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Published byDamon Wilson Modified over 7 years ago
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Ingo Mayer, Philipp Ludewig, Johannes Kugele, Alex Schmidt
REXUS 17/18 SMARD Shape Memory Alloy Reusable Deployment Mechanism Hello -> Team SMARD Vorstellung: Philipp -> Struktur Johannes -> Elektronik Ingo -> Software Alex -> Software Ingo Mayer, Philipp Ludewig, Johannes Kugele, Alex Schmidt
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Team - SMARD New team picture taken at our university 24.06.2014
SMARD – CDR
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Mission Statement Develop and verify a solar panel hold down release mechanism for a CubeSat using Shape Memory Alloys on REXUS 18. Mission Statement -> vorlesen SMARD – CDR
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Esrange Kiruna REXUS Length: 5.6m ∅: 35.6cm Payload Mass: 40kg
2 min with reduced gravity REXUS is an unguided, spin-stabilised, solid-propellant, single stage rocket. Each flight carries a payload consisting solely of student experiments. SMARD – CDR
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1.2 Mechanical Design - Overview
Gravity SMARD – CDR
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1.2 Mechanical Design - Experiment Frame
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1.2 Mechanical Design - Experiment Frame
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1.2 Mechanical Design - Experiment Frame
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1.2 Mechanical Design - Solar Panel
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1.2 Mechanical Design – HDRM
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1.2 Mechanical Design - HDRM
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1.2 Mechanical Design - HDRM
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1.2 Mechanical Design - HDRM
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Voraussichtliche Kosten
Flug pro Person: ca. 400€ Hotel pro Person: Ca. 70€ die Nacht Kampagne 12Tage: 840€ Ca. 1240€ Kosten pro Person Nicht geförderte Teammitglieder: 5 SMARD – CDR
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Thank you for your attention!
SMARD – CDR
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