| contributor author | W. W. Hough | |
| contributor author | B. D. Elrod | |
| date accessioned | 2017-05-09T00:26:41Z | |
| date available | 2017-05-09T00:26:41Z | |
| date copyright | February, 1969 | |
| date issued | 1969 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27532#13_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/137301 | |
| description abstract | The dependence of solar array energy on orbital parameters is given for cases that achieve optimum array pointing, and therefore, maximum performance. Optimum pointing requires continual array articulation and/or active spacecraft attitude control. Performance obtained in local-vertical attitudes with fixed or incrementally articulated arrays is compared with the maximum. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Solar Array Performance as a Function of Orbital Parameters and Spacecraft Attitude | |
| type | Journal Paper | |
| journal volume | 91 | |
| journal issue | 1 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3591492 | |
| journal fristpage | 13 | |
| journal lastpage | 20 | |
| identifier eissn | 1528-8935 | |
| keywords | Solar cell arrays AND Space vehicles | |
| tree | Journal of Manufacturing Science and Engineering:;1969:;volume( 091 ):;issue: 001 | |
| contenttype | Fulltext | |
