Gaia was launched by
Arianespace, using a
Soyuz ST-B rocket with a
Fregat-MT upper stage, from the
Ensemble de Lancement Soyouz at
Kourou in
French Guiana on 19 December 2013 at 09:12 UTC (06:12 local time). The satellite separated from the rocket's upper stage 43 minutes after launch at 09:54 UTC. The craft headed towards the Sun–Earth
Lagrange point L2 located approximately 1.5 million kilometres from Earth, arriving there 8 January 2014. The L2 point provided the spacecraft with a very stable gravitational and thermal environment. There, it used a
Lissajous orbit that avoided blockage of the Sun by the Earth, which would have limited the amount of solar energy the satellite could produce through its
solar panels, as well as disturbing the spacecraft's thermal equilibrium. After launch, a 10-metre-diameter sunshade was deployed. The sunshade always maintained a fixed 45 degree angle to the Sun, while precessing to scan the sky, thus keeping all telescope components cool and powering
Gaia using solar panels on its surface. These factors and the materials used in its creation allowed
Gaia to function in conditions between -170
°C and 70
°C.
Scientific instruments The
Gaia payload consists of three main instruments: • The astrometry instrument
(Astro) precisely determines the positions of all stars brighter than magnitude 20 by measuring their angular position. Multi-colour photometry is provided by two low-resolution fused-silica
prisms dispersing all the light entering the field of view in the along-scan direction prior to detection. The Blue Photometer (BP) operates in the wavelength range 330–680 nm; the Red Photometer (RP) covers the wavelength range 640–1050 nm. • The Radial-Velocity Spectrometer
(RVS) is used to determine the velocity of celestial objects along the line of sight by acquiring high-resolution spectra in the spectral band 847–874 nm (field lines of calcium ion) for objects up to magnitude 17. Radial velocities are measured with a precision between 1 km/s (V=11.5) and 30 km/s (V=17.5). The measurements of radial velocities are important "to correct for perspective acceleration which is induced by the motion along the line of sight". Therefore, only a few dozen pixels around each object could be downlinked.
Measurement principles Similar to its predecessor
Hipparcos, but with a precision one hundred times greater,
Gaia consisted of two telescopes providing two observing directions with a fixed, wide angle of 106.5° between them. The spacecraft rotated continuously around an axis perpendicular to the two telescopes' lines of sight, with a spin period of 6 hours. Thus, every 6 hours the spacecraft scanned a great circle strip approximately 0.7 degrees wide. The spin axis in turn had a slower
precession across the sky: it maintained a fixed 45 degree angle to the Sun, but followed a cone around the Sun every 63 days, giving a
cycloid-like path relative to the stars. Over the course of the mission, each observed star was scanned many times from various scan directions, providing interlocking measurements over the full sky. The two key telescope properties were: • 1.45 × 0.5 m
primary mirror for each telescope • 1.0 × 0.5 m
focal plane array on which light from both telescopes was projected. This in turn consisted of 106
CCDs of 4500 × 1966 pixels each, for a total of 937.8 megapixels (commonly depicted as a
gigapixel-class imaging device). These measurements will help determine the astrometric parameters of stars: two corresponding to the angular position of a given star on the sky, two for the derivatives of the star's position over time (motion) and lastly, the star's
parallax from which distance can be calculated. The radial velocity of the brighter stars was measured by an integrated
spectrometer observing the
Doppler effect. Because of the physical constraints imposed by the Soyuz spacecraft,
Gaia focal arrays could not be equipped with optimal radiation shielding, and ESA expected their performance to suffer somewhat toward the end of the initial five-year mission. Ground tests of the CCDs while they were subjected to radiation provided reassurance that the primary mission's objectives could be met. An atomic clock on board
Gaia played a crucial role in achieving the mission's primary objectives.
Gaia rotated with angular velocity of 60"/sec or 0.6 microarcseconds in 10 nanoseconds. Therefore, in order to meet its positioning goals,
Gaia had to be able to record the exact time of observation to within nanoseconds. Furthermore, no systematic positioning errors over the rotational period of 6 hours should be introduced by the clock performance. For the timing error to be below 10 nanoseconds over each rotational period, the frequency stability of the on-board clock needed to be better than 10−12. The rubidium atomic clock aboard the
Gaia spacecraft had a stability reaching ~ 10−13 over each rotational period of 21600 seconds.
Gaia's measurements contribute to the creation and maintenance of a high-precision celestial reference frame, the
Barycentric Celestial Reference System (BCRS), which is essential for both astronomy and navigation. This reference frame serves as a fundamental grid for positioning celestial objects in the sky, aiding astronomers in various research endeavors. All observations, regardless of the actual positioning of the spacecraft, must be expressed in terms of this reference system. As a fully relativistic model, the influence of the gravitational field of the solar-system must be taken into account, including such factors as the gravitational light-bending due to the Sun, the major planets and the Moon. The expected accuracies of the final catalogue data have been calculated following in-orbit testing, taking into account the issues of stray light, degradation of the optics, and the basic angle instability. The best accuracies for parallax, position and proper motion are obtained for the brighter observed stars, apparent magnitudes 3–12. The standard deviation for these stars is expected to be 6.7 micro-arcseconds or better. For fainter stars, error levels increase, reaching 26.6 micro-arcseconds error in the parallax for 15th-magnitude stars, and several hundred micro-arcseconds for 20th-magnitude stars. For comparison, the best parallax error levels from an analysis in 2007 of the Hipparcos data (which observed objects of magnitude 11 or brighter) are no better than 100 micro-arcseconds, with typical levels several times larger. == Launch and orbit ==