Peering into the hidden hearts of stars
Finding and exploring exoplanets
Reading stellar life stories
AT A GLANCE
Scientific Goals (in astro-jargon)
- Asteroseismology of acoustic and gravity-mode oscillations in Sun-like stars, magnetic
(rapidly oscillating Ap or roAp) stars, cool giants, pre-main-sequence delta Scuti
pulsating stars, massive O and B stars, and other stellar classes, to probe uniquely
their internal structures and evolutionary states
- Analyses of the transits and eclipses of exoplanets around Sun-like stars and red
dwarf stars, to reveal their sizes, atmospheric compositions, magnetic fields and
other properties
- Measurement of the turbulent variations in massive evolved (Wolf-Rayet) stars to
understand how they add gas to the interstellar medium
- Measurements of structure & variability of gas and dust disks around pre-main-sequence
stars
Scientific Goals (in plainer English)
Can we understand our Sun in the context of other stars? By putting a birth date
on the oldest stars in the solar neighbourhood, can we set a limit on the age of
the Universe? How do strong magnetic fields affect the physics of other stars and
our own Sun? What are mysterious planets around other stars really like? How did
the atoms which make up our planet and our very bodies escape from stars in the first
place?
What MOST does?
It performs ultra-high-precision photometry (measurements of the brightness variations
to a level as small as 1 part per million) of stars down to the naked-eye limit of
visibility (visual apparent magnitude 6) for up to two months without major interruptions.
(To put the sensitivity of MOST in perspective, look at a street lamp 1 km away and
then move your eye 0.5 mm closer to it. The street lamp is now about 1 part per million
brighter to your eye.) MOST is also capable to performing extremely precise photometry
of stars as faint as magnitude 16.
The instrument
An optical telescope with a collecting mirror only 15 cm across, feeding a CCD camera
with a Marconi 47-20 frame-transfer device for collecting science measurements and
for tracking guide stars for satellite attitude control. The Instrument contains
a single broadband filter which selects light in the wavelength range 350 - 700 nanometres
(nm).
The camera is equipped with an array of Fabry microlenses which project a large stable
image of the telescope pupil illuminated by target starlight, which is key to the
highest photometric precision of MOST. For low cost and high reliability, the instrument
has no moving parts. The structure automatically maintains the same focus across
a wide range of temperatures, and exposure times are controlled by rapid frame transfer
of the CCDs. The CCDs are cooled by a passive radiator system.
The spacecraft
The Instrument is housed in a suitcase-sized microsatellite (65 x 65 x 30 cm; mass
= 54 kg) powered by solar panels and oriented by a system of miniature reaction wheels
and magneto-torquers. The attitude control system keeps the telescope pointing to
better than 1 arcsecond (less than 1/4000th of a degree) of the desired target position
99% of the time. This is an improvement of three orders of magnitude over previous
microsatellite pointing capability.
Launch and orbit
MOST was carried aloft aboard a Russian three-stage Rockot (a former Soviet ICBM
now being put to peaceful service) on 30 June 2003, from a launch site in northern
Russia (Plesetsk Cosmodrome). MOST was injected into a low-Earth polar orbit (820
km altitude; period ~ 101 minutes) in a Sun-synchronous mode remaining over the terminator
(dividing line between day and night) of the Earth. From that vantage point, it has
a Continuous Viewing Zone (CVZ) spanning declinations from about −19 to +36 degrees,
in which a selected target star will remain observable for up to 60 days without
interruption.
Communications
Three S-band stations with 2.5-metre dishes are located in Toronto, Vancouver, and
Vienna to allow the MOST team to send commands and receive data from the microsatellite.
We are in direct contact with MOST for up to 40 minutes per day per ground station,
during which commands are uploaded at 9,600 kB/s and data downlinked at 38,400 kB/s.