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Abstract

The transportation and deployment subsystem (TDS) has to hold and protect the ballute spacecraft from the point of integration to the ballute spacecraft's point of release. During interplanetary cruise, the ballute has to be kept well tempered and prevented from cold welding of packed envelope layers. Upon deployment, the system has to ensure that the ballute spacecraft properly unfolds in space and is held in position until fully inflated. Eventually, the system has to safely release the ballute spacecraft.

Keywords

Parabolic Flight Base Package Cold Welding Coil Spring Deployment System 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Vieweg+Teubner Verlag | Springer Fachmedien Wiesbaden GmbH 2011

Authors and Affiliations

  • Hannes Griebel

There are no affiliations available

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