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Progress of super-pressure balloon development: A new “tawara” concept with improved stability
Authors:H Fuke  N Izutsu  D Akita  I Iijima  Y Kato  J Kawada  K Matsushima  Y Matsuzaka  E Mizuta  M Namiki  N Nonaka  S Ohta  Y Saito  T Sato  M Seo  Y Shoji  A Takada  K Tamura  M Toriumi  K Yamada  T Yamagami  T Yoshida
Institution:1. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (ISAS/JAXA), Sagamihara, Kanagawa 252-5210, Japan;2. The Fujikura Parachute Co. Ltd., Shinagawa, Tokyo 142-0063, Japan
Abstract:The super-pressure balloon (SPB) has been expected to be a flight vehicle that can provide a long flight duration to science. Since 1997, we have developed the SPB. Now we are at the phase of developing an SPB of a practical size. In 2009, we carried out a test flight of a pumpkin-shaped SPB with a 60,000 m3 volume. The undesirable result of this flight aroused us to resolve the deployment instability of the pumpkin-shaped SPB, which has been known as one of the most challenging issues confronting SPB development. To explore this deployment issue, in 2010, we carried out a series of ground tests. From results of these tests, we found that an SPB design modified from pumpkin, named “tawara”, can be a good candidate to greatly improve the deployment stability of the lobed SPB.
Keywords:Scientific balloon  Stratosphere  Super-pressure  Tawara  Membrane structure  Deployment stability
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