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- Lightweight, low-volume flexible blanket array
- Developed in support of New Millennium Program ST4 comet rendezvous mission
- Inflatable Solar Array Experiment (ISAE) planned for technology demonstration on Shuttle
- ILC Dover / AEC-ABLE / L’Garde / JPL / USAF Team
- 5 kW flexible blanket array
- Inflatable, rigidizable beam provides structure
- Rigidization method is heated thermoset epoxy
- Controlled deployment (wire brake roll-up)
- Array size : 15m x 3m, split blanket configuration
- 102W/Kg with 15% mass margin
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| For more information on Engineered Inflatables, please contact Gil Baird. |
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