Full-Scale Testing of Portable and Automatic High Altitude Balloon Launching Platform

Nicholas Hennigan, Jonathan Reynolds, Kevin Hefner, Kyle Guerre, A. Stoica
{"title":"Full-Scale Testing of Portable and Automatic High Altitude Balloon Launching Platform","authors":"Nicholas Hennigan, Jonathan Reynolds, Kevin Hefner, Kyle Guerre, A. Stoica","doi":"10.1109/AERO55745.2023.10115690","DOIUrl":null,"url":null,"abstract":"This paper presents subsystem prototypes and tests of a novel design architecture to autonomously inflate and launch high altitude balloons (HABs). Three core subsystems were previously tested at reduced scale utilizing a 350-gram balloon; this paper test these subsystems at full scale, in the field, utilizing a full-scale, 1500-gram balloon. A first subsystem, the Balloon Capsule is a rigid container that utilizes a novel packing technique, allowing a latex balloon to be safely transported. Internal geometry of the capsule passively controls slack of the balloon during inflation. A second subsystem, the Helium Engagement and Locking System (HEL), oversees connecting the helium supply, locking the balloon in place, sensing lift values, and launching the balloon. A third subsystem, the Balloon Inflation Barrier (BiB), supports the balloon during inflation and prevents excessive deflection during high winds. Results from full scale compressed air testing showcased a need for a neoprene based internal retention mesh for the Balloon Capsule. Both the HEL and BiB performed satisfactorily. Helium tests concluded the Balloon Capsule performed as designed in light winds and failed at medium winds due to the excessive unreeling of balloon slack. The HEL system was actuated manually and successfully locked, inflated, and released a full scale 1500- gram balloon with lift values exceeding 2.26 kg. The BiB performed as expected when balloons were fully inflated, however, during inflation, BiB's failed at high winds due to structure buckling and excessive balloon slack. The full scale autolauncher prototype weighs less than 11 kg and is 1.2 m long, 1.2 m wide, and 1.1 m tall. This design allows one person to inflate and launch a balloon in under 30 mins. Critical elements of future work include the refinement of BiB structure, the automation of the HEL system, and implementation of the helium gas control logic; and the design of balloon payload storage system.","PeriodicalId":344285,"journal":{"name":"2023 IEEE Aerospace Conference","volume":"200 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-03-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO55745.2023.10115690","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

This paper presents subsystem prototypes and tests of a novel design architecture to autonomously inflate and launch high altitude balloons (HABs). Three core subsystems were previously tested at reduced scale utilizing a 350-gram balloon; this paper test these subsystems at full scale, in the field, utilizing a full-scale, 1500-gram balloon. A first subsystem, the Balloon Capsule is a rigid container that utilizes a novel packing technique, allowing a latex balloon to be safely transported. Internal geometry of the capsule passively controls slack of the balloon during inflation. A second subsystem, the Helium Engagement and Locking System (HEL), oversees connecting the helium supply, locking the balloon in place, sensing lift values, and launching the balloon. A third subsystem, the Balloon Inflation Barrier (BiB), supports the balloon during inflation and prevents excessive deflection during high winds. Results from full scale compressed air testing showcased a need for a neoprene based internal retention mesh for the Balloon Capsule. Both the HEL and BiB performed satisfactorily. Helium tests concluded the Balloon Capsule performed as designed in light winds and failed at medium winds due to the excessive unreeling of balloon slack. The HEL system was actuated manually and successfully locked, inflated, and released a full scale 1500- gram balloon with lift values exceeding 2.26 kg. The BiB performed as expected when balloons were fully inflated, however, during inflation, BiB's failed at high winds due to structure buckling and excessive balloon slack. The full scale autolauncher prototype weighs less than 11 kg and is 1.2 m long, 1.2 m wide, and 1.1 m tall. This design allows one person to inflate and launch a balloon in under 30 mins. Critical elements of future work include the refinement of BiB structure, the automation of the HEL system, and implementation of the helium gas control logic; and the design of balloon payload storage system.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
便携式自动高空气球放飞平台的全尺寸试验
本文介绍了一种新型高空气球自主充气发射设计体系的分系统原型和试验。三个核心子系统先前在一个350克的气球上进行了缩小规模的测试;本文利用一个重达1500克的全尺寸气球,在现场对这些子系统进行了全尺寸测试。第一个子系统,气球胶囊是一个刚性容器,利用一种新颖的包装技术,允许乳胶气球安全运输。胶囊的内部几何结构被动地控制气球在膨胀过程中的松弛度。第二个子系统是氦气接合和锁定系统(HEL),负责连接氦气供应、将气球锁定到位、感知升力值并发射气球。第三个子系统,气球膨胀屏障(BiB),在膨胀过程中支撑气球,防止在大风时过度偏转。全尺寸压缩空气测试的结果表明,需要一种基于氯丁橡胶的气球胶囊内部保留网。HEL和BiB均表现良好。氦气测试得出结论,气球胶囊在微风中表现良好,在中等风中由于气球松弛过度而失败。手动启动HEL系统,成功锁定、充气并释放了一个1500克的全尺寸气球,升力值超过2.26千克。当气球完全充气时,BiB的性能与预期一致,但在充气过程中,由于结构弯曲和气球过度松弛,BiB在大风中失效。全尺寸自动发射装置原型重量小于11公斤,长1.2米,宽1.2米,高1.1米。这种设计可以让一个人在30分钟内给气球充气并放飞气球。未来工作的关键要素包括BiB结构的细化、HEL系统的自动化和氦气控制逻辑的实现;以及气球载荷存储系统的设计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
The Mission for Education and Multimedia Engagement: Breaking the Barriers to Satellite Education TID Testing of COTS-based, Two-Phase, Point-of-Load Converters for Aerospace Applications Point-Source Target Detection and Localization in Single-Frame Infrared Imagery Comparative Analysis of Different Profiles of Riblets on an Airfoil using Large Eddy Simulations A Receiver-Independent GNSS Smart Antenna for Simultaneous Jamming and Spoofing Protection
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1