General information | |
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NSSDC ID | 2009-026B |
Organization | European Space Agency with Thales Alenia Space as Prime Contractorship |
Launch date | 2009-05-14 13:12:02 UTC |
Launched from | Guiana Space Centre French Guiana |
Launch vehicle | Ariane 5 ECA |
Mission length | elapsed: 1 year and 9 months |
Location | 1.5 million km (L2 Lagrangian point) |
Wavelength | 350 to 10,000 µm |
Instruments | |
Low Frequency Instrument (LFI) | 30–70 GHz receivers |
High Frequency Instrument (HFI) | 100–857 GHz receivers |
Website | Planck Science Team Home |
Planck is a space observatory designed to observe the anisotropies of the cosmic microwave background (CMB) over the entire sky, using high sensitivity and angular resolution. Planck was built in the Cannes Mandelieu Space Center by Thales Alenia Space and created as the third Medium-Sized Mission (M3) of the European Space Agency's Horizon 2000 Scientific Programme. The project—initially called COBRAS/SAMBA after its approval—is named in honour of the German scientist Max Planck (1858–1947), who won the Nobel Prize for Physics in 1918.
Planck was launched into orbit in 2009, succcessfully reaching the Earth/Sun's L2 Lagrangian point in July, and had successfully completed a second all-sky survey by February, 2010. Prelimiary data from these has been released. Planck is expected to yield definitive data on a number of astronomical issues in 2012. The mission will complement and improve upon observations made by the NASA Wilkinson Microwave Anisotropy Probe, which has measured the anisotropies at larger angular scales and lower sensitivity than Planck. Planck will provide a major source of information relevant to several cosmological and astrophysical issues, such as testing theories of the early universe and the origin of cosmic structure.
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The mission has a wide variety of scientific aims, including:[1]
Planck represents an advance over WMAP in several respects.
It is expected that most Planck measurements will be limited by how well foregrounds can be subtracted, rather than by the detector performance or length of the mission. This is particularly important for the polarization measurements. The dominant foreground depends on frequency, but examples include synchrotron radiation from the Milky Way at low frequencies, and dust at high frequencies.
The spacecraft carries two instruments; the Low Frequency Instrument (LFI) and the High Frequency Instrument (HFI).[1] Both instruments can detect both the total intensity and polarization of photons, and together cover a frequency range of 30 to 857 GHz. The cosmic microwave background spectrum peaks at a frequency of 160.2 GHz
Frequency (GHz) |
Bandwidth () |
Resolution (arcmin) |
Sensitivity (total intensity) , 14 month observation (10−6) |
Sensitivity (polarization) , 14 month observation (10−6) |
---|---|---|---|---|
30 | 0.2 | 33 | 2.0 | 2.8 |
44 | 0.2 | 24 | 2.7 | 3.9 |
70 | 0.2 | 14 | 4.7 | 6.7 |
The LFI has three frequency bands, covering the range of 30–70 GHz. The detectors use High Electron Mobility Transistors.[1]
Frequency (GHz) |
Bandwidth () |
Resolution (arcmin) |
Sensitivity (total intensity) , 14 month observation (10−6) |
Sensitivity (polarization) , 14 month observation (10−6) |
---|---|---|---|---|
100 | 0.33 | 10 | 2.5 | 4.0 |
143 | 0.33 | 7.1 | 2.2 | 4.2 |
217 | 0.33 | 5.5 | 4.8 | 9.8 |
353 | 0.33 | 5.0 | 14.7 | 29.8 |
545 | 0.33 | 5.0 | 147 | N/A |
857 | 0.33 | 5.0 | 6700 | N/A |
The HFI has six frequency bands, between 100 and 857 GHz. They use bolometers to detect photons. The four lower frequency bands have sensitivity to linear polarization; the two higher bands do not.[1]
NASA played a role in the development of the mission and will contribute to the analysis of science data. Its Jet Propulsion Laboratory built components of the science instruments, including bolometers for the high-frequency instrument, a 20 Kelvin cryocooler for both the low- and high-frequency instruments, and amplifier technology for the low-frequency instrument.[2]
A common service module (SVM) was designed and built by Thales Alenia Space in its Turin plant, for both the Herschel Space Observatory and Planck missions, combined into one single program[1] .
Structurally the Herschel and Planck SVM's are very similar. Both SVM's are of octagonal shape and for both, each panel is dedicated to accommodate a designated set of warm units, while taking into account the dissipation requirements of the different warm units, of the instruments as well as the spacecraft.
Furthermore, on both spacecraft a common design for the avionics, the attitude control and measurement system (ACMS) and the command and data management system (CDMS), and power subsystem and the tracking, telemetry and command subsystem (TT&C) has been achieved.
All spacecraft units on the SVM are redundant.
On each spacecraft, the power subsystem consists of the solar array, employing triple-junction solar cells, a battery and the power control unit (PCU). It is designed to interface with the 30 sections of each solar array, provide a regulated 28 V bus, distribute this power via protected outputs and to handle the battery charging and discharging.
For Planck, the circular solar array is fixed on the bottom part of the satellite, facing always the sun, as the satellite is spinning around its vertical axis.
This function is performed by the attitude control computer (ACC) which is the platform for the ACMS. It is designed to fulfil the pointing and slewing requirements of the Herschel and Planck payload.
The Planck satellite is spun at one revolution per minute, the absolute pointing error needs to be less than 37 arc min. For Planck being a survey platform, there is also a requirement to be met on pointing reproducibility error to be less than 2.5 arc min over 20 days.
The main sensor of the line of sight in both spacecraft is the star tracker.
The satellite was successfully launched, along with the Herschel Space Observatory, at 13:12:02 on 14 May 2009 aboard an Ariane 5 ECA heavy launch vehicle. The launch placed the craft into a very elliptical orbit (perigee: 270 km, apogee: more than 1,120,000 km), bringing it near the L2 Lagrangian point of the Earth-Sun system, 1.5 million kilometers from the Earth.
The maneuver to inject Planck into its final orbit around L2 was successfully completed on July 3, 2009, when it entered a Lissajous orbit of 400,000 km radius around the L2 Lagrangian point.[3] The temperature of the High Frequency Instrument reached just a tenth of a degree above absolute zero (0.1 K) on July 3, 2009, placing both the Low Frequency and High Frequency Instruments within their cryogenic operational parameters, making Planck fully operational.[4]
Planck started its First All-Sky Survey on 13 August 2009.[5] In September 2009, the European Space Agency announced the preliminary results from the Planck First Light Survey (performed to demonstrate the stability of the instruments and the ability to calibrate them over long periods). The results indicated that the data quality is excellent.[6]
On 15 January 2010 the mission was extended by 12 months, with observation continuing until at least the end of 2011. After the successful conclusion of the First Survey, the spacecraft started its Second All Sky Survey on 14 February 2010, with more than 95% of the sky observed already and 100% sky coverage being expected by mid-June 2010.[7]
Some planned pointing list data from 2009 have been released publicly, along with a video visualization of the surveyed sky. Some preliminary results are scheduled for release in December 2010,[7] and the final results (with all processed data) are expected to be delivered to the worldwide community towards the end of 2012.
On 17 March 2010 the first Planck photos were published, showing dust concentration within 500 light years from the Sun.[8][9]
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