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The concept of electric sailing Uranus beyond Voyager 2: from recent - - PowerPoint PPT Presentation

Feb 20, 2023 113 likes •243 views

The concept of electric sailing Uranus beyond Voyager 2: from recent advances to future missions Meudon Observatory, France, 16-18 September, 2013 Pekka Janhunen Finnish Meteorological Institute http://www.electric-sailing.fi 1

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The concept of electric sailing

Pekka Janhunen Finnish Meteorological Institute “Uranus beyond Voyager 2: from recent advances to future missions” Meudon Observatory, France, 16-18 September, 2013

http://www.electric-sailing.fi

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Contributors

Petri Toivanen, Jouni Envall, Jouni Polkko, Sini Merikallio, Henri Seppänen (Finnish Meteorological Institute), Pekka Salminen (SkyTron, Finland), Edward Haeggström, Timo Rauhala, Jukka Ukkonen, Göran Maconi, Anni Toppila (Univ. Helsinki, Finland), Sergiy Kiprich (NSC Kharkov Inst. Physics, Ukraine), Hannu Koivisto, Olli Tarvainen, Taneli Kalvas, Antti Nuottajärvi (Univ. Jyväskylä, Finland), Alexander Obraztsov (Univ. Eastern Finland at Joensuu, and Moscow State Univ.), Greger Thornell, Sven Wagner, Johan Sundqvist (ÅSTC, Uppsala, Sweden), Tor- Arne Grönland, Kristoffer Palmer (Nanospace AB, Uppsala, Sweden), Roland Rosta, Tim van Zöst (DLR-Bremen, Germany), Mart Noorma, Viljo Allik, Silver Lätt, Urmas Kvell (Univ. Tartu, Estonia), Giovanni Mengali, Alessandro Quarta, Generoso Aliasi (Univ. Pisa, Italy), Salvo Marcuccio, Pierpaolo Pergola, Nicola Giusti (Alta S.p.A., Pisa, Italy)

http://www.electric-sailing.fi

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Electric sail

  • Coulomb drag with natural solar wind

pushes spacecraft

  • Long, charged tethers (10-20 km, 25-50

μm wire, +20-40 kV)

  • Max 1 N thrust from <200 kg package (at

1 au; scales ~1/r)

  • Hardware is at TRL 4-5
  • ESTCube-1 is flying, waiting for

experiment to start... http://www.electric-sailing.fi

Janhunen et al., Rev. Sci. Instrum., 2010

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Plasma simulation of E-sail

(With nominal solar wind parametres at 1 au)

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Approximate thrust formula

V0 = 20 kV tether voltage V1 = 1 kV solar wind proton energy Pdyn = ρv² = 2 nPa solar wind dynamic pressure R = 100 m electron sheath radius rw = 1 mm effective electric width of tether ==> dF/dz = 500 nN/m thrust per tether length

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Tether manufacture

1 km tether (m=11 grams) 10 m ESTCube-1 tether http://www.electric-sailing.fi

Seppänen et al., Rev. Sci. Instrum., 2013

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Ultrasonic bonding tether factory

http://www.electric-sailing.fi

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ESTCube-1 mission

  • Estonia's first satellite
  • Launched May 8, 2013 with Vega to 670 km orbit
  • Will deploy 10 m tether, charge it to 500 V and measure

LEO E-sail effect by sync-deltaspin method http://www.electric-sailing.fi

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Aalto-1 mission (2014)

  • 3U CubeSat of Aalto University, Finland
  • Longer tether (100 m), higher voltage (1 kV)

http://www.electric-sailing.fi

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Some classes of E-sail applications

  • Multi-asteroid touring missions
  • Asteroid deflection (e.g. retrograde impactors, or gradually)
  • Non-Keplerian orbit missions
  • e.g., off-Lagrange point space weather monitoring
  • As a “booster” for outer solar system missions
  • Such as Uranus(!)
  • Replacement of gravity assist manoeuvres: faster & more

frequency launch windows & lower launch mass

  • Also outer-of-heliosphere missions

http://www.electric-sailing.fi

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Conclusions: where do we stand?

  • Propulsion revolution around the corner? May well be.
  • We are at TRL 4-5 now – it wasn't difficult to get here
  • We think we know how to build a 0.5-1 N, 100-200 kg sail
  • We need an in-orbit deployment demonstration
  • We need to measure the effect in the solar wind

http://www.electric-sailing.fi