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Starlight

Starlight Combiner & Collector [Ball]

Starlight (formerly ST-3 and DS-3) was to develop and flight validate technologies for precision formation flying and separated spacecraft interferometry that will enable future astrophysics missions.

The separated spacecraft mission is designed to provide a technology demonstration for deep space precision formations and very long baseline optical interferometry. The interferometer would be distributed over two small spacecraft: one spacecraft would serve as a collector, directing starlight toward a second one, called the Combiner, which would collect starlight separately and combine the light to perform the integerometric detection. The interferometer baselines would be variable, allowing spacecraft separations of 40 m to 1 km in a parabolic formation, and providing angular resolutions from 5 to 0.5 nanoradian (1 to 0.1 milliarcsec).

It was originally planned for a launch in 2003 on a Delta-7325-10C rocket. It was reduced to a ground demonstration of interferometry technology.

Nation: USA
Type / Application: Astronomy, interferometer
Operator: NASA
Contractors: Ball Aerospace
Equipment:
Configuration:
Propulsion:
Power: Solar cells, batteries
Lifetime:
Mass:
Orbit: Heliocentric, earth leading orbit
Satellite COSPAR Date LS Launch Vehicle Remarks
Starlight Combiner - cancelled CC SLC-17 Delta-7325-10C with Starlight Collector
Starlight Collector - cancelled CC SLC-17 Delta-7325-10C with Starlight Combiner