudes of the latest launched sounding rockets, S-210JA-22 and S-310JA-1 were also determinated. The three-dimensional orientation of the S-210JA-22 rocket axis was obtained by the geomagnetic aspect sensors and the solar aspect sensor. The result shows that the precessional motion of the S-210JA-22 vehicle included the geomagnetic field line. The spin frequency of these 14 vehicles was mostly in the range from 1.1 to 1.3Hz and their conical (precessional) half angle was mostly from 20 to 60 degrees, with the conical rotational period mostly from 50 to 120 seconds.
机译:1972年5月至1973年8月在南极洲Syowa站发射的12枚探空火箭的姿态由地磁纵横比传感器确定。还确定了最新发射的探空火箭S-210JA-22和S-310JA-1的态度。 S-210JA-22火箭轴的三维方向是通过地磁纵横比传感器和太阳纵横比传感器获得的。结果表明,S-210JA-22车辆的进动包括地磁场线。这14辆车的旋转频率通常在1.1到1.3Hz的范围内,并且它们的圆锥形(进动)半角通常在20到60度之间,圆锥形旋转周期通常在50到120秒之间。

著录项

  • 作者

    TohyamaFumio; AoyamaIwao;

  • 作者单位
  • 年度 1978
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

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