On
the Pegasus XL launch vehicle, the aft skirt has
been installed. The fins
are mechanically mated and alignment is underway. The
GPS and UHF antennas have also been installed.
The
DART spacecraft arrived at Vandenberg Air Force Base
on July 13 to begin final preparations for launch. The spacecraft’s
Reaction Control System (RCS) has been charged with
gaseous nitrogen and leak checks are underway.
DART
has been designed and built for NASA by Orbital Sciences
Corporation as a flight demonstrator to locate and
maneuver near an orbiting satellite. The DART spacecraft weighs about
800 pounds, is nearly 6 feet long and 3 feet in diameter. The
Orbital Sciences Pegasus XL vehicle will launch
DART into a circular polar orbit of approximately
475 miles.
The
Demonstration of Autonomous Rendezvous Technology (DART)
satellite is an advanced flight demonstrator that provides
a key step in establishing autonomous rendezvous capabilities
for the U.S. Space Program. While previous rendezvous
and docking efforts have been piloted by astronauts,
the unmanned DART satellite will have computers and
cameras to perform all of its rendezvous functions.
Once
in orbit, DART will rendezvous with a target satellite,
the Multiple Paths, Beyond-Line-of-Site Communications
(MUBLCOM), also built by Orbital Sciences and launched
in 1999. DART will then
perform several close-proximity operations, such
as moving toward and away from the satellite using
navigation data provided by onboard sensors. The
entire mission will last only 24 hours and will be
accomplished without human intervention. The
DART flight computer will determine its own path
to accomplish its mission objectives.
DART
is designed to demonstrate technologies required
for a spacecraft to locate and rendezvous, or maneuver
close to, other craft in space. Results
from the DART mission will aid in the development
of NASA’s Crew Exploration Vehicle (CEV)
and will also assist in vehicle development for
crew transfer and crew rescue capability to and
from the International Space Station. |