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- W2029242126 abstract "A satellite in orbit can propel itself by retracting and deploying a length of tether, with expenditure of energy but with no use of on-board reaction mass, as shown by Landis and Hrach in a previous paper. The orbit can be raised, lowered, or the orbital position changed, by reaction against the gravitational gradient. Energy is added to or removed from the orbit by pumping the tether length in the same way as pumping a swing. Examples of tether propulsion in orbit without use of reaction mass are discussed, including: (1) using tether extension to reposition a satellite in orbit without fuel expenditure by extending a mass on the end of a tether; (2) using a tether for eccentricity pumping to add energy to the orbit for boosting and orbital transfer; and (3) length modulation of a spinning tether to transfer angular momentum between the orbit and tether spin, thus allowing changes in orbital angular momentum." @default.
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- W2029242126 date "1992-05-01" @default.
- W2029242126 modified "2023-09-23" @default.
- W2029242126 title "Reactionless orbital propulsion using tether deployment" @default.
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- W2029242126 doi "https://doi.org/10.1016/0094-5765(92)90076-u" @default.
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