5-14-03 SPACECRAFT AND EXPENDABLE VEHICLES STATUS REPORT

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SPACECRAFT AND EXPENDABLE VEHICLES STATUS REPORT
May 14, 2003

George H. Diller
Kennedy Space Center
321/867-2468
                                         
MISSION: Mars Exploration Rover (MER-2)
LAUNCH VEHICLES: Delta II/Delta II Heavy
LAUNCH PADS: 17-A
LAUNCH DATES: June 5
LAUNCH TIMES: 2:16 p.m. / 2:55:29 p.m. EDT

          Mating of the MER-2 entry vehicle to the cruise stage was
completed on May 7.  The spacecraft has completed its weight and center of
gravity determination and underwent its initial spin balance testing.  On
May 11 the spacecraft was fueled.  Tomorrow night, May 15, will be second
spin test now that the spacecraft is fueled.

          During routine testing of the cruise stage and the MER-2 rover
over the weekend, an unexpected measurement in the rover's power system was
observed.  Troubleshooting is under way but it is not expected to delay the
schedule of planned pre-launch spacecraft preparations at this time.  

          The mission will have two launch opportunities each day during the
launch period, which is scheduled to close on June 19.  Arrival at Mars is
set for Jan 4, 2003, regardless of the launch date within that period.
     
          On Cape Canaveral Air Force Station, the solid rocket booster
erection begins today with the first three set of motors being attached to
the first stage, the second set of three will be erected on Thursday, May
15, and the final set will be hoisted into position on Friday, May 16.  The
first stage was erected on Pad 17-A on Wednesday, April 23.  The second
stage erection was completed on Monday, April 28 and the fairing was hoisted
into the white room on April 30.  The Simulated Flight test of the first
stage was successfully completed May 9.  The spacecraft is scheduled to be
mated to the third stage in the Payload Hazardous Servicing Facility (PHSF)
on May 23.  MER-2 will be transported to the launch pad on May 27.  


MISSION: Mars Exploration Rover (MER-2)
LAUNCH VEHICLE: Delta II Heavy
LAUNCH PAD:  17-B
LAUNCH DATE:  June 25, 2003
LAUNCH TIME:  12:38:16 a.m. / 1:19:19 a.m. EDT

          On MER-1, rover installation onto the base petal and lander air
bag installation were completed on May 9.  The operation to install the
backshell over the lander begins tonight and is scheduled to be complete on
Friday.  Full integration of the MER-1 entry vehicle (back shell, heat
shield, lander and rover) is to be completed by May 21 and followed by
mating the entry vehicle to the cruise stage.

          The MER-B vehicle's first stage is on Pad 17-B and the solid
rocket boosters will be erected May 19-24; the second stage will be hoisted
atop the first stage on May 28. 


MISSION:  SCISAT-1/Atmospheric Chemistry Experiment
LAUNCH VEHICLE: Pegasus XL
LAUNCH FACILITY: Vandenberg Air Force Base, California
LAUNCH DATE: NET July 25, 2003
LAUNCH TIME:  10:36:55 p.m. - 11:34:04 p.m.

          The SCISAT spacecraft is completing final testing at the Canadian
Space Agency's David Florida Laboratories.  The pre-ship review prior to
transportation of the spacecraft to Vandenberg Air Force Base is to be held
near the end of the month.

          SCISAT-1 weighs approximately 330 pounds and will be placed in a
400-mile-high polar orbit to investigate processes that control the
distribution of ozone in the upper atmosphere.    

          Meanwhile, the Pegasus XL rocket is undergoing prelaunch
preparations at Vandenberg Air Force Base in California by Orbital Sciences
Corporation.

          The scientific mission of SCISAT-1/ACE (Atmospheric Chemistry
Experiment) mission is to measure and understand the chemical processes that
control the distribution of ozone in the Earth's atmosphere, particularly at
high altitudes.  The data from the satellite will provide Canadian and
international scientists with improved measurements relating to global ozone
processes and help policy makers assess existing environmental policy and
develop protective measures for improving the health of our atmosphere,
preventing further zone depletion.  The mission is designed to last two
years.


MISSION: Space Infrared Telescope Facility (SIRTF)
LAUNCH VEHICLE: Delta II Heavy
LAUNCH PAD: 17-B, Cape Canaveral Air Force Station
LAUNCH DATE:  August 27, 2003 
LAUNCH TIME:   TBD

          The SIRTF observatory is in NASA's class 10,000 laminar flow clean
room at spacecraft Hangar AE awaiting its return to the launch pad,
currently anticipated to occur in mid-August. 

          Project management of SIRTF for NASA is by the Jet Propulsion
Laboratory.  The observatory has been built for NASA by Lockheed Martin and
Ball Aerospace.

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