Referenzen

Projekte









Partner



 

   
















Veröffentlichungen

    2003

  • IIn Orbit Bonding (IOB) of Long Deployable Structures, 2003
    T. Schmidt, K. Seifart, F. Burger, J.Eder
    Proceedings of the 10th European Space Mechanisms and Tribology Symposium; ESA SP-524

    2005

  • Deployable structure for flexible solar generators, 2005
    K. Seifart, W. Göhler, T. Schmidt, R. John, S. Langlois
    Proceeding of the European Conference on Spacecraft Structures, Materials & Mechanical Testing; ESA SP-581
  • Structural Design of Flexible Solar Generators, 2005
    K. Seifart, T. Schmidt, W. Göhler, S. Langlois;
    Proceedings of the 7th European Space Power Conference; ESA SP-589.
  • Thin Film Demonstrator: A First Step toward Thin Film Solar Array, 2005
    M. L. Fille, R. Zwannenburg, S. Brunner, K. Otte, P. Greff;
    Proceeding of the 7th European Space Power Conference; ESA SP-589.

    2007

  • Testing of Flexible Cu(In,Ga)Se2 Solar Cells for Space Applications, 2007
    K. Zajac, S. Fasoulas, S. Brunner, K. Seifart, K. Otte;
    Proceedings of the 1st CEAS European Air and Space Conference; CEAS-2007-165, pp. 1817 – 1822.
  • Advancement of Multifunktional support structure technologies (AMFSST), 2007
    R. John, HTS GmbH Germany; G. Atxaga, Inasmet Spain; H.J. Frerker, OHB Systems AG; A. Newerla, European Space Agency ESTEC Netherlands;
    Proceedings, International Workshop on thermal investigations of ICs and systems.
  • Ultra Light Self-Motorized Mechanism for Deployment of Light-Weight Reflector Antennas and appendages, 2007
    C. Boesch, C. Pereira, RUAG Aerospace Switzerland; R. John, T. Schmidt, K. Seifart, HTS GmbH Germany; J.M. Lautier, European Space Agency ESTEC Netherlands;
    Proceedings, 12th European Space Mechanisms and Tribology Symposium.
  • Simulation of Ultra Light Self-Motorized Mechanism for Deployment of Light-Weight Reflector Antenna, 2007
    R. John, T. Schmidt, K. Seifart, H. Sparr, HTS GmbH Germany;
    Proceedings, ANSYS Conference & 25th CADFEM Users' Meeting.

    2008

  • Testing of Cu(In,Ga)Se2 Solar Cells on Flexible Substrates for Space Applications, 2008
    K. Zajac, S. Fasoulas, K. Seifart, S. Brunner, K. Otte, C. Scheit;
    Proceedings of the 23rd European Photovoltaic Solar Energy Conference and Exhibition, 1DV.3.4, pp. 768 – 772.
  • The German Joint Project ‘Flexible CIGSe Thin Film Solar Cells for Space Flight’, 2008
    K. Zajac, S. Brunner, R. John, C. A. Kaufmann, K. Otte, A. Rahm, F. Kessler;
    Proceedings of the 8th European Space Power Conference, ESA SP-661.
  • Ground Based Space Environment Test of Flexible Cu(In,Ga)Se2 Solar Cells, 2008
    K. Zajac, S. Brunner, K. Seifart, K. Otte;
    Proceedings of the 8th European Space Power Conference, ESA SP-661.
  • Investigation on Thin Film Solar Array Using Lock-In Thermography, 2008
    S. Brunner, K. Zajac, K. Seifart;
    Proceedings of the 8th European Space Power Conference, ESA SP-661.
  • Ultra Light Self-Motorized Mechanism for Deployment of Light Weight Space Craft Appendages, 2008
    C. Boesch, C. Pereira, RUAG Aerospace Switzerland; R. John, T. Schmidt, K. Seifart, H. Sparr HTS GmbH Germany; J.M. Lautier, European Space Agency ESTEC Netherlands; T. Pyttel University of Applied Sciences Friedberg Germany;
    Proceedings, 39th Aerospace Mechanisms Symposium.

