Title :
High contrast imaging testbed for the Terrestrial Planet Finder coronagraph
Author :
Lowman, Andrew E. ; Trauger, John T. ; Gordon, Brian ; Green, Joseph J. ; Moody, Dwight ; Niessner, Albert F. ; Shi, Fang
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Abstract :
One of the architectures under consideration for Terrestrial Planet Finder (TPF) is a visible coronagraph. To achieve TPF science goals, the coronagraph must have extreme levels of wavefront correction (less than 1 Å rms over controllable spatial frequencies) and stability to get the necessary suppression of diffracted starlight (10-10 contrast). The High Contrast Imaging Testbed is the TPF platform for laboratory validation of key coronagraph technologies, as well as demonstration of a flight-traceable approach to coronagraph implementation. Various wavefront sensing approaches are under investigation on the testbed, with wavefront control provided by a precision high actuator density deformable mirror. Diffracted light control is achieved through a combination of an occulting or apodizing mask and stop; many concepts exist for these components and are explored. Contrast measurements on the testbed establishes the technical feasibility of TPF requirements, while model and error budget validation are demonstrate implementation viability. This paper describes the current testbed design and preliminary experimental results.
Keywords :
actuators; aerospace test facilities; astronomical photometry; astronomical techniques; coronagraphs; extrasolar planets; wavefront sensors; TPF; Terrestrial Planet Finder coronagraph; controllable spatial frequency; diffracted light control; diffracted starlight suppression; error budget validation; high actuator density deformable mirror; high contrast imaging testbed design; visible coronagraph technology; wavefront control; wavefront correction; wavefront sensing; Actuators; Diffraction; Frequency; Laboratories; Lighting control; Mirrors; Optical imaging; Planets; Stability; Testing;
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Print_ISBN :
0-7803-8155-6
DOI :
10.1109/AERO.2004.1368008