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Influence of interorbit acceleration on the design of large space antennas
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hedgepeth, J. M. |
| Copyright Year | 1980 |
| Description | The characteristics of the acceleration-induced loading in structures consisting of triangular lattices are investigated and some initial quantitative results on the effect on the design mass and stowage volume are presented. The approach used defines the structural design that would be used if no interorbit acceleration were required and then determines what strengthening would be required to accommodate the loads due to acceleration. The basic zero acceleration design can be based on the stringent accuracy requirements placed on the antennas. |
| File Size | 966934 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800022955 |
| Archival Resource Key | ark:/13960/t79s6k56w |
| Language | English |
| Publisher Date | 1980-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Bending Moments Space Erectable Structures Antenna Design Aerospace Environments Acceleration Physics Structural Design Criteria Struts Radiation Shielding Thrust Loads Load Distribution Forces Trusses Large Space Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
