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- W2023551021 abstract "This paper examines the use of an elliptically-orbiting tethered-dumbbell (Space Shuttle-satellite) system for satellite transfer to geosynchronous altitude. The twodimensional rigid body equations of motion are derived using a Lagrangian method. Integration of these equations yields the system states, from tether deployment through payload release. These states are used to predict the A V savings (compared to a Hohmann transfer) when the payload is given a swing zero release, that is, the payload is released on a forward swing when the libration angle is instantaneously zero. By varying the pre-deployment true anomaly, the swing zero is caused to occur nearly simultaneously with periapse passage, resulting in maximum A V savings. The system deployment velocity and tether length were also varied to observe their effect on A V savings." @default.
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- W2023551021 date "1986-08-17" @default.
- W2023551021 modified "2023-09-25" @default.
- W2023551021 title "Advantages of using an elliptically-orbiting tethered-dumbbell system for a satellite transfer to geosynchronous orbit" @default.
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- W2023551021 doi "https://doi.org/10.2514/6.1986-2276" @default.
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