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)
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