Rapid structural assessment approach for square solar sails including edge support cords

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Mikulas, Martin M ^a   Adler, Aaron L ^b  

^a UNIVERSITY OF COLORADO   (United States)

^b SAT Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

SOLAR EQUIPMENT; SOLAR RADIATION; STRUCTURAL DYNAMICS;

CURVED BOUNDARY; DESIGN DRIVERS; EDGE SUPPORTS; GEOMETRIC NON-LINEARITY; PRELIMINARY DESIGN; SIMPLIFYING ASSUMPTIONS; STRUCTURAL ASSESSMENTS;

SOLAR SAILS;

EID: 85088721681     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1447     Document Type: Conference Paper

References (9)

1. Wright, Jerome, "Space Sailing, " Gordon and Breach Publishers, 1992.
2. Stein, Manuel, Hedgepeth, John, "Analysis of Partly Wrinkled Membranes, " NASA TN D-813, 1961.
3. Adler, Aaron, Mikulas, Martin, and Hedgepeth, John, "Static and Dynamic Analysis of Partly Wrinkled Membrane Structures, " AIAA 2000-1810, AIAA SDM Conference April 2000.
4. Adler, Aaron L.; Finite Element Approaches for Static and Dynamic Analysis of Partially Wrinkled Membrane Structures. PhD thesis, Aerospace Engineering Department, University of Colorado, 2000.
5. nd AIAA Structures, Structural Dynamics, and Materials Conference, April 16-19, Seattle, 2001, WA.
6. Adler, Aaron, and Mikulas, Martin, "Application of a Membrane Finite Element Approach to Advanced Membrane Structures, " AIAA Paper # 2001-5990, Albuquerque, August 2001.
7. rd AIAA Structures, Dynamics and Materials Conference, April, 2002, AIAA 2002-1560.
8. Mikulas, Martin M. "Structural Efficiency of Long Lightly Loaded Truss and Isogrid Columns for Space Applications, " NASA Technical Memorandum 78687, Langley Research Center, July 1978.
9. Lienard, Sebastien, "Characterization of Large Thin Film Membrane Dynamic Behavior With UAI-NASTRAN Finite Element Solver, " SAE, 1999-01-5518.