<> "The repository administrator has not yet configured an RDF license."^^ .
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"Tape-tether design for de-orbiting from given altitude and inclination"^^ .
"The product of the tether-to-satellite mass ratio and the\r\nprobability of tether cuts by small debris must be small\r\nto make electrodynamic bare tethers a competitive and\r\nuseful de-orbiting technology. In the case of a circular\r\norbit and assuming a model for the debris population, the\r\nproduct can be written as a function that just depends\r\non the initial orbit parameters (altitude and inclination)\r\nand the tether geometry. This formula, which does not\r\ncontain the time explicitly and ignores the details of the\r\ntether dynamics during the de-orbiting, is used to find design rules for the tape dimensions and the orbit parameter\r\nranges where tethers dominate other de-orbiting technologies\r\nlike rockets, electrical propulsion, and sails."^^ .
"2013-04-22" .
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"ESA Communications"^^ .
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"ESA Communications"^^ .
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"Gonzalo"^^ .
"Sánchez Arriaga"^^ .
"Gonzalo Sánchez Arriaga"^^ .
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"S. B."^^ .
"Khan"^^ .
"S. B. Khan"^^ .
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"Antonio"^^ .
"Sánchez-Torres"^^ .
"Antonio Sánchez-Torres"^^ .
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"Juan Ramón"^^ .
"Sanmartín Losada"^^ .
"Juan Ramón Sanmartín Losada"^^ .
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"Mario"^^ .
"Charro"^^ .
"Mario Charro"^^ .
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"6th European Conference on Space Debris"^^ .
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"Darmstadt, Germany"^^ .
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"Tape-tether design for de-orbiting from given altitude and inclination (PDF)"^^ .
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"C36.pdf"^^ .
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"Tape-tether design for de-orbiting from given altitude and inclination (Image (PNG))"^^ .
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"preview.png"^^ .
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"Tape-tether design for de-orbiting from given altitude and inclination (Other)"^^ .
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