2017
DOI: 10.1016/j.actaastro.2016.12.022
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Space experiments on basic technologies for a space elevator using microsatellites

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Cited by 16 publications
(5 citation statements)
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“…which we write in the form ωg(x) = h(x) providing us with a relation for ω as a function of x: ω = h(x)/g(x) 5 . The sought ω is the smallest solution of this equation so that by taking a derivative and setting it equal to zero we obtain an equation for x corresponding to the extremum, h (x)g(x) = h(x)g (x).…”
Section: The Fast and The Slowmentioning
confidence: 99%
See 1 more Smart Citation
“…which we write in the form ωg(x) = h(x) providing us with a relation for ω as a function of x: ω = h(x)/g(x) 5 . The sought ω is the smallest solution of this equation so that by taking a derivative and setting it equal to zero we obtain an equation for x corresponding to the extremum, h (x)g(x) = h(x)g (x).…”
Section: The Fast and The Slowmentioning
confidence: 99%
“…This situation is of interest not only in the general relativistic case as a tool to distinguish various non-local effects but also in Newtonian gravity as this effect can be used to stabilize orientation of artificial satellites and even to alter their orbital parameters. In this respect, apart from the seminal thoughts of Tsiolkovsky from 1895, the first papers on tether-controlled satellites appeared in the 1960s (see [1] for a review of literature) with research continuing until this day [2][3][4] and there have even been in-orbit experiments (for example, the Gemini XI mission in 1966 and, more recently, STARS-C aboard ISS [5]). Likewise, in general relativity this effect can influence the trajectory of an oscillating body, pushing it into a higher or lower orbit, speeding up or slowing down its descent or ascent in a predefined background spacetime but it can also be used as a tool to investigate the properties of a given gravitational field, perhaps distinguishing between various field characteristics in the resonance regime that would remain below detection threshold with a single point particle approach.…”
Section: Introductionmentioning
confidence: 99%
“…Their analysis shows that the classical TPDB model is accurate in describing the overall motions of the PSE and suitable for control law development, provided the control law is robust. Besides the theoretical studies, Yamagiwa et al [14] investigated the PSE from an engineering aspect for space demonstration.…”
Section: Introductionmentioning
confidence: 99%
“…Due to the exceptional creep resistance of polyarylate fibers, braided polyarylate fiber ropes are particularly favored by spacecraft deployable structures with long-term static load, such as thermal knife hold-down and release device, space tether, mesh expandable antenna, and space habitat. [1][2][3][4] However, the tensile properties of braided polyarylate fiber ropes depend on the loading history that leads to the difficulty of predicting the mechanical behavior of the rope and essentially affects the design of the ropes for the spacecraft deployable structures.…”
Section: Introductionmentioning
confidence: 99%