2006
DOI: 10.1016/j.actaastro.2005.07.024
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Heliopause Explorer—a sailcraft mission to the outer boundaries of the solar system

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Cited by 36 publications
(28 citation statements)
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“…In order to explore the structure and properties of the heliospheric interface it is, however, necessary to get in-situ observations from the heliopause and the region beyond. Therefore, a 'Heliopause Explorer' mission (Leipold et al, 2003), now called Interstellar Heliopause Probe (IHP, see Falkner (2005), Lyngvi et al (2005a) and Lyngvi et al (2005b)), can represent the next step in the exploration of the outer boundaries of the heliosphere.…”
Section: Introductionmentioning
confidence: 99%
“…In order to explore the structure and properties of the heliospheric interface it is, however, necessary to get in-situ observations from the heliopause and the region beyond. Therefore, a 'Heliopause Explorer' mission (Leipold et al, 2003), now called Interstellar Heliopause Probe (IHP, see Falkner (2005), Lyngvi et al (2005a) and Lyngvi et al (2005b)), can represent the next step in the exploration of the outer boundaries of the heliosphere.…”
Section: Introductionmentioning
confidence: 99%
“…In particular, a 21.2 year, 0.75 mm/s 2 ideal sail trajectory has been presented, that spirals down to 0.37 AU and then executes a dual photonic assist, however the closest solar approach is just 0.1 AU, placing severe thermal loads on the spacecraft and sail assembly [15]. The mission scenario considered herein shall use the sail from Earth departure until it is jettisoned at 5 AU, as per requirement 5, and shall apply a strict solar approach limit of 0.25 AU due to the thermal effects on the sail as discussed previously.…”
Section: Trajectory Design For the Interstellar Heliopause Probementioning
confidence: 99%
“…Recent trajectories considered by Leipold, et al and ESA-ESTEC have considered lower performance sails to achieve a slower transit to 200 AU with a conventional 3-axis stabilized square sail, with DLR (Deutsches Zentrum für Luft-und Raumfahrt; the German Centre for Air and Space Flight) derived composite booms [15,[28][29][30]. In particular, a 21.2 year, 0.75 mm/s 2 ideal sail trajectory has been presented, that spirals down to 0.37 AU and then executes a dual photonic assist, however the closest solar approach is just 0.1 AU, placing severe thermal loads on the spacecraft and sail assembly [15].…”
Section: Trajectory Design For the Interstellar Heliopause Probementioning
confidence: 99%
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