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Dive into the research topics where Martin E. Zander is active.

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Featured researches published by Martin E. Zander.


2nd AIAA Spacecraft Structures Conference | 2015

Deployment Testing of the De-Orbit Sail Flight Hardware

Martin Hillebrandt; Sebastian Meyer; Martin E. Zander; Christian Hühne

The paper describes the results of the deployment testing of the De-Orbit Sail flight hardware, a drag sail for de-orbiting applications, performed by DLR. It addresses in particular the deployment tests of the fullscale sail subsystem and deployment force tests performed on the boom deployment module. For the fullscale sail testing a gravity compensation device is used which is described in detail. It allows observations of the in-plane interaction of the booms with the sail membrane and the central satellite body to which the booms and sails are attached. During the tests issues with the sail deployment tests were encountered which lead to design changes regarding the sail and type of sail attachment.


Advances in Space Research | 2017

Gossamer-1: Mission concept and technology for a controlled deployment of gossamer spacecraft

Patric Seefeldt; Peter Spietz; Tom Sproewitz; Jan Thimo Grundmann; Martin Hillebrandt; Catherin Hobbie; Michael Ruffer; Marco Straubel; Norbert Toth; Martin E. Zander


Archive | 2014

The Boom Design of the De-Orbit Sail Satellite

Martin Hillebrandt; Sebastian Meyer; Martin E. Zander; Marco Straubel; Christian Hühne


Archive | 2016

Advanced Deployable Structural Systems for Small Satellites

W. Keith Belvin; Marco Straubel; W. Keats Wilkie; Martin E. Zander; Juan M. Fernandez; Martin Hillebrandt


Archive | 2015

MECHANICAL CHARACTERIZATION OF DEPLOYABLE THIN SHELL CFRP BOOMS FOR THE CUBESAT “DE-ORBIT SAIL”

Martin E. Zander; Martin Hillebrandt; Michael Sinapius; Christian Hühne


Archive | 2017

ADEO PASSIVE DE-ORBIT SUBSYSTEM ACTIVITY LEADING TO A DRAGSAIL DEMONSTRATOR: CONCLUSION AND NEXT STEPS

Thomas Sinn; Lars Tiedemann; Arne Riemer; Robert Hahn; Tom Spröwitz; Patric Seefeldt; Maciej Sznajder; Siebo Reershemius; Sebastian Meyer; Martin E. Zander; Karl Dietrich Bunte; S. Weikert; A. Wiegand; Tiziana Cardone; Daniele Teti; Robert Knockert


Archive | 2017

Design of the Gossamer-1 Deployment Demonstrator

Tom Spröwitz; Patric Seefeldt; Jan Thimo Grundmann; Peter Spietz; Norbert Toth; Martin Hillebrandt; Marco Straubel; Martin E. Zander


Archive | 2017

Design, Test and Comparison of mechanical support principles to increase the robustness of deployable thin shell CFRP Booms of the deorbiting device ADEO

Martin E. Zander; Gerrit Kottke; Sebastian Meyer; Christian Hühne; Michael Sinapius


7th European Conference on Space Debris | 2017

RESULTS OF THE DEPLOYABLE MEMBRANE & ADEO PASSIVE DE-ORBIT SUBSYSTEM ACTIVITIES LEADING TO A DRAGSAILDEMONSTRATOR

Thomas Sinn; Lars Tiedemann; Arne Riemer; Robert Hahn; Tom Spröwitz; Patric Seefeldt; Maciej Sznajder; Siebo Reershemius; Sebastian Meyer; Martin E. Zander; Karl Dietrich Bunte; Tiziana Cardone; Daniele Teti; Robert Knockert


Archive | 2016

Preliminary creep test for estimating the long term stowage behavior of DLR's CFRP booms

Sebastian Meyer; Martin E. Zander; Christian Hühne

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Norbert Toth

German Aerospace Center

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Maciej Sznajder

University of Zielona Góra

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Peter Spietz

German Aerospace Center

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