(Updated August 99)
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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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 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 |
| Data downlink | 32 kbs to 1024 kbs |
On-board Data Capture
| Method | Solid-state recorder |
| Capacity |
1.8 gbs 16.8 hrs |
High Resolution Mirror Assembly
| Configuration |
4 sets of nested, grazing incidence paraboloid/hyperboloid mirror pairs |
| Mirror Weight | 2,093 lbs |
| Focal length | 33 ft |
| Outer diameter | 4 ft |
| Length | 33.5 in |
| Material | Zerodur |
| Coating | 600 angstroms of iridium |
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 |
| Thrust , Stage 2 | 16,350 lbs, average |
| Burn Duration , Stage 2 | 117 seconds |
Support Equipment
Weights| Airborne Support Equipment | 5,365 lbs |
| Other | 1,285 lbs |
| Total Support Equipment | 6,650 lbs |
Total Payload
Weight|
Total Chandra/IUS/Support equipment at liftoff |
50,162 lbs |
Length
| Total IUS/Chandra | 57.0' |
FS-1999-09-111-MSFC
August 1999
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