首页> 中文期刊> 《导弹与航天运载技术》 >CZ-2E火箭高空风弹道修正

CZ-2E火箭高空风弹道修正

         

摘要

here is larger effect of flow angle-of-attack caused by highaltitude wind on aerodynamic load and flight environment in rocket flighting. This effect can make flighting rocket flight fail sometimes. For improving rocket flight conditions as good as possible, in ballistic design, the ballistic design concept of decreasing flow angle-of-attack in rocket flighting i.e.to decreasing flow angle-of-attack in rocket flighting with ballistic correction method of high altitude wind can be used. The principle, the method and computing the correspending computation model of ballistic correction of high altitude wind are mainly introduced in this paper.%高空风引起的气流攻角对火箭飞行中的气动载荷和飞行环境有较大的影响。这种影响有时可造成火箭飞行失败。为尽可能地改善火箭的飞行条件,在弹道考虑上,可采用降低飞行中气流攻角的弹道设计方案——以高空风弹道修正法来降低飞行中的气流攻角。本文主要介绍的是高空风弹道修正的原理和方法以及相关的计算模型。

著录项

相似文献

  • 中文文献
  • 外文文献
  • 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