    2009

  • Qualitätssicherung an Solarzellen Modulen durch Lock-in Thermographie, 2009
    S. Brunner, K. Zajac, L. Haupt, B. Köhler, M. Küttner, F. Raddatz;
    Thermographie-Kolloquium der Deutschen Gesellschaft für Zerstörungsfreie Prüfung e.V..
  • The German Joint Project ‘Flexible CIGSe Thin Film Solar Cells for Space Applications’, 2009
    R. Caballero, C.A. Kaufmann, R. Klenk, H.W. Schock, K. Zajac, S. Brunner, R. John, A. Rahm, H. Zachmann, C. Scheit, A. Braun, K. Otte, M. Wagner, R. Würz, F. Kessler, P. Schülke;
    Proceedings of the 24th European Photovoltaic Solar Energy Conference and Exhibition; 1DV.5.8, pp. 707 – 710.
  • New Findings of the German Joint Project ‘Flexible CIGSe Thin Film Solar Cells for Space Flight’, 2009
    K. Zajac, S. Brunner, C. A. Kaufmann, R. Caballero, A. Rahm, C. Scheit, H. Zachmmann, F. Kessler, M. Wagner;
    Proceedings of the 34th IEEE Photovoltaic Specialists Conference; pp. 55 - 59.

    2010

  • Latest Results of the German Joint Project “Flexible CIGSe Thin Film Solar Cells for Space Applications”, 2010
    K. Zajac, S. Brunner, C. A. Kaufmann, R. Caballero, H.-W. Schock, A. Rahm, C. Scheit, H. Zachmann, F. Kessler, R. Wuerz, P. Schülke
    Proceedings of the 35th IEEE Photovoltaic Specialists Conference; pp. 16 - 19
  • Recent Results of the German Joint Project "Flexible CIGSe Thin Film Solar Cells for Space Applications", 2010
    C.A. Kaufmann, R. Caballero, R. Klenk, H.-W. Schock, K. Zajac, S. Brunner, A. Rahm, C. Scheit, H. Zachmann, A. Braun, K. Otte, R. Würz, F. Kessler, P. Schülke
    Proceedings of the 25th European Photovoltaic Solar Energy Conference and Exhibition; 3DO.4.5, pp. 2849 - 2853
  • Investigation on Flexible Thin Film Solar Cells Using Lock-in Thermography and Electroluminescence, 2010
    K. Zajac, S. Brunner, K. Seifart, N. Löcher, M. Münch, M. Meißner, C. Scheit, L. Hartmann
    Proceedings of the 25th European Photovoltaic Solar Energy Conference and Exhibition; 3BV.2.7, pp. 3331 - 3334

    2011

  • Recent Progress towards Space Applications of Thin Film Solar Cells – The German Joint Project ‘Flexible CIGSe Thin Film Solar Cells for Space Flight’ and OOV
    S. Brunner, K. Zajac, M. Nadler, K. Seifart, C. A. Kaufmann, R. Caballero, H.-W. Schock, L. Hartmann, K. Otte, A. Rahm, C. Scheit, H. Zachmann, F. Kessler, R. Wuuml;rz, P. Schuuml;lke
    Proceedings of the 9th European Space Power Conference; ESA SP-690
  • A High-Precision, High-Reliability Binary Rotary Encoder using Hall-Effect Sensors, 2011
    S. Kottmeier, S. Muuml;ller, T. Schmidt, K. Zajac, M. Schmalbach
    Proceedings of the 14th European Space Mechanisms and Tribology Symposium; ESA SP-698; pp. 395 – 401
  • Development of a Two Hinge Shutter and Calibration Mechanism, 2011
    M. Schmalbach, M. Eigenmann, T. Schmidt
    Proceedings of the 14th European Space Mechanisms and Tribology Symposium; ESA SP-698; pp. 431 – 434
  • Simulating and Analysing the Microvibration Signature of Reaction Wheels for Future Non-Intrusive Health Monitoring Methods, 2011
    R. Hahn, R. Seiler
    Proceedings of the 14th European Space Mechanisms and Tribology Symposium; ESA SP-698; pp. 415 – 422
  • Development of a Fine Pointing and Trim Mechanism, 2011
    A. Vuilleumier, M. Eigenmann, A. Bergander, T. Blais, L. Scolamiero
    Proceedings of the 14th European Space Mechanisms and Tribology Symposium; ESA SP-698; pp. 451 – 454
  • Ultra-Light Deployment Mechanism (UDM) for Sectioned Large Deployable Antenna Reflectors, 2011
    M. Eigenmann, M. Schmalbach, M. Schiller, T. Schmidt, L. Scolamiero
    Proceedings of the 14th European Space Mechanisms and Tribology Symposium; ESA SP-698; pp. 479 – 484
  • Development of a Two Hinge Shutter and Calibration Mechanism, 2011
    M. Schmalbach, M. Eigenmann, T. Schmidt
    Proceedings of the 14th European Space Mechanisms and Tribology Symposium; ESA SP-698; pp. 509 – 512

