2019
DOI: 10.18178/ijmerr.8.3.424-429
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Using the Technology of Inflatable Structures for the Removal of Spacecraft’s from Low Orbits

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Cited by 11 publications
(1 citation statement)
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“…[1][2][3][4] Tensioned membrane structures found a variety of applications in space missions such as solar cell arrays, solar sails, inflatable booms, reflector antennas, and other auxiliary systems. [5][6][7][8][9] Most of the spacecraft systems are designed with mass and volume constraints; therefore, flexible, elastic, and membrane-based structures are increasing applications in spaceborne systems. [10][11][12] The membrane structures possess small thickness along with negligible bending and compressive strength.…”
Section: Introductionmentioning
confidence: 99%
“…[1][2][3][4] Tensioned membrane structures found a variety of applications in space missions such as solar cell arrays, solar sails, inflatable booms, reflector antennas, and other auxiliary systems. [5][6][7][8][9] Most of the spacecraft systems are designed with mass and volume constraints; therefore, flexible, elastic, and membrane-based structures are increasing applications in spaceborne systems. [10][11][12] The membrane structures possess small thickness along with negligible bending and compressive strength.…”
Section: Introductionmentioning
confidence: 99%