General:
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)
Chandra Mission at a Glance: 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
Chandra Mission at a Glance: Support Equipment
Weights:
Airborne Support Equipment: 5,365 lbs
Other: 1,285 lbs
Total Support Equipment: 6,650 lbs
Chandra Mission at a Glance: Total Payload
Weight:
Total Chandra/IUS/Support equipment at liftoff: 50,162 lbs
Length:
Total IUS/Chandra: 57.0
More Information
Links to the Chandra X-ray Observatory can be found at the following website: