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A deployment mechanism for the double roll-out flexible solar array on the space telescope
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cawsey, T. R. |
| Copyright Year | 1982 |
| Description | A roll-out flexible array which provides more than 4 kW of power for the space telescope was developed. The Array is configured as two wings. The deployment mechanism for each wing is based on flight-proven FRUSA design. Modifications have been incorporated to accommodate an increase in size and mission requirements. The assembly and operation of the deployment mechanism are described together with environmental and functional tests results. |
| File Size | 755728 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820015485 |
| Archival Resource Key | ark:/13960/t14n40z4v |
| Language | English |
| Publisher Date | 1982-05-01 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Flexible Bodies Solar Blankets Positioning Devices Machinery Solar Arrays Engineering Drawings Hubble Space Telescope Deployment Spacecraft Power Supplies Mechanical Devices Satellite Solar Energy Conversion Mechanical Drives Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