    2012

  • Recent EM Testing Results for Ultra-light Deployment Mechanism (UDM) for sectioned large Deployable Antenna Reflectors, 2011
    T. Schmidt, M. Schiller, M. Schmalbach, A. Fix, L. Scolamiero
    Proceedings of the Workshop on Large Deployable Antennas; ESA

    2013

  • Verification Test for Ultra-Light Deployment Mechanism for Sectioned Deployable Antenna Reflectors, 2013
    K. Zajac, T. Schmidt, M. Schiller, K. Seifart, M. Schmalbach, L. Scolamiero
    Proceedings of the 15th European Space Mechanisms and Tribology Symposium; ESA SP-718; ESA
  • New Results of the Flexible Thin Film Solar Cell Panel on TET-1
    K. Zajac, S. Brunner, K. Seifart, L. Hartmann, L. Wägele, K. Otte
    62. Deutscher Luft- und Raumfahrtkongress, Stuttgart; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2013

    2014

  • Bis zur Unendlichkeit
    K. Zajac
    audimax ING. 04.2014, audimax Medien GmbH
  • Design and Testing of a Flexible Solar Generator for On-Orbit Verification Mission
    S. Langendorf, S. Brunner, K. Zajac
    Proceedings of the 13th European Conference on Spacecraft Structures, Materials & Environmental Testing; ESA SP-727; 2014
  • In-Flight Results of the Flexible Solar Cell Panel on TET-1
    S. Brunner, K. Zajac, K. Seifart, L. Hartmann, K. Otte
    Proceedings of the 10th European Space Power Conference; ESA SP-719; 2014
  • Flexible Solar Generator for On-Orbit Verification on a Small Satellite Mission
    S. Langendorf, S. Brunner, K. Zajac
    Proceedings of the 4S Symposium; ESA SP-; 2014
  • Flexible Cu(In,Ga)Se2 Thin Film Solar Cells for Space Applications - Recent Results from a German Joint Project
    C.A. Kaufmann, D. Greiner, S. Harndt, R. Klenk, S. Brunken, R. Schlatmann & H.-W. Schock, K. Zajac, S. Brunner, F. Daume, C. Scheit, A. Rahm, R. Würz, F. Kessler, M. Günthner, M. Pscherer, S. Ihlow, G. Motz, H. Morgner, R.G. Schmidt, A. Lambrecht, J.T. Grundmann, P. Spietz, P. Schülke
    Proceedings of the 29th European Photovoltaic Solar Energy Conference and Exhibition; 3AO.5.4
  • Design of a Flexible Solar Generator for on-Orbit Verification of Flexible CIGSe Thin Film Solar Cells
    K. Zajac, S. Brunner, S. Langendorf
    Proceedings of the 29th European Photovoltaic Solar Energy Conference and Exhibition; 4DO.13.2

