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CREW:
John
H. Casper, Commander; Curtis L. Brown Jr., Pilot; Daniel W. Bursch, Mission
Specialist; Mario Runco, Jr., Mission Specialist; Marc
Garneau, Mission Specialist (CSA); Andrew S. W. Thomas,
Mission Specialist
LAUNCH
INFO:
Date: Sept.
16, 1996
Time: 4:54 a.m. EDT
Site: Kennedy Space Center, FL
SHUTTLE
FLIGHT:
Orbiter: Atlantis
(OV-104)
Orbit Altitude: 196–245 nautical
miles
Orbit Inclination: 51.6°
Mission Duration: 10 Days, 3 hours,
19 minutes
MIR
DOCKING:
Docking: 4th Mir Docking
Dock Date: Sept. 17, 1996
Dock Time: 10:13 p.m. CDT
Undock Date: Sept. 23, 1996
Undock Time: 8:31 p.m. CDT
LANDING
INFO:
Date: Sept.
26, 1996
Time: 8:14 a.m. EDT
Site: Kennedy Space Center, FL
PAYLOAD(S):
SPACEHAB-LDM Logistics
Double
Module* (FU2/FU3)
*Maiden
voyage of the LDM
[View
Experiment Details]

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Mission Patch]
The
new SPACEHAB Logistic Double Module (LDM) debuted
on STS-79, providing commercial logistics resupply
services for Phase I of the International Space
Station Program.
The 7,100 pounds of cargo carried in the LDM included Russian logistics items,
Risk Mitigation Experiments (RMEs), science experiments and resupply hardware,
unique hardware in support of Phase I requirements, and crew supplies, such as
food and clothing. The mission's cargo was accommodated in three double racks
and one single rack in the LDM, including the first soft stowage double rack,
a double rack housing the gyrodyne and Individual Equipment and Seat Liner, the
first International Space Station Payload Rack (ISPR) to fly in space housing
the Active Rack Isolation System (ARIS), and one single rack housing the Extreme
Temperature Translation Furnace (ETTF) and Real-Time Radiation Monitoring and
Detection Device (RRMD). SPACEHAB developed a unique structure to accommodate
the ISPR, an ISPR Structural Adapter or ISA.
The logistics items carried in the SPACEHAB Modules during the Shuttle-Mir missions
included vital equipment and supplies required by astronauts to live and work
in space for extended periods. Specific items included a Russian gyrodyne, which
is a device used to stabilize Mir, power sources such as the large storage batteries
carried up three at a time, and the individual equipment and seat liner for the
U.S. astronaut in case of the need for an emergency return to Earth in a Russian
Soyuz capsule. A vast array of daily-use items also were carried as logistics,
such as laptop computers and associated cables and disk drives, flashlights,
digital timers, mission schedule reference documents, food packages, personal
hygiene equipment, and clothing and sleeping garments.
The LDM is composed of two SPACEHAB flight units. A science-equipped Single Module
is the forward half of the structure, with a cargo-equipped Single Module as
the aft half. A new intermediate adapter ring mates the two flight units. There
is limited science carried in the aft half of the LDM, so a full floor is not
necessary. Two roof-top viewports are available for rendezvous and docking operations,
as well as for mission documentation photography. The LDM has a total cargo capacity
of nearly 10,000 pounds.
Most of the logistics items that are stowed inside the LDM are housed inside
a soft stowage system. The system is a series of canvas-like bags, similar to
backpacks or duffel bags, in various sizes that attach to the interior surfaces
of the Module. The primary size bag is equivalent to a middeck locker to facilitate
loading into the Module. Most bags are secured to the interior surface of the
Module with a strap and buckle, similar to an automobile seat belt.
To secure the contents inside the bags, foam is specially cut at SPACEHAB Payload
Processing Facility in Cape Canaveral, Florida, to form fit around the logistics
items inside or a foam pillow is fitted to the contents. The bags weigh less
than standard middeck lockers which typically house science experiments, allowing
mission managers to manifest more and varied cargo to be carried in SPACEHAB
Modules.
The system allows for an average of up to 20% more cargo than standard lockers.
A unique double rack structure was added to the aft half of the LDM to stow 16
soft stowage system bags. Because the aft half of the LDM did not have a floor
in this place on this mission, seven soft bags were mounted directly to the Module's
subfloor.
To facilitate the astronauts transfer of the bags to and from the LDM and Mir,
a system was developed using a visual cue of color coded cards in red, white
and blue. The contents of the bags marked with a red card are transferred to
Mir and remain there, the contents of the bags marked with a white card may transfer
out of the Module for use on-orbit, but are carried back to Earth in the Module,
and the bags marked with a blue card remain in the Module and are filled with
contents transferred from Mir.
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