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      KENNEDY SPACE CENTER SPACE SHUTTLE STATUS REPORT THURSDAY, JANUARY 12, 1995 (11:55 AM EST) MISSION: STS-63 -- MIR RENDEZVOUS, SPARTAN and SPACEHAB-3 VEHICLE: Discovery/OV-103 LOCATION: Pad 39B TARGET LAUNCH DATE/TIME: Feb. 2, 1995 at 12:49 a.m. EST LAUNCH WINDOW: 5 minutes TARGET KSC LANDING DATE/TIME: Feb. 10 at 7:05 a.m. MISSION DURATION: 8 days, 6 hours, 13 minutes CREW SIZE: 6 ORBITAL ALTITUDE and INCLINATION: 196-245 statute miles/51.60 degrees IN WORK TODAY: Solid rocket booster portion of the flight readiness test Shuttle interface verification test WORK COMPLETED: Securing of auxiliary power unit no. 2 Launch pad validations Power up Shuttle vehicle WORK SCHEDULED: Main engine frequency response test (Friday) Launch readiness review (Friday) KEY OPERATIONAL MILESTONES SCHEDULED FOR JANUARY (dates are targeted only): Remove leaking thruster R3A (Jan. 17) Terminal Countdown Demonstration Test (Jan. 17-19) Flight Readiness Review (Jan. 18) Hot fire auxiliary power unit no. 2 (Jan. 22) Countdown begins (4:30 p.m. Jan. 29) MISSION: STS-67 -- ASTRO-2 VEHICLE: Endeavour/OV-105 LOCATION: OPF bay 1 TARGET LAUNCH DATE: March 2 APPROX. LAUNCH TIME: 1:37 a.m. LAUNCH WINDOW: 2 hours, 30 minutes 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: Aft engine compartment close-outs Preparations to remove and repair a signal conditioner on the right hand orbital maneuvering system pod WORK COMPLETED: Securing of main engine no. 3 following installation Payload end-to-end tests WORK SCHEDULED: Remove and repair right hand orbital maneuvering system pod (Monday) 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: Remove and replace six ball screw housings on the orbiter docking system (ODS) in the Vehicle Assembly Building Main propulsion system verification checks Remove auxiliary power units (2 of 3 units out, last unit removal is in work) WORK COMPLETED: Fuel cell no. 2 functional checks Remove space shuttle main engines WORK SCHEDULED: Reconfigure payload bay for ODS installation next month

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