The SIM Lite Astrometric Observatory (aka SIM Lite), a micro-arcsecond astrometry space mission, has been developed
in response to NASA's indefinite deferral of the SIM PlanetQuest mission. The SIM Lite mission, while significantly
more affordable than the SIM PlanetQuest mission concept, still addresses the full breadth of SIM science envisioned by two previous National Research Council (NRC) Astrophysics Decadal Surveys at the most stringent "Goal" level of
astrometric measurement performance envisioned in those surveys. Over the past two years, the project has completed
the conceptual design of the SIM Lite mission using only the completed SIM technology; published a 250 page book
describing the science and mission design (available at the SIM website: http://sim.jpl.nasa.gov); been subject to an
independent cost and technical readiness assessment by the Aerospace Corporation; and submitted a number of
information responses to the NRC Astro2010 Decadal Survey. The project also conducted an exoplanet-finding
capability double blind study that clearly demonstrated the ability of the mission to survey 60 to 100 nearby sun-like
dwarf stars for terrestrial, habitable zone planets in complex planetary systems. Additionally, the project has continued
Engineering Risk Reduction activities by building brassboard (form, fit & function to flight) version of key instrument elements and subjecting them to flight qualification environmental and performance testing. This paper summarizes the progress over the last two years and the current state of the SIM Lite project.
The Space Interferometry Mission PlanetQuest Light (or SIM-Lite) is a new concept for a space borne astrometric
instrument, to be located in a solar Earth-trailing orbit. SIM-Lite utilizes technology developed over the past ten years
for the SIM mission. The instrument consists of two Michelson stellar interferometers and a precision telescope. The
first interferometer chops between the target star and a set of Reference stars. The second interferometer monitors the
attitude of the instrument in the direction of the target star. The telescope monitors the attitude of the instrument in the
other two directions.
SIM-Lite will be capable of one micro-arc-second narrow angle astrometry on magnitude 6 or brighter stars, relative to
magnitude 9 Reference stars in a two degree field. During the 5 year mission, SIM-Lite would search 65 nearby stars for
planets of masses down to one Earth mass, in the Habitable Zone, which have orbit periods of less than 3 years. SIMLite
will also perform global astrometry on a variety of astrophysics objects, reaching 4.5 micro-arc-seconds absolute
position and parallax measurements. As a pointed instrument, SIM-Lite will be capable of achieving 8 micro-arc-second
astrometric accuracy on 19th visual magnitude objects and 15 micro-arc-second astrometric accuracy on 20th visual
magnitude objects after 100 hours of integration.
This paper will describe the instrument, how it will do its astrometric measurements and the expected performance
based on the current technology.
SIM, a micro-arcsecond astrometry space mission, has been impacted by significant changes in NASA priorities over the
last two years, resulting in the mission being indefinitely delayed. The project team has responded by investigating
alternative mission concepts based upon completed SIM technology. Several alternative mission concepts have been
identified, ranging from a planets-only concept, to versions of SIM, called SIM-Lite, that still address the full breadth of
science envisioned by two previous National Academy Astrophysics Decadal Surveys but with lower precision and
reduced throughput. These mission concepts are significantly more affordable and may fit into a nearer-term future
scenario than the full SIM PlanetQuest17 would. This paper describes the current state of the project, including its design
and technology, and the alternative mission concepts for the use of these designs and technology.
KEYWORDS: Stars, Planets, Galactic astronomy, Astrophysics, Radio optics, Planetary systems, James Webb Space Telescope, Space operations, Motion measurement, Distance measurement
Optical interferometry will open new vistas for astronomy over the next decade. The Space Interferometry Mission
(SIM-PlanetQuest), operating unfettered by the Earth's atmosphere, will offer unprecedented astrometric precision that
promises the discovery of Earth-analog extra-solar planets as well as a wealth of important astrophysics. Results from
SIM will permit the determination of stellar masses to accuracies of 2% or better for objects ranging from brown dwarfs
through main sequence stars to evolved white dwarfs, neutron stars, and black holes. Studies of star clusters will yield
age determinations and internal dynamics. Microlensing measurements will present the mass spectrum of the Milky
Way internal to the Sun while proper motion surveys will show the Sun's orbital radius and speed. Studies of the
Galaxy's halo component and companion dwarf galaxies permit the determination of the Milky Way's mass distribution,
including its Dark Matter component and the mass distribution and Dark Matter component of the Local Group.
