THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER[J]. MECHANICS IN ENGINEERING, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

Citation:

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER[J]. MECHANICS IN ENGINEERING, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

Citation:

THE DEPLOYMENT OF TETHERED SUBSATELLITE WITH HOHMANN TRANSFER[J]. MECHANICS IN ENGINEERING, 1998, 20(6): 27-28. DOI: 10.6052/1000-0992-1999-361

Abstract

The new strategy for the deployment of tethered satellite is presented, which is similar to the idea of Hohmann transfer. The dynamics is studied, and the transfer condition is derived from the orbital equations and Kepler′s equation. At last, a numerical example is given .

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