2018 IEEE Aerospace Conference 2018
DOI: 10.1109/aero.2018.8396390
|View full text |Cite
|
Sign up to set email alerts
|

On-orbit validation of the roll-out solar array

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2019
2019
2024
2024

Publication Types

Select...
8

Relationship

0
8

Authors

Journals

citations
Cited by 20 publications
(7 citation statements)
references
References 7 publications
0
4
0
Order By: Relevance
“…[50] The aforementioned features of PSCs make them promising candidates for space PVs for many reasons. In particular, low weight and flexibility are pivotal requirements for space applications, not only to reduce the launching costs of spacecraft but also to allow the fabrication of roll-out solar arrays, [4,51,52] which are currently produced by using rigid, thick, and heavy SCs (such as Si-and InGaP/GaAs/Ge-based devices). To promote the space applications of PSCs, a few groups have already investigated the effects of various extreme space environments on the perovskite films and PSC's performance.…”
Section: Measurement Of Organic Perovskite and Other New Solar Cellsmentioning
confidence: 99%
“…[50] The aforementioned features of PSCs make them promising candidates for space PVs for many reasons. In particular, low weight and flexibility are pivotal requirements for space applications, not only to reduce the launching costs of spacecraft but also to allow the fabrication of roll-out solar arrays, [4,51,52] which are currently produced by using rigid, thick, and heavy SCs (such as Si-and InGaP/GaAs/Ge-based devices). To promote the space applications of PSCs, a few groups have already investigated the effects of various extreme space environments on the perovskite films and PSC's performance.…”
Section: Measurement Of Organic Perovskite and Other New Solar Cellsmentioning
confidence: 99%
“…Compared to STEM, slit-tube actuators are less rigid; they withstand less bending and torsional forces. In [24] the power of the stored strain energy in the composite slit-tube is used to deploy a folded solar array in space.…”
Section: Slit-tubementioning
confidence: 99%
“…Due to this technology, a reduction of 33% in mass and of a factor of 4 in volume is attained with respect to an equivalent rigid panel. 22 Another notable example is constituted by the NASA's Deployable Composite Booms (DCB) project, which aims to develop a 54-foot long thin-shell composite boom to be used for supporting deployable systems, such as solar sails (up to 2000 m 2 ) 23 and arrays, or for instrumentation-hosting purpose. However, in current boom designs, the gain of cross-section inertia after deployment is directly dependent on the width of the boom, with higher cross-section inertia requiring a boom that is larger in the transversal dimension.…”
Section: Introductionmentioning
confidence: 99%