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KENNEDY SPACE CENTER SPACE SHUTTLE STATUS REPORT THURSDAY, JAN. 26, 1995 (10:30 AM EST) MISSION: STS-63 -- MIR RENDEZVOUS, SPARTAN and SPACEHAB-3 VEHICLE: Discovery/OV-103 LOCATION: Pad 39B LAUNCH DATE/APPROX. TIME: Feb. 2, 1995 at 12:48 a.m. EST LAUNCH WINDOW: 5 minutes KSC LANDING DATE/TIME: Feb. 10 at 6:13 a.m. MISSION DURATION: 8 days, 5 hours, 25 minutes CREW SIZE: 6 ORBITAL ALTITUDE and INCLINATION: 196-245 statute miles/51.60 degrees IN WORK TODAY: Closeouts of the solid rocket boosters Launch countdown preparations Closing out the orbiter's aft compartment for flight Install and checkout the two contingency space suits in the orbiter's airlock (tonight) WORK COMPLETED: Installed ordnance devices Completed initial stowing of experiments and equipment into the SPACEHAB module KEY OPERATIONAL MILESTONES (dates are targeted only): Hypergolic propellant pressurization (Jan. 27) Purges of the external tank (Jan. 27) Complete orbiter aft engine compartment close-outs (Jan. 29) Countdown begins (4:30 p.m. Jan. 29) Crew arrival for launch (12 midnight Jan. 29) MISSION: STS-67 -- ASTRO-2 VEHICLE: Endeavour/OV-105 LOCATION: OPF bay 1 TARGET LAUNCH DATE/TIME: March 2 at approximately 1:37 a.m. LAUNCH WINDOW: 2 hours, 30 minutes TARGET KSC LANDING DATE/TIME: March 18 at 3:09 p.m. MISSION DURATION: 15 days, 13 hours CREW SIZE: 7 ORBITAL ALTITUDE and INCLINATION: 218 statute miles/28.45 degrees IN WORK TODAY: Checks of the body flap Close-outs of the orbiter's midbody and aft engine compartment Leak tests of the forward reaction control system Closeouts of orbital maneuvering system pods Installing various panels on the vehicle Checks of the flight controls and main propulsion system thrust vector control system Frequency response test of the orbiter's aerosurfaces WORK SCHEDULED: Structural leak tests Positive pressure test MISSION: STS-71 -- 1st MIR DOCKING VEHICLE: Atlantis/OV-104 LOCATION: OPF bay 3 TARGET LAUNCH PERIOD: May/June APPROX. LAUNCH TIME: early morning LAUNCH WINDOW: 5 minutes KSC LANDING DATE/TIME: TBD MISSION DURATION: 9 days, 20 hours CREW SIZE: 7 up, 8 down ORBITAL ALTITUDE and INCLINATION: 196-245 statute miles/51.60 degrees IN WORK TODAY: Systems testing of the power reactant storage and distribution system Servicing the orbiter's potable water system Repositioning of the waste water dump nozzle Tests of the main propulsion system and Ku band antenna Orbital maneuvering system functional tests Configuring the midbody for the orbiter docking system WORK SCHEDULED: Reconfigure payload bay for ODS installation next month