Dependence of solar array energy on orbital parameters is given for cases that achieve optimum array pointing and 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 maximum. (30798)
Solar array performance as function of orbital parameters and spacecraft attitude
ASME Aviation Space -- Progress Prospects
ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Power supply
1968
9 pages
Aufsatz (Konferenz)
Englisch
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Solar arrayperformance as a function of orbital parameters and spacecraft attitude
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