Modeling of Triangular Lattice Space Structures with Curved Battens
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.22628
Reference9 articles.
1. Demonstration of a 10-M Solar Sail System
2. Effects of Initial Waviness on the Strength and Design of Built-up Structures
3. Strength of Initially Wavy Lattice Columns
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1. A deployable mast for solar sails in the range of 100–1000m;Advances in Space Research;2011-12
2. Concept Design of Deployable Isogrid Booms;52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2011-04-04
3. Mechanical Design of a Kilometer-Sized Solar Sail;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12
4. A Deployable Truss Beam for Long or Lightly Loaded Space Applications;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04
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