Cosmology benefits from precision (1-2%) determination of distances to Cepheid and RR Lyrae standard candles. The
emission mechanism of supermassive black holes will be investigated. Finally, radio and optical celestial reference frames will be tied together by an improvement of two orders of magnitude.
Optical interferometers present severe technological
challenges. The Jet Propulsion Laboratory, with the support of
Lockheed Martin Advanced Technology Center (LM ATC)
and Northrop Grumman Space Technology (NGST), has
addressed these challenges with a technology development
program that is now complete. The requirements for SIM have
been satisfied, based on outside peer review, using a series of
laboratory tests and appropriate computer simulations: laser
metrology systems perform with 10 picometer precision;
mechanical vibrations have been controlled to nanometers,
demonstrating orders of magnitude disturbance rejection; and
knowledge of component positions throughout the whole test
assembly has been demonstrated to the required picometer
level. Technology transfer to the SIM flight team is now well
along.
SIM is a space astrometric interferometer capable of better than one-microarcsecond ( as) single measurement accuracy,
providing the capability to detect stellar "wobble" resulting from planets in orbit around nearby stars. While a search for
exoplanets can be optimized in a variety of ways, a SIM five-year search optimized to detect Earth analogs (0.3 to 10
Earth masses) in the middle of the habitable zone (HZ) of nearby stars would yield the masses, without M*sin(i)
ambiguity, and three-dimensional orbital parameters for planets around ~70 stars, including those in the HZ and further
away from those same stars. With >200 known planets outside our solar system, astrophysical theorists have built
numerical models of planet formation that match the distribution of Jovian planets discovered to date and those models
predict that the number of terrestrial planets (< 10 M(+) ) would far exceed the number of more massive Jovian planets.
Even so, not every star will have an Earth analog in the middle of its HZ. This paper describes the relationship between
SIM and other planet detection methods, the SIM planet observing program, expected results, and the state of technical
readiness for the SIM mission.
SIM-PlanetQuest is a NASA astrophysics mission that is implementing the National Research Counsel's recommended Astrometric Interferometry Mission (AIM) to develop the first, in-space, optical, long-baseline Michelson Stellar Interferometer for performing micro-arcsecond-level astrometry. This level of astrometric precision will enable characterization of planetary systems around nearby stars and enable a number of key investigations in astrophysics including calibration of the cosmological distance scale, stellar and galactic structure and evolution, and dark matter/energy distribution. This paper provides an update on the SIM-PlanetQuest Mission covering the results of the 2005 mission redesign and the recent completion of the last in a series of technology "gates." The SIM-PlanetQuest mission redesign was directed by NASA to recover eroded mass and power margins and to meet specific implementation cost targets. The resulting mission redesign met all redesign objectives with minimal impact to mission science performance. This paper provides the mission redesign objectives and describes the resulting mission and system design including changes in science capability. SIM-PlanetQuest also completed the last of eight major technology development gates that were established in 2001 by NASA, completing the enabling technology development. The technology development program, the last gate, and its significance to the project's flight verification and validation (V&V) approach are briefly described (covered in more detail in a separate paper at this conference). An update on project programmatic status and plans is also provided.
The Space Interferometry Mission (SIM) will be the first in-space, long-baseline Michelson Stellar Interferometer. SIM will perform precision astrometry at the micro-arcsecond accuracy level, which will be used to characterize planetary systems around stars within about ten parsecs of Earth and address a number of other key astrophysics projects. This paper provides a broad overview of the SIM Mission. Topics covered include: the science objectives, key top level requirements, how the mission will be implemented (technical and programmatic), technology development status, an assessment of where the project is today, and prognosis for the future.
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