Reel.SMRT: A feasibility analysis of a novel balloon-borne platform for low-gravity experimentation

M. Jandak*, K. M. Bennell, M. E.R. Fittock, D. Leal Martinez, C. J. Pegg, S. M. Persson, J. Speidel, N. Termtanasombat

*Corresponding author for this work

    Research output: Chapter in Book/Report/Conference proceedingConference article in proceedingsScientificpeer-review

    Abstract

    A balloon-borne platform that can drop and reel back up a tethered payload and perform this multiple times, may have the potential to significantly expand the scope of balloon-based experimentation and low gravity platforms. The reel.SMRT Project is a mission that was launched on a Stratospheric Balloon in October 2009 from Esrange Space Center following an 8-month development period as part of the BEXUS-9 campaign (Balloon-borne Experiments for University Students). Through this programme, reel.SMRT investigated the feasibility of such a platform. The vision is that the platform may be ultimately up-scaled to provide a viable and cost-effective alternative to parabolic flights and drop towers. It has the potential to drastically increase the maximum drop lengths and versatility of such systems, along with more frequent drops and a greater number of drops in a single mission. The reel.SMRT system also has secondary applications for balloon experimentation, such as a controlled lowering of a payload, via which it is possible to take measurements further from the gondola, increasing experimental sampling range. Other advantages of an up-scaled system would include: capability for large-dimension payloads such as antenna deployment tests; multiple drops to gain more test data; and variable payload acceleration to simulate Martian or Lunar conditions. Additionally, the tether has applications as a safety line for unmanned aerial vehicle experimentation, or for lowering a sensor or object to near the surface for a low-altitude mission (such as in Martian exploration). The project's simulations have shown that with minimal tension, milli-gravity performance is limited only by drag of the lower atmosphere after kilometres of drop distance. Challenges to implementation included sensor sensitivity and sampling rates as well as the rate of the line coming off the spool. For this feasibility analysis, the system had a 30m drop length (70m total reel length) and 5G braking force, to demonstrate the quality of the low gravity environment for a dropped payload without actuators, using commercial off-the-shelf components including standard fishing tackle and line as the reeling mechanism, on a low budget.

    Original languageEnglish
    Title of host publication61st International Astronautical Congress 2010, IAC 2010
    Pages10315-10323
    Number of pages9
    Volume12
    Publication statusPublished - 1 Dec 2010
    MoE publication typeA4 Conference publication
    EventInternational Astronautical Congress - Prague, Czech Republic
    Duration: 27 Sept 20101 Oct 2010
    Conference number: 61

    Conference

    ConferenceInternational Astronautical Congress
    Abbreviated titleIAC
    Country/TerritoryCzech Republic
    CityPrague
    Period27/09/201001/10/2010

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