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CREW:
James
D. Wetherbee, Commander; Eileen M. Collins, Pilot; C. Michael Foale, Ph.D.,
Mission Specialist; Janice E. Voss, Ph.D., Mission Specialist; Bernard A.
Harris, Jr., M.D., Mission Specialist; Vladimir G. Titov, Cosmonaut
LAUNCH
INFO:
Date: Feb.
3, 1995
Time: 12:22 a.m. EST
Site: Kennedy Space Center, FL
SHUTTLE
FLIGHT:
Orbiter: Discovery
(OV-103)
Orbit Altitude: 213 nautical miles
Orbit Inclination: 51.6°
Mission Duration: 8 Days, 6 hours,
28 minutes
LANDING
INFO:
Date: Feb. 11, 1995
Time: 6:51 p.m. EST
Site: Kennedy Space Center, FL
PAYLOAD(S):
SPACEHAB-SM Single
Module (FU1)
SPARTAN204
[View
Experiment Details]

[Download
Mission Patch]
When
Discovery took to orbit for the 20th time, NASA
set the stage for future international cooperation
in a pathfinding mission featuring a rendezvous
with the Russian Space Station Mir, an assortment
of scientific and commercial investigations in
the SPACEHAB and a five-hour spacewalk.
STS-63's highest priority objective was to rendezvous with Mir in a dress rehearsal
of docking missions that followed later in 1995. On the mission, Eileen Collins
became the first woman to pilot a Space Shuttle mission. She was joined by
the second Russian cosmonaut to fly aboard a U.S. Space Shuttle, Vladimir Titov.
SPACEHAB New System Features
As a result of experience gained on the first two SPACEHAB missions, it was
clear that there were some resources that SPACEHAB shares with the Space Shuttle
that are very scarce. One of those resources is crew time. SPACEHAB developed
two new system features to reduce the demands on crew time significantly. The
first new feature was a video switch to reduce the demand for crew time in
video operations, and the second new feature was an experiment interface to
the SPACEHAB telemetry system to reduce the demand for crew time in experiment
data downlink.
Video Switch
The SPACEHAB video system uses camcorders that are tied to the Orbiter closed
circuit television system and then downlinked through the Orbiter. On prior
SPACEHAB missions, the crew set up the camcorders and manually switched from
one camera to another, a time-consuming operational arrangement.
For
this mission SPACEHAB installed a video switching
unit allowing up to eight camcorders to be cabled
into the SPACEHAB video switch. Then, by ground
control, one of the camcorders could be switched
into the Orbiter system for downlink. Also, another
one of the camcorders could collect a digital image
on a freeze frame and send it down through SPACEHAB's
telemetry stream, independent of other Orbiter
video downlink operations. This new video switch
and digital television downlink capability provides
operational flexibility that is valuable on this
flight and on subsequent flights.
Experiment
Data Interface
SPACEHAB
has enhanced the experiment data interface with the
SPACEHAB telemetry system in the interest of on-orbit
efficiency. The SPACEHAB telemetry system now allows
an experimenter with a standard RS232 computer interface
to tie directly into the system and send continuous
information down to the ground, offloading this task
from the crew and enhancing ground controller monitoring
of experiment status.
Windows
On
the roof of the SPACEHAB laboratory, two 12-inch
diameter windows were installed for STS-63. One window
has a NASA docking camera to assist in the Mir proximity
operations.
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