InflateSail de-orbit flight demonstration results and follow-on drag-sail applications

被引:40
作者
Underwood, Craig [1 ]
Viquerat, Andrew [2 ]
Schenk, Mark [3 ]
Ben Taylor [1 ]
Massimiani, Chiara [1 ]
Duke, Richard [1 ]
Stewart, Brian [1 ]
Fellowes, Simon [1 ]
Bridges, Chris [1 ]
Aglietti, Guglielmo [1 ]
Sanders, Berry [4 ]
Masutti, Davide [5 ]
Denis, Amandine [5 ]
机构
[1] Univ Surrey, Surrey Space Ctr, Guildford GU2 7XH, Surrey, England
[2] Univ Surrey, Dept Mech Sci, Guildford GU2 7XH, Surrey, England
[3] Univ Bristol, Fac Engn, Bristol BS8 1TH, Avon, England
[4] HDES Serv & Engn, Mijnbouwstr 120, NL-2628 RX Delft, Netherlands
[5] Von Karman Inst Fluid Dynam, Waterloosesteenweg 72, B-1640 Rhode St Genese, Belgium
关键词
CubeSat; Drag-sail; Active debris removal; Post mission disposal; QB50;
D O I
10.1016/j.actaastro.2019.05.054
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The InflateSail (QB50-UK06) CubeSat, designed and built at the Surrey Space Centre (SSC) for the Von Karman Institute (VKI), Belgium, was one of the technology demonstrators for the European Commission's QB50 programme. The 3.2 kg 3U CubeSat was equipped with a 1 m long inflatable mast and a 10 m(2) deployable drag sail. InflateSail's primary mission was to demonstrate the effectiveness of using a drag sail in Low Earth Orbit (LEO) to dramatically increase the rate at which satellites lose altitude and re-enter the Earth's atmosphere and it was one of 31 satellites that were launched simultaneously on the PSLV (polar satellite launch vehicle) C-38 from Sriharikota, India on 23rd June 2017 into a 505 km, 97.44 degrees Sun-synchronous orbit. Shortly after safe deployment in orbit, InflateSail automatically activated its payload. Firstly, it inflated its metre-long metal-polymer laminate tubular mast, and then activated a stepper motor to extend four lightweight bi-stable rigid composite (BRC) booms from the end of the mast, so as to draw out the 3.1 m x 3.1 m square, 12 mu m thick polyethylene naphthalate (PEN) drag-sail. As intended, the satellite immediately began to lose altitude, causing it to re-enter the atmosphere just 72 days later - thus successfully demonstrating for the first time the de-orbiting of a spacecraft using European inflatable and drag-sail technologies. The InflateSail project was funded by two European Commission Framework Program Seven (FP7) projects: DEPLOYTECH and QB50. DEPLOYTECH had eight European partners including DLR, Airbus France, RolaTube, Cambridge University, and was assisted by NASA Marshall Space Flight Centre. DEPLOYTECH's objectives were to advance the technological capabilities of three different space deployable technologies by qualifying their concepts for space use. QB50 was a programme, led by VKI, for launching a network of 50 CubeSats built mainly by university teams all over the world to perform first-class science in the largely unexplored lower thermosphere. The mast/drag-sail technology developed by SSC will next be used on a third FP7 Project: RemoveDebris, launched in 2018, which will demonstrate the capturing and de-orbiting of artificial space debris targets using a net and harpoon system. This paper describes the results of the InflateSail mission, including the observed effects of atmospheric density and solar activity on its trajectory and body dynamics. It also describes the application of the technology to RemoveDebris and its potential as a commercial de-orbiting add-on package for future space missions.
引用
收藏
页码:344 / 358
页数:15
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