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MISSION: STS-106 -- 4th ISS Flight (2A.2b) |
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| VEHICLE |
Atlantis/OV-104 |
| LOCATION |
Orbiter Processing Facility (OPF)
bay 3 |
| TARGET KSC
LAUNCH DATE/TIME |
Sept. 8, 2000 at
8:31 a.m. EDT |
| TARGET KSC LANDING DATE/TIME |
Sept. 19, 2000 at 3:12 a.m. |
| LAUNCH WINDOW |
10 minutes |
| MISSION DURATION |
10 days, 18 hours and 41 minutes |
| CREW |
Wilcutt, Altman,
Lu, Malenchenko, Morukov, Mastracchio, Burbank |
| ORBITAL ALTITUDE and INCLINATION |
177 nautical miles/51.6 degrees |
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| Shuttle Processing Note |
This week workers
installed Discovery's window No. 4 and completed installation of the pitch actuator for
the left-hand orbiter maneuvering engine. Today, technicians are testing the orbiter's
ground control interface logic system and an onboard operations recorder. The STS-106
astronauts are at KSC participating in Crew Equipment Interface Test activities through
the weekend.
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MISSION: STS-92 -- 5th ISS Flight (3A) -- Z-1 Truss, PMA-3 |
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| VEHICLE |
Discovery/OV-103 |
| LOCATION |
OPF bay 1 |
| TARGET KSC LAUNCH
DATE/TIME |
Oct. 5, 2000 at about
9:49 p.m. EDT |
| TARGET KSC LANDING DATE/TIME |
Oct. 16, 2000 |
| MISSION DURATION |
11 days |
| CREW |
Duffy, Melroy, Wakata, Chiao, Wisoff, Lopez-Alegria, McArthur |
| ORBITAL ALTITUDE and
INCLINATION |
177 nautical miles/51.6
degrees |
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| Shuttle Processing Note |
Interface verification
testing for the pressurized mating adapter payload is complete. Workers continue routine checks of
Discovery's orbiter maneuvering system pod.
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MISSION: STS-97 -- 6th ISS Flight (4A) -- PV Module P6 |
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| VEHICLE |
Endeavour/OV-105 |
| LOCATION |
OPF bay 2 |
| TARGET KSC LAUNCH
DATE/TIME |
Nov. 30, 2000 at time
10:48 p.m. (under review) |
| TARGET KSC LANDING DATE/TIME |
Dec. 9, 2000 at time TBD |
| MISSION DURATION |
9 days |
| CREW |
Jett, Bloomfield,
Tanner, Noriega, Garneau |
| ORBITAL ALTITUDE and
INCLINATION |
177 nautical miles/51.6
degrees |
|
| Shuttle Processing Note |
This week technicians
installed the antenna for Endeavour's new space-to-space orbiter radio system. Functional tests of
the orbiter docking system (ODS) continue and ODS pyrotechnic system checks are ongoing.
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