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Mission Overview |
Flight Plan |
Payloads |
DTO/DSO/RME
Media Contacts Crew Members | Shuttle Reference Data | Related Links | Media Assistance Download the STS-93 Press Kit in PDF format for printing ( 2.7 MB). Requires Adobe Reader 3.0 |
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Columbia OV102 Launch: Tuesday, July 20, 1999 12:36 AM (eastern time) |
| Mission Objectives |
| The primary objective of the STS-93 mission is the deployment of the $1.5 billion Chandra X-Ray Observatory, the third in NASA's series of "Great Observatories". Astronaut Cady Coleman is scheduled to deploy the observatory about seven hours after liftoff. Chandra will spend the next five years in a highly elliptical orbit which will take it one-third of the way to the moon to study invisible and often violent sources of astronomical activity in the distant universe. Secondary objectives include the firing of Columbia's jet thrusters at various times during the flight to help an Air Force satellite gather data on the characteristics of jet plumes in orbit. In addition, crew members will operate the Southwest Ultraviolet Imaging System, a small telescope which will be mounted at the side hatch window in Columbia's middeck to collect data on ultraviolet light originating from a variety of planetary bodies. Pilot Jeff Ashby and Mission Specialists Steve Hawley and Michel Tognini will conduct an in-flight assessment of an exercise system planned for the International Space Station. The on-orbit treadmill, referred to as the Treadmill Vibration Isolation and Stabilization (TVIS) system, should provide the crew with a reliable exercise device while also meeting International Space Station (ISS) load transmission requirements to avoid disrupting on-orbit experiments. |
| Crew |
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| Commander: | Eileen M. Collins |
| Pilot: | Jeffrey S. Ashby |
| Mission Specialist 1: | Cady G. Coleman |
| Mission Specialist 2: | Steven A. Hawley |
| Mission Specialist 3: | Michel Tognini |
| Launch | |
| Orbiter: | Columbia OV102 |
| Launch Site: | KSC Pad 39-B |
| Launch Window: | 46 minutes |
| Altitude: | 153 nautical miles |
| Inclination: | 28.45 degrees |
| Duration: | 4 Days 22 Hrs. 56 Min. |
| Vehicle Data | |
| Shuttle Liftoff Weight: | 4,524,727 lbs. |
| Orbiter/Payload Liftoff Weight: | 270,142 lbs. |
| Orbiter/Payload Landing Weight: |
219,980 lbs. |
| Payload Weights | |
| SWUIS | 60 lb. |
| 50,162 lbs. |
| Software Version: | OI-26B |
| Space Shuttle Main Engines: (1 MB pdf) | ||
| SSME 1: #2012 | SSME 2: #2031 | SSME 3: #2019 |
| External Tank: ET-99 |
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SRB Set: BI-097 |
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| Auxiliary Power Units: (900 KB pdf) | ||
| APU-1: SN 401 | APU-2: SN 410 | APU-3: SN 304 |
| Fuel Cells: (1.4 MB pdf) | ||
| FC-1: SN 113 | FC-2: SN 125 | FC-3: SN 115 |
| Shuttle Aborts | |
Abort Landing Sites RTLS: Kennedy Space Center TAL: Banjul (prime); Ben Guerir (alternate) AOA: Edwards Air Force Base, California
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| Shuttle Abort History |
| Landing | |
| Landing Date: | 07/24/99 |
| Landing Time: | 11:32 PM (eastern time) |
| Primary Landing Site: | Kennedy Space Center Shuttle Landing Facility |
Editorial/Technical Comments: ShuttlePresskit