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Chandra X-ray Observatory


Organization NASA , SAO , CXC
Wavelength regimeX-ray
Orbit height10 000 km (perigee), 140 161 km (apogee)
Orbit period3858 min, 64.3 h
Launch date 23 July 1999
Deorbit dateN/A
Mass4 800 kg, 10 600 lb
Other namesAdvanced X-ray Astrophysics Facility, AXAF
COSPAR ID 1999-040B
Webpagehttp://chandra.harvard.edu/
Physical characteristics
Telescope style4 nested pairs of grazing incidence paraboloid and hyperboloid mirrors
Diameter1.2 m, 3.9 ft
Collecting area0.04 m&2 at 1 keV, 0.4 ft&2 at 1 keV
Focal length10 m, 33 ft
Instruments
ACIS imaging spectrometer
HRC camera
HETGS high resolution spectrometer
LETGS high resolution spectrometer


The Chandra X-ray Observatory is a Satellite launched on STS-93 by NASA on July 23 , 1999 . It was named in honor of Indian - American Physicist Subrahmanyan Chandrasekhar who is known for determining the Mass Limit for White Dwarf stars to become Neutron Star s. " Chandra " also means "moon" or "luminous" in Sanskrit .

Chandra Observatory is the third of NASA's four Great Observatories . The first was Hubble Space Telescope ; second the Compton Gamma Ray Observatory , launched in 1991 ; and last is the Spitzer Space Telescope . Prior to successful launch, the Chandra Observatory was known as AXAF, the '''Advanced X-ray Astrophysics Facility'''. AXAF was assembled and tested by TRW (now Northrop Grumman Space Technology) in Redondo Beach , California .

Since the Earth's Atmosphere absorbs the vast majority of X-ray s, they are not detectable from Earth-based Telescope s, requiring a space-based telescope to make these observations.


DISCOVERIES

The data gathered by Chandra have greatly advanced the field of X-ray Astronomy .



TECHNICAL DESCRIPTION

(upper right) and its parent galaxy NGC 1260 (lower left) in false color as observed through the Chandra X-Ray Observatory.]]
Unlike Optical telescopes which possess simple aluminized Parabolic surfaces (mirrors), X-ray telescopes generally have nested cylindrical Paraboloid and Hyperboloid surfaces coated with Iridium or Gold . X-ray Photon s would be absorbed by normal mirror surfaces, so mirrors with a low grazing angle are necessary to reflect them. Chandra uses four pairs of nested Iridium mirrors, together with their support structure, called the High Resolution Mirror Assembly (HRMA).

Chandra's high Elliptical orbit allows it to observe continuously for up to 55 hours of its 65 hour Orbital Period .

With an Angular Resolution of 0.5 Arcsecond (2.4 µrad), Chandra possesses a resolution over one thousand times better than that of the first orbiting X-ray telescope.


Instruments

The Science Instrument Module (SIM) holds the two focal plane instruments, the Advanced CCD Imaging Spectrometer (ACIS) and the High Resolution Camera (HRC), moving whichever is called for into position during an observation.

ACIS consists of 10 CCD chips and provides images as well as Spectral information of the object observed. It operates in the range of 0.2 - 10 KeV . HRC has two Micro-channel Plate components and images over the range of 0.1 - 10 keV. It also has a time resolution of 16 Microsecond s. Both of these instruments can be used on their own or in conjunction with one of the observatory's two Transmission Gratings .

The transmission gratings, which swing into the optical path behind the mirrors, provide Chandra with high resolution spectroscopy. The High Energy Transmission Grating Spectrometer (HETGS) works over 0.4 - 10 keV and has a spectral resolution of 60-1000. The Low Energy Transmission Grating Spectrometer (LETGS) has a range of 0.09 - 3 keV and a resolution of 40-2000.

mission STS-93 .]]


HISTORY

In 1976 the Chandra X-ray Observatory (called AXAF at the time) was proposed to NASA by Riccardo Giacconi and Harvey Tananbaum . Preliminary work began the following year at Marshall Space Flight Center (MSFC) and the Smithsonian Astrophysical Observatory (SAO). In the meantime, in 1978 , NASA launched the first imaging X-ray telescope, Einstein (HEAO-2), into orbit. Work continued on the Chandra project through the 1980's and 1990's. In 1992 , to reduce costs, the spacecraft was redesigned. Four of the twelve planned mirrors were eliminated, as were two of the six scientific instruments. Chandra's planned orbit was changed to an elliptical one, reaching one third of the way to the Moon's at its farthest point. This eliminated the possibility of improvement or repair by the Space Shuttle but put the observatory above the Earth's Radiation Belts for most of its orbit.

AXAF was renamed Chandra in 1998 and launched in 1999 by the shuttle Columbia (STS-93). At 22753 kg, it was the heaviest payload ever launched by the shuttle, a consequence of the two-stage Inertial Upper Stage booster rocket system needed to transport the spacecraft to its high orbit.

Chandra has been returning data since the month after it launched. It is operated by the SAO at the Chandra X-ray Center in Cambridge, Massachusetts , with assistance from MIT and Northrop Grumman Space Technology. The ACIS CCDs suffered particle damage during early radiation belt passages. To prevent further damage, the instrument is now removed from the telescope's focal plane during passages.

In 2004 Chandra celebrated its fifth year of operation.


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