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Use of CYPRES™ cutters with a Kevlar clamp band for hold-down and release of the Icarus De-Orbit Sail payload on TechDemoSat-1 (2014)

First Author: Kingston J

Attributed to: Astronomy and Planetary Sciences at the Open University (APSOU) funded by STFC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.actaastro.2014.03.014

Publication URI: http://dx.doi.org/10.1016/j.actaastro.2014.03.014

Type: Journal Article/Review

Parent Publication: Acta Astronautica