Sjekk hvor teleskopet befinner seg i sin ferd mot Lagrange L2 punktet, 1,5 mill. km. fra jorda, her: https://tinyurl.com/44fcxsyh - Du finner også videoer med hva som skjer underveis. Nå gjelder det å få ut solskjermingen; det sølvblanke i illustrasjonen under. (Red.)
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(Image Courtesy: NASA)
Due to Precision Launch, NASA Says Webb
Space Telescope’s Fuel Likely To Last Way More Than 10 Years
After a successful launch of NASA’s James Webb Space Telescope on December
25, and completion of two mid-course correction maneuvers, the Webb team has
analyzed its initial trajectory and determined the observatory should have
enough propellant to allow support of science operations in orbit for
significantly more than a 10-year science lifetime. (The minimum baseline for
the mission is five years.)
Arianespace’s Ariane 5 rocket launches with NASA’s James Webb Space
Telescope onboard, Saturday, December 25, 2021, from the ELA-3 Launch Zone of
Europe’s Spaceport at the Guiana Space Centre in Kourou, French Guiana. The
James Webb Space Telescope (sometimes called JWST or Webb) is a large infrared
telescope with a 21.3 foot (6.5 meter) primary mirror. The observatory will
study every phase of cosmic history—from within our solar system to the most
distant observable galaxies in the early universe.
The analysis shows that less propellant than originally planned for is
needed to correct Webb’s trajectory toward its final orbit around the second
Lagrange point known as L2, a point of gravitational balance on the far side of
Earth away from the Sun. Consequently, Webb will have much more than the
baseline estimate of propellant – though many factors could ultimately affect
Webb’s duration of operation.
Webb has rocket propellant onboard not only for midcourse correction and
insertion into orbit around L2, but also for necessary functions during the life
of the mission, including “station keeping” maneuvers – small thruster burns to
adjust Webb’s orbit — as well as what’s known as momentum management, which
maintains Webb’s orientation in space.
The extra propellant is largely due to the precision of the Arianespace
Ariane 5 launch, which exceeded the requirements needed to put Webb on the right
path, as well as the precision of the first mid-course correction maneuver – a
relatively small, 65-minute burn after launch that added approximately 45 mph
(20 meters/sec) to the observatory’s speed. A second correction maneuver
occurred on December 27, adding around 6.3 mph (2.8 meters/sec) to the
speed.
The accuracy of the launch trajectory had another result: the timing of the
solar array deployment. That deployment was executed automatically after
separation from the Ariane 5 based on a stored command to deploy either when
Webb reached a certain attitude toward the Sun ideal for capturing sunlight to
power the observatory – or automatically at 33 minutes after launch. Because
Webb was already in the correct attitude after separation from the Ariane 5
second stage, the solar array was able to deploy about a minute and a half after
separation, approximately 29 minutes after launch.
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