  This paper reports a design study for a space-based decametric wavelength
telescope. While not a new concept, this design study focused on many of the
operational aspects that would be required for an actual mission. This design
optimized the number of spacecraft to insure good visibility of approx. 80% of
the radio galaxies -- the primary science target for the mission. A 5,000 km
lunar orbit was selected to guarantee minimal gravitational perturbations from
Earth and lower radio interference. Optimal schemes for data downlink,
spacecraft ranging, and power consumption were identified. An optimal mission
duration of 1 year was chosen based on science goals, payload complexity, and
other factors. Finally, preliminary simulations showing image reconstruction
were conducted to confirm viability of the mission. This work is intended to
show the viability and science benefits of conducting multi-spacecraft
networked radio astronomy missions in the next few years.
