Structural design of flexible solar generators

European Space Agency, (Special Publication) ESA SP

Volumn , Issue 589, 2005, Pages 233-238

  Seifart, Klaus ^a   Schmidt, Tilo ^a   Göhler, Wolfgang ^a   Langlois, Stéphane ^b  

^a Hoch Technologie Systeme GmbH   (Germany)

^b EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

COST EFFECTIVENESS; ELECTRIC BATTERIES; FREQUENCIES; GLASS FIBERS; SPACECRAFT; STRUCTURAL DESIGN; VIBRATION MEASUREMENT;

FRAME STRUCTURES; POWER RANGES; SOLAR ARRAYS (S/A); SOLAR GENERATORS;

SOLAR POWER GENERATION;

EID: 23844480178     PISSN: 03796566     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Unda J., Weisz J., Rivacoba J., Ruiz Uríen I., Capitanio R.S., Family of Deployable / Retractable Structures for Space Application, 43rd Congress of International Astronautical Federation, Washington, DC, 1992.
2. Thomson M.W., Deployable and retractable telescoping tubular structure development, AIAA No. 93-0976, Aerospace Design Conference, Irvine, CA, 1993.
3. Conley P.L., Space Vehicle Mechanisms, John Wiley & Sons, New York, 1998.
4. Schmidt T., Seifart K., Burger F., Eder J., In Orbit Bonding (IOB) of Long Deployable Structures, European Space_Mechanism and Tribology Symposium, San Sebastian, 2003.