    2015

  • A Small Satellite Radar Earth Observation Mission with a Large Deployable Antenna
    A. Nicolai, R. Eberwein, C. Raschke, O. Reichmann, M. Lori, J. Schmidt, A. Ihle, T. Schmidt, K. Zajac
    Proceedings of the 10th IAA Symposium on Small Satellites for Earth Observation; IAA-B10-0308P
  • Multiaxialer Entfaltungs- und Positioniermechanismus für Hochleistungsantennen
    K. Zajac, T. Endler, C. Raum, T. Schmidt
    4. Nationale Konferenz Satellitenkommunikation in Deutschland
  • Design, Qualification and Lessons Learned of Shutter Calibration Mechanism for EnMAP Mission
    T. Schmidt, S. Müller, A. Bergander, K. Zajac, K. Seifart
    Proceedings of the 16th European Space Mechanisms and Tribology Symposium
  • Mechanical Testing on the Core Sample Transportation Mechanism of the ExoMars 2018 Mission
    C. Melzer, A. A. Cubillo, M. Nadler, F. Pfitzner, R. Hahn
    Proceedings of the 16th European Space Mechanisms and Tribology Symposium
  • Development of Magneto-Resistive Angular Position Sensors for Space Applications
    R. Hahn
    Proceedings of the 16th European Space Mechanisms and Tribology Symposium
  • Design, Qualification and Lessons Learned of SWIR Switch Mechanism for EnMAP Misson
    K. Zajac, J. Richter, T. Schmidt, S. Müller, A. Bergander, K. Seifart
    Deutscher Luft- und Raumfahrtkongress 2015, Rostock; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2015 URN: urn:nbn:de:101:1-201510233215
  • Development of an External Secondary Payload Unit for Time Resolved Atomic Oxygen Measurement
    K. Zajac, A. Riemer, T. Schmiel, T. Henschel, A. Hilgers
    Deutscher Luft- und Raumfahrtkongress 2015, Rostock; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2015 URN: urn:nbn:de:101:1-201510233224
  • Design and Development of a Deployable Membrane for Passive Deorbiting Systems
    R. Hahn
    CleanSat Workshop, 18.03.2015, ESA/ESTEC

    2016

  • Dynamische Mehrkörpersimulation eines passiv angetriebenen Entfaltungsmechanismus für Raumfahrtanwendungen
    C. Holzapfel, R. Hahn
    Deutschsprachige NAFEMS Regionalkonferenz 2016: Berechnung und Simulation – Anwendungen, Entwicklungen, Trends; 25. - 27. April 2016, Bamberg
  • Development of a Magneto-Resistive Angular Position Sensor for Space Mechanisms
    R. Hahn, T. Schmidt, K. Seifart, R. Slatter, B. Olberts, F. Romera
    Proceedings of the 43rd Aerospace Mechanisms Symposium, NASA Ames Research Center, May 4-6, 2016
  • Time Resolved Atomic Oxygen Measurement in the Atmosphere with the Payload unit APOLLON
    K. Zajac, A. Riemer, T. Schmiel, T. Henschel, A. Hilgers
    65. Deutscher Luft- und Raumfahrtkongress – Braunschweig, 13. – 15. Sep. 2016 URN: urn:nbn:de:101:1-201609234918
  • Design, Analysis and Testing of a Deployable Membrane for a passive De-Orbiting System
    R. Hahn, A. Riemer, T. Sinn, P. Seefeldt, S. Meyer, T. Spröwitz, M. Sznajder, M. Zander , L. Tiedemann, T. Cardone, R. Knockaert
    Clean Space Industry Days (23. –27.05.2016), ESA ESTEC
  • ADEO -Architectural Design and Testing of De-orbiting Subsystem (GSTP)
    T. Sinn, P. Seefeldt, A. Riemer, S. Meyer, T. Spröwitz, R. Hahn, M. Zander, L. Tiedemann, K. D. Bunte, T. Cardone, D. Teti;
    Clean Space Industry Days (23. –27.05.2016), ESA ESTEC

    2017

  • Development of Magneto-Resistive Angular Position Sensors for Space Mechanisms
    R. Hahn, T. Schmidt, K. Seifart, B. Olberts, F. Romera
    Proceedings of the 14th Symposium – Magnetoresistive Sensors and Magnetic Systems, Wetzlar, 21. – 22.03.2017
  • Entwicklung, Test und Lessons Learned des Multiaxialen Entfaltungs und Positioniermechanismus MEP
    K. Zajac, T. Endler, C. Raum, T. Schmidt
    Nationale Konferenz Satellitenkommunikation in Deutschland, Bonn, 28.–29.03.2017
  • Breadboard Test Results and Lessons Learned of Magneto-Resistive Positions Sensors for Space Allications
    T. Schmidt
    2017 Mechanisms Final Presentation Days, ESA ESTEC, 30. – 31.03.2017

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