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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
 
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

SRB Set:  BI-097

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

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


Payloads

Cargo Bay
Chandra X-Ray Observatory

In-Cabin
Plant Growth Investigations in Microgravity 1
Southwest Ultraviolet Imaging System
Gelation of Sols: Applied Microgravity Research
Space Tissue Loss
Lightweight Flexible Solar Array Hinge
Cell Culture Model, Configuration C
Shuttle Amateur Radio Experiment II
Commercial Generic Bioprocessing Apparatus
Micro-Electromechanical Systems
Biological Research in Canisters


Mission Overview |  Flight Plan |  Payloads |  DTO/DSO/RME
Media Contacts
Crew Members |  Shuttle Reference Data |  Related Links |  Media Assistance

Updated: 07/13/1999

Boeing NASA United Space Alliance

Editorial/Technical Comments: ShuttlePresskit