Title :
StarLight spacecraft concept descriptions
Author :
Deininger, William D. ; Bladt, J. ; Davis, W. ; Jarski, A. ; O´Quinn, C. ; Porter, B.S. ; Sholes, E.H. ; Brown, G.M. ; Patel, K.C.
Author_Institution :
Ball Aerosp. & Technol. Corp., Boulder, CO, USA
Abstract :
StarLight, conceived as the third NASA New Millennium Program space technology mission (ST3) and now part of the Planet Finder Program within the NASA Origins Theme, is focused on validation of key technologies for future separated spacecraft interferometers, such as Terrestrial Planet Finder (TPF) and the Micro-Arcsecond X-ray Imaging Mission (MAXIM). The main technologies to be demonstrated by StarLight are precision formation flying and separated spacecraft interferometry. This mission uses two spacecraft, launched together into an Earth-trailing heliocentric orbit on a Delta II 7925, to validate these technologies. Launch is planned for June 2006. This paper summarizes the mission concept and describes the two spacecraft in detail with emphasis on the configuration, formation and attitude control subsystem, telecommunications subsystem, electrical power and distribution subsystem and the cold gas propulsion subsystem.
Keywords :
attitude control; electromagnetic wave interferometry; space vehicles; Earth-trailing heliocentric orbit; Micro-Arcsecond X-ray Imaging Mission; NASA New Millennium Program space technology mission; NASA Origins Theme; Planet Finder Program; StarLight spacecraft; Terrestrial Planet Finder; attitude control subsystem; cold gas propulsion subsystem; distribution subsystem; electrical power subsystem; mission concept; precision formation flying; separated spacecraft interferometers; separated spacecraft interferometry; telecommunications subsystem; Interferometers; NASA; Optical control; Optical interferometry; Payloads; Planets; Propulsion; Space technology; Space vehicles; Telescopes;
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
DOI :
10.1109/AERO.2002.1036845