Quick Facts:The Chandra X-ray Observatory
NASA's newest space telescope, the Chandra X-ray Observatory, will allow scientists from around the world to obtain unprecedented X-ray images and spectra of violent, high-temperature events and objects to help us better understand the structure and evolution of our universe.
It will also serve as a unique tool to study detailed physics in a unique laboratory -- the universe itself , one that cannot be replicated here on Earth.
Managed by NASA's Marshall Space Flight Center in Huntsville, Ala., Chandra is a sophisticated, state-of-the-art instrument that represents a tremendous technological advance in X-ray astronomy.
Did you know?-
The Chandra X-ray Observatory is the world's most powerful X-ray telescope. It has eight-times greater resolution and will be able to detect sources more than 20-times fainter than any previous X-ray telescope.
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The Chandra X-ray Observatory, with its Inertial Upper Stage and support equipment, is the largest and heaviest payload ever launched by the Space Shuttle.
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The Chandra X-ray Observatory's operating orbit takes it 200-times higher than the Hubble Space Telescope. During each orbit of the Earth, Chandra travels one-third of the way to the Moon.
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The Chandra X-ray Observatory's resolving power is , 0.5 arc-seconds -- equal to the ability to read the letters of a stop sign at a distance of 12 miles. Put another way, Chandra's resolving power is equivalent to the ability to read a 1-centimeter newspaper headline at the distance of a half-mile.
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If the State of Colorado were as smooth as the surface of the Chandra X-ray Observatory mirrors, Pike's Peak would be less than an inch tall.
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Another of NASA's incredible time machines, the Chandra X-ray Observatory will be able to study some quasars as they were 10 billion years ago.
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The Chandra X-ray Observatory will observe X-rays from clouds of gas so vast that it takes light more than five-million years to go from one side to the other.
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Although nothing can escape the incredible gravity of a black hole, not even light, the Chandra X-ray Observatory will be able to study particles up to the last millisecond before they are sucked inside.
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It took almost four centuries to advance from Galileo's first telescope to NASA's Hubble Space Telescope — an increase in observing power of about a half-billion times. NASA's Chandra X-ray Observatory is about one-billion times more powerful than the first X-ray telescope, and we have made that leap in slightly more than three decades.
Chandra Mission at a Glance:
Chandra X-ray Observatory Mission Duration
Chandra science mission |
Approx. 5 yrs
|
Orbital Activation & Checkout period |
Approx. 2 mos
|
Orbital Data
Inclination |
28.5 degrees
|
Altitude at apogee |
86,487 sm
|
Altitude at perigee |
5,999 sm
|
Orbital period |
64 hrs
|
Observing time per orbital period |
Up to 55 hrs
|
Dimensions
Length , (Sun shade open) |
45.3'
|
Length , (Sun shade closed |
38.7'
|
Width , (Solar arrays deployed) |
64.0'
|
Width , (Solar arrays stowed) |
14.0'
|
Weights
Dry |
10,560 lbs
|
Propellant |
2,153 lbs
|
Pressurant |
10 lbs
|
Total at launch |
12,930 lbs
|
Integral Propulsion System
Liquid Apogee Engines |
4 engines
(Only 2 used at a time)
|
Fuel |
Hydrazine
|
Oxidizer |
Nitrogen tetroxide
|
Thrust per engine |
105 lbs
|
Electrical Power
Solar Arrays |
2 arrays
3 panels each
|
Power generated |
2,350 watts
|
Electrical power storage |
3 batteries
40-amp-hour
nickel hydrogen
|
Communications
Antennas |
2 low-gain antennas
|
Communication links |
Shuttle Payload Interrogator
Deep Space Network
|
Command link |
2 kbs per second
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Data downlink |
32 kbs to 1024 kbs
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On-board Data Capture
Method |
Solid-state recorder
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Capacity |
1.8 gbs
16.8 hrs
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High Resolution Mirror Assembly
Configuration |
4 sets of nested,
grazing incidence
paraboloid/hyperboloid
mirror pairs
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Mirror Weight |
2,093 lbs
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Focal length |
33 ft
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Outer diameter |
4 ft
|
Length |
33.5 in
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Material |
Zerodur
|
Coating |
600 angstroms of iridium
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Attitude Control & Pointing
Reaction wheels |
6
|
Inertial reference units |
2
|
Aspect camera |
1.40 deg x 1.40 deg fov
|
Science Instruments
Charged Coupled Imaging Spectrometer (ACIS) |
High Resolution Camera (HRC) |
High Energy Transmission Grating (HETG) |
Low Energy Transmission Grating (LETG) |
The Inertial Upper Stage
Dimensions
Length |
17.0'
|
Diameter |
9.25'
|
Weights
Stage 1 , Dry |
2,566 lbs
|
Stage 1 , Propellant |
19,621 lbs
|
Stage 1 - Total |
22,187 lbs
|
Stage 2 , Dry |
2,379 lbs
|
Stage 2 , Propellant |
6,016 lbs
|
Stage 2 - Total |
8,395 lbs
|
Total Inertial Upper Stage , At launch |
30,582 lbs
|
Performance
Thrust , Stage 1 |
46,198 lbs, average
|
Burn Duration , Stage 1 |
125 seconds
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Thrust , Stage 2 |
16,350 lbs, average
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Burn Duration , Stage 2 |
117 seconds
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Support Equipment
Weights
Airborne Support Equipment |
5,365 lbs
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Other |
1,285 lbs
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Total Support Equipment |
6,650 lbs
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Total Payload
Total Chandra/IUS/Support equipment at liftoff |
50,162 lbs
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Length
Total IUS/Chandra |
57.0'
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FS-1999-09-111-MSFC
August 1999
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