Study of environment analysis and thermodynamic on Venus balloon

LEI Yan-peng; YANG Chun-xin

Chinese

您当前的位置：

首页 >

文章列表页 >

Study of environment analysis and thermodynamic on Venus balloon

更新时间：2026-07-07

- Study of environment analysis and thermodynamic on Venus balloon
- Vol. 27, Issue 11, (2012)
- 作者机构：
  
  北京航空航天大学航空科学与工程学院,北京,100191
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2012
- 稿件说明：
移动端阅览
LEI Yan-peng, YANG Chun-xin. Study of environment analysis and thermodynamic on Venus balloon[J]. 2012, 27(11).
DOI：

LEI Yan-peng, YANG Chun-xin. Study of environment analysis and thermodynamic on Venus balloon[J]. 2012, 27(11). DOI：

摘要

分析了金星独特的大气环境

归纳了影响金星气球飞行的主要环境因素

并建立了数学模型.依据金星气球的投放、飘浮程序

设计了金星原型氦气球

设计驻留高度为35km.建立了金星气球热动力仿真平台.计算结果表明:金星气球在30~40km高度释放

可快速到达驻留高度并作长期飘浮;金星气球系统的温度范围为440~520K

最大速度低于10m/s.这为进一步开展对金星气球的研究提供了依据.

Abstract

The Venus atmospheric environment was described with mathematical model.The Venus balloon thermodynamic model was established.Then

the floating process of a helium prototype balloon

of which the floating altitude was designed as 35km

was numerically designed by this model.The results show that when the Venus balloon is released at the altitude between 30km and 40km

it can reach floating altitude quickly and keep long-term floating

the balloon system should endure the temperature between 440K and 520K

its instantaneous maximum speed is less than 10m/s.This research would provide basis for the further development of Venus balloon further development.

关键词

Keywords

references

Views

494

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Influence of temperature on torque properties of miniature flexible joint

Aerothermodynamic analysis of spacecraftduring its atmospheric reentry flight

Experiment on heat exchange and cooling of pulse detonation engine detonation tube wall

Transient behavior analysis of adiabatic thermal elasto-hydrodynamic lubrication of journal bearing under step load

Study on adiabatic transient behavior of tilting-pad journal bearing

Related Author

杨敬贤

刘宇

郑开发

任军学

苏浩

SONG Bao-yin

LUO Zu-fen

HUANG Xi-qiao

Related Institution

北京航空航天大学宇航学院

中国航天科技集团公司上海航天技术研究院上海航天动力技术研究所

College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics

School of Power and Energy,Northwestern Polytechnical University

College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