Talk:SpaceElevatorDeployment: Difference between revisions

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(New page: The deployment spacecraft should be largely built with conventional satellite technology. Work needed on the cimber: {| border="1" cellpadding="2" |- |width="200pt"| Item |width="400pt"...)
 
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|Ribbon deployment || dynamics, speed, matching tension in multiple ribons, attaching ribbons end-to-end.  
|Ribbon deployment || dynamics, speed, matching tension in multiple ribons, attaching ribbons end-to-end.  
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|Overall structure design || Minimize mass, design to handle oscillations, operation in unidirectional gravity field (0 - 0.1G)
|Overall structure design || Minimize mass, design to handle oscillations, operation in unidirectional gravity field (0 - 0.1G)  
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|Retrieving the end of the ribbon at Earth || General scenario, issues, end unit design, performance requirements
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|Operations || Work out a detailed operational scenario including fault handling, despooling and speed control   
|Operations || Work out a detailed operational scenario including fault handling, despooling and speed control   

Revision as of 23:04, 29 June 2008

The deployment spacecraft should be largely built with conventional satellite technology.

Work needed on the cimber:

Item Notes
Overall system engineering Overall satellite constraints and components need to be defined along with the trade-offs for overall performance and subcomponents
Categorize available electromagnetic propulsion systems of the size required Define, performance, mass, maturity, cost,
Examine large scale ribbon spooling techniques
Ribbon deployment dynamics, speed, matching tension in multiple ribons, attaching ribbons end-to-end.
Overall structure design Minimize mass, design to handle oscillations, operation in unidirectional gravity field (0 - 0.1G)
Retrieving the end of the ribbon at Earth General scenario, issues, end unit design, performance requirements
Operations Work out a detailed operational scenario including fault handling, despooling and speed control

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