2018 AIAA Spacecraft Structures Conference 2018
DOI: 10.2514/6.2018-2206
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Development of High Specific Power Solar Arrays with Shape Memory Polymer Hinge Lines

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Cited by 6 publications
(9 citation statements)
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“…At present, there are still many researchers focus on developing SMPC hinges and booms, most of which are based on the EMC hinge and boom developed by CTD, but have been refined in material preparation, structural optimization and testing method to meet different engineering requirements [50,158,162]. Some new applications, such as the wrinkled/ slack control component, the release devices, the solar arrays, and the deployable trusses with new configurations, have been developed [28,163,164]. They may not have attracted much attention at the moment, but have promising prospects and can provide inspirations for new application development.…”
Section: Potential Applications Of Smp/smpc In Aerospace Fieldmentioning
confidence: 99%
“…At present, there are still many researchers focus on developing SMPC hinges and booms, most of which are based on the EMC hinge and boom developed by CTD, but have been refined in material preparation, structural optimization and testing method to meet different engineering requirements [50,158,162]. Some new applications, such as the wrinkled/ slack control component, the release devices, the solar arrays, and the deployable trusses with new configurations, have been developed [28,163,164]. They may not have attracted much attention at the moment, but have promising prospects and can provide inspirations for new application development.…”
Section: Potential Applications Of Smp/smpc In Aerospace Fieldmentioning
confidence: 99%
“…In recent years, Chen [107], CTD [108], and Liu [109] have developed new space-deployable structures based on SMPCs.…”
Section: (2) Deployable Structures Of Smpcsmentioning
confidence: 99%
“…In order to meet the high power and large area requirements of the solar array for small spacecraft, such as the micro-/nano-satellites for the future, as shown in Fig. 10, Alexi Rakow et al of CTD designed a composite lightweight array utilizing the shape-memory polymer (CLASP) based on elastic memory composite (EMC) linear hinges [108]. The EMC hinges in the CLASP structure were folded in to a "Z" shape to achieve the smooth, slow, and controllable deployment of the solar array.…”
Section: (2) Deployable Structures Of Smpcsmentioning
confidence: 99%
“…[15]. Also, advances in solar sails and solar panels pose a challenge to design lighter deployable structures with lower stowed volume [16]. The need for efficient usage of volume makes it difficult to employ traditional deployable structures [15].…”
Section: List Of Tablesmentioning
confidence: 99%