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KENNEDY SPACE CENTER SPACE SHUTTLE STATUS REPORT FRIDAY, NOVEMBER 11, 1994 (10:54 AM EST) MISSION: STS-66 -- ATLAS-3/CRISTA-SPAS FLIGHT DAY 9 VEHICLE: Atlantis/OV-104 ORBITAL ALTITUDE: 189 sm LOCATION: en orbit INCLINATION: 57 degrees LAUNCH DATE and TIME: Nov. 3 at 11:59 a.m. EST KSC LANDING DATE and TIME: Nov. 14 at 7:46 a.m. MISSION DURATION: 10 days/19 hours/46 minutes Landing of Atlantis at Kennedy Space Center remains scheduled for Monday, Nov. 14, at 7:46 a.m. EST on the first of two opportunities. The second KSC landing opportunity occurs at about 9:20 a.m. Two landing opportunities are available for Tuesday at KSC. Monday's landing weather outlook is generally favorable. Weather specifics will be available tomorrow. (Mission STS-66 status reports are issued daily by Johnson Space Center, Houston, Tx.) CREW: Commander Don McMonagle; Pilot Curtis Brown; and Mission Specialists Ellen Ochoa, Joseph Tanner, Jean-Francois Clervoy and Scott Parazynski. MISSION: STS-63 -- MIR RENDEZVOUS, SPARTAN and SPACEHAB-3 VEHICLE: Discovery/OV-103 ORBITAL ALTITUDE: 196 sm LOCATION: OPF bay 2 INCLINATION: 51.60 degrees TARGET LAUNCH DATE: Feb. 2 MISSION DURATION: 8 days/4 hours LAUNCH TIME: 12:40 a.m. EST LAUNCH WINDOW: 5 minutes TARGET KSC LANDING DATE/TIME: Feb. 10/4:55 a.m. IN WORK TODAY: Preparations to install Spacehab tunnel adapter Reconfigure payload bay water lines Landing gear functional checks Test microwave scanning beam landing system WORK COMPLETED: Water spray boiler borescope checks Brake anti-skid tests WORK SCHEDULED NEXT WEEK: Preparations to install main engines Install forward reaction control system Water spray boiler leak and functional checks Crew compartment leak checks MISSION: STS-67 -- ASTRO-2 VEHICLE: Endeavour/OV-105 ORBITAL ALTITUDE: 218 sm LOCATION: OPF bay 1 INCLINATION: 28.45 degrees TARGET LAUNCH PERIOD: late February CREW SIZE: 7 APPROX. LAUNCH TIME: very early morning KSC LANDING DATE/TIME: TBD LAUNCH WINDOW: 2 hours/3 minutes MISSION DURATION: 13 D/14H IN WORK TODAY: Preparations to remove and replace fuel cell no. 2 Main propulsion system verification checks WORK SCHEDULED NEXT WEEK: Functional checks of orbital maneuvering system pods Remove and replace fuel cell no. 2 Install extended duration orbiter pallet WORK COMPLETED: Remove main engines Forward reaction control system functional checks Remove GAS can payload