khayo@sonia.math.ucla.edu (Eric Behr) (05/21/88)
===================================================================== Thursday, May 19, 1988 STS-26 - DISCOVERY (OV 103) - OPF BAY 1 Final testing and flight preparations are continuing on Discovery and roll out of the Orbiter Processing Facility is planned in a few weeks. The helium signature leak test of Discovery's main engines is scheduled to being today. During this two and half day test each of the three main engines will be pressurized with helium so that any leaks will be detected. Today technicians are scheduled to continue shaving tiles on the nose landing gear door and surrounding area to meet specified contour measurements. The payload bay doors have been reopened and final closeouts of the orbiter's midbody are scheduled. A leak check of the crew module was successfully completed yesterday which wrapped up the orbiter's structural pressure test. The primary payload for the STS-26 mission, the Tracking and Data Relay Satellite (TDRS-C), arrived at KSC Monday, May 16. The spacecraft is in the Vertical Processing Facility where pre-flight processing operations occur. The inertial upper stage for the TDRS spacecraft is scheduled to arrive later this month. STS-27 - ATLANTIS (OV 104) - OPF BAY 2 Operations scheduled today include: tests of the brake anti-skid control boxes, installation of two of three fuel cells and leak and functional testing of the liquid oxygen side of the main propulsion system. Orbiter modifications scheduled include chin panel, crew escape and installing protection for wiring in the aft compartment. STS-28 - COLUMBIA (OV 102) - OMRF Powered down orbiter modifications scheduled today include crew escape and bonding heat absorbing strips to the orbiter's belly for the RTV heat sink mod. STS-26 SOLID ROCKET BOOSTERS - VAB/RPSF Later today the right forward center segment is scheduled to be lifted over the sill and into the high bay where it will be mated with the rest of the STS-26 solid rocket motors. After the segment is hanging over the stack, workers will perform inspections, grease the metal parts, install the o-rings and install the field joint assembly fixture (FJAF). The FJAF is a new tool required to mate the tighter fitting redesigned SRMs. Meanwhile, preparations of the right forward segment are continuing in the RPSF. This is the last of four segments for the right hand booster. The nose cones will be attached last. ===================================================================== Friday, May 20, 1988 STS-26 - DISCOVERY (OV 103) - OPF BAY 1 The helium signature test was started yesterday and is scheduled to continue through tomorrow evening. Installation of thermal blankets in the orbiter's midbody is scheduled as orbiter closeouts continue in preparation for rollover to the VAB. A test to monitor the level of outgasing in the crew module is scheduled tomorrow. Routine readings of pressure in the flight tires are being taken. The orbiter will be powered down on Sunday to allow the installation of a few panels in the crew compartment. Fit checks of the nose landing gear door thermal barrier are planned today along with other thermal protection system operations. STS-27 - ATLANTIS (OV 104) - OPF BAY 2 Testing of the brake anti-skid control boxes was completed yesterday. Technicians installed one fuel cell yesterday and are scheduled to install another one today. Orbiter modifications scheduled today include crew escape, chin panel, adding protection for wiring in the aft compartment and elevon cove seal. STS-28 - COLUMBIA (OV 102) - OMRF Technicians finished inspections of the air revitalization system ducts. Meanwhile RTV heat absorbing strips are being installed in Columbia and electrical modifications are being worked in the forward and aft sections of the orbiter. STS-26 SOLID ROCKET BOOSTERS - VAB/RPSF Last night, the right forward center segment was hoisted into the high bay where mating preparations are underway. The right forward segment is being prepared in the RPSF for transfer to the VAB this weekend. The left forward assembly was inspected and checked out in the transfer aisle. This assembly which contains the nose cone will be installed after all the solid rocket motor segments have been stacked on the mobile launcher platform. ===================================================================== Eric