Deployable morphing modular solar array
A Deployable Morphing Modular Solar Array (DMMSA) for deploying Deployable Morphing Modular Solar Power Assemblies (DMMSPAs) from a spacecraft is provided. The DMMSA comprises a Root Staging and Deployment Mechanism (RSDM) mounted to a spacecraft. A plurality of petal assemblies are rotatably secure...
Saved in:
Main Authors | , |
---|---|
Format | Patent |
Language | English |
Published |
26.08.2014
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Abstract | A Deployable Morphing Modular Solar Array (DMMSA) for deploying Deployable Morphing Modular Solar Power Assemblies (DMMSPAs) from a spacecraft is provided. The DMMSA comprises a Root Staging and Deployment Mechanism (RSDM) mounted to a spacecraft. A plurality of petal assemblies are rotatably secured to the RSDM with each petal assembly having at least DMMSPA secured thereon and each DMMSPA having a slight V-configuration. A launch restraint assembly stacks and sandwiches the petal assemblies prior to deployment with the launch restraint assembly pre-loading each petal assembly's one or more DMMSPA into a substantially flat configuration. Upon release of the launch restraint assembly, the stacked and sandwiched petal assemblies rotate relative to the spacecraft and each petal assemblies DMMSPA elastically morphs from the substantially flat configuration into the slight V-configuration. |
---|---|
AbstractList | A Deployable Morphing Modular Solar Array (DMMSA) for deploying Deployable Morphing Modular Solar Power Assemblies (DMMSPAs) from a spacecraft is provided. The DMMSA comprises a Root Staging and Deployment Mechanism (RSDM) mounted to a spacecraft. A plurality of petal assemblies are rotatably secured to the RSDM with each petal assembly having at least DMMSPA secured thereon and each DMMSPA having a slight V-configuration. A launch restraint assembly stacks and sandwiches the petal assemblies prior to deployment with the launch restraint assembly pre-loading each petal assembly's one or more DMMSPA into a substantially flat configuration. Upon release of the launch restraint assembly, the stacked and sandwiched petal assemblies rotate relative to the spacecraft and each petal assemblies DMMSPA elastically morphs from the substantially flat configuration into the slight V-configuration. |
Author | HARVEY THOMAS JEFFREY HARVEY TOBY JUSTIN |
Author_xml | – fullname: HARVEY TOBY JUSTIN – fullname: HARVEY THOMAS JEFFREY |
BookMark | eNrjYmDJy89L5WRQd0ktyMmvTEzKSVXIzS8qyMjMSwcyUkpzEosUivNBZGJRUWIlDwNrWmJOcSovlOZmUHBzDXH20E0tyI9PLS5ITE7NSy2JDw22sDA0MbC0dDI0JkIJAFjkKcM |
ContentType | Patent |
DBID | EVB |
DatabaseName | esp@cenet |
DatabaseTitleList | |
Database_xml | – sequence: 1 dbid: EVB name: esp@cenet url: http://worldwide.espacenet.com/singleLineSearch?locale=en_EP sourceTypes: Open Access Repository |
DeliveryMethod | fulltext_linktorsrc |
Discipline | Medicine Chemistry Sciences |
ExternalDocumentID | US8814099B1 |
GroupedDBID | EVB |
ID | FETCH-epo_espacenet_US8814099B13 |
IEDL.DBID | EVB |
IngestDate | Fri Jul 19 10:39:45 EDT 2024 |
IsOpenAccess | true |
IsPeerReviewed | false |
IsScholarly | false |
Language | English |
LinkModel | DirectLink |
MergedId | FETCHMERGED-epo_espacenet_US8814099B13 |
Notes | Application Number: US201113199430 |
OpenAccessLink | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140826&DB=EPODOC&CC=US&NR=8814099B1 |
ParticipantIDs | epo_espacenet_US8814099B1 |
PublicationCentury | 2000 |
PublicationDate | 20140826 |
PublicationDateYYYYMMDD | 2014-08-26 |
PublicationDate_xml | – month: 08 year: 2014 text: 20140826 day: 26 |
PublicationDecade | 2010 |
PublicationYear | 2014 |
RelatedCompanies | HARVEY THOMAS JEFFREY HARVEY TOBY JUSTIN MMA DESIGN, LLC |
RelatedCompanies_xml | – name: HARVEY THOMAS JEFFREY – name: HARVEY TOBY JUSTIN – name: MMA DESIGN, LLC |
Score | 2.9474106 |
Snippet | A Deployable Morphing Modular Solar Array (DMMSA) for deploying Deployable Morphing Modular Solar Power Assemblies (DMMSPAs) from a spacecraft is provided. The... |
SourceID | epo |
SourceType | Open Access Repository |
SubjectTerms | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
Title | Deployable morphing modular solar array |
URI | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140826&DB=EPODOC&locale=&CC=US&NR=8814099B1 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3NS8MwFH-MKepNp-L8ogepp2Kbpq09FKFfDGEfuFV2G8mawA77YK2I_70voZte9BYSeEke_PLyvgEehAgJ47ZrcSm5RUuXWJypQsjCJpIEtgy0K6Y_8HsFfZ160xYsdrkwuk7opy6OiIiaI95r_V5vfoxYqY6trJ74AqfWL_kkSs1GO3ZU-2TfTOMoGw3TYWImSVSMzcFb9KwrO4UxKkoH-IsOFBiy91glpWx-S5T8FA5HSGxVn0FLrDpwnOwar3XgqN_4u3HYQK86h8dUqN68KtPJWK6ROyhzcFCqMFKjUgqqwbZb9nUBRp5Nkp6FO872t5sV4_3Z3Etoo9IvrsDwFLKIdN0yoNQjLBQOC925DIjPaUidLnT_JHP9z9oNnCg2Kaso8W-hXW8_xB2K1Zrfa4Z8AzZjfDo |
link.rule.ids | 230,309,783,888,25576,76876 |
linkProvider | European Patent Office |
linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3NT8IwFH8haMSbokb83MHM0-Jou80dFpNtEFQYRDbDjaysTTjwEZgx_ve-NoBe9Na0yWv7kl9f3zfAnRA-yblNLS4lt1hBicVzVQhZ2EQSz5aedsX0EreTsZeRM6rAdJsLo-uEfuriiIioCeK91O_18seIFevYyvUDn-LU4qmdBrG50Y6bqn2ya8Zh0Br0435kRlGQDc3kLXjUlZ38EBWlPfxhewoMrfdQJaUsf0uU9hHsD5DYvDyGipjXoRZtG6_V4aC38XfjcAO99Qncx0L15lWZTsZsgdxBmYODQoWRGmuloBr5apV_nYLRbqVRx8Idx7vbjbPh7mz0DKqo9ItzMByFLCIpLTzGHJL7opn7dCI94nLms2YDGn-Sufhn7RZqnbTXHXefk9dLOFQsUxZS4l5BtVx9iGsUsSW_0cz5BjRIfy0 |
openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Apatent&rft.title=Deployable+morphing+modular+solar+array&rft.inventor=HARVEY+TOBY+JUSTIN&rft.inventor=HARVEY+THOMAS+JEFFREY&rft.date=2014-08-26&rft.externalDBID=B1&rft.externalDocID=US8814099B1 |