A new mission concept is introduced for future astrophysical observatories. This concept is to use a solar orbit that remains bounded to the Earth at a large distance on the order of several million kilometers. These orbits are termed here distant Retrograde Orbits (DRO's). This type of orbit is ideal for a space telescope that needs to be separated from the Earth by a large distance to avoid the near-Earth environmental effects, yet needs to remain bounded within some pre-defined distance for communication purposes. Another application is for a solar storm warning system that can provide warning times greater than those available from a similar system at the interior libration point of the Sun-Earth/Moon system. Several classes of DRO's in the Sun-Earth/Moon system are presented. The associated launch and insertion energies for impulsive and continuous thrust transfers from a low Earth parking orbit are investigated.
Transfer trajectories for distant retrograde orbiters of the Earth
1993-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Transfer Trajectories for Distant Retrograde Orbiters of the Earth (AAS 93-344)
British Library Conference Proceedings | 1993
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Online Contents | 2006
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