Once in science mission orbits, the four 0.12-km diameter observatories plan to form a tetrahedron with as little as 4-km of separation between spacecraft. The stated operational goal of maneuvering the fleet is no more often than once every two weeks (on average). Derived maneuvering accuracy requirement levied on the ACS
Orbital Maneuvering System Design and Performance for the Magnetosperic Multiscale Formation
AAS/AIAA Astrodynamics Specialist Conference ; 2015 ; Vail, CO, United States
2015-08-13
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Englisch