TY - GEN
T1 - Alternative rigidisation method for inflatable structures
AU - Markaide, N.
AU - Marcos, J.
AU - Zubillaga, O.
PY - 2008
Y1 - 2008
N2 - Thermally rigidised thermoset composites and UV rigidised composites are methods that have been widely studied in inflatable structures. However, these methods based on chemical rigidisation present some awbacks, as for example the influence of space environment in polymerisation and thus, in final properties obtained in the composite. Alternative and promising methods are passive cooled thermoplastics. The aim of this project has been to conduct further research in this new rigidisation technology. A study of different materials has been performed based on the final properties required in space conditions, but also properties specifically needed for folding, inflation and rigidisation steps. Thus, the approach has been planned in two phases. The first phase covers a material study and testing at coupon level, which has allowed the optimisation of the rigidisation process. The second phase deals with the manufacturing, testing and validation of a reduced size breadboard, consisting of a solar array composed by two lateral flexible solar panels (membranes) supported by a central rigidisable boom.
AB - Thermally rigidised thermoset composites and UV rigidised composites are methods that have been widely studied in inflatable structures. However, these methods based on chemical rigidisation present some awbacks, as for example the influence of space environment in polymerisation and thus, in final properties obtained in the composite. Alternative and promising methods are passive cooled thermoplastics. The aim of this project has been to conduct further research in this new rigidisation technology. A study of different materials has been performed based on the final properties required in space conditions, but also properties specifically needed for folding, inflation and rigidisation steps. Thus, the approach has been planned in two phases. The first phase covers a material study and testing at coupon level, which has allowed the optimisation of the rigidisation process. The second phase deals with the manufacturing, testing and validation of a reduced size breadboard, consisting of a solar array composed by two lateral flexible solar panels (membranes) supported by a central rigidisable boom.
UR - http://www.scopus.com/inward/record.url?scp=77950503807&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77950503807
SN - 9781615671601
T3 - International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
SP - 5340
EP - 5344
BT - International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
T2 - 59th International Astronautical Congress 2008, IAC 2008
Y2 - 29 September 2008 through 3 October 2008
ER -