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INSTITUTET FÖR RYMDFYSIK |
UPPSALA |
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Swedish Institute of Space Physics |
(59°50.272′N, 17°38.786′E) |
Student project at IRF Uppsala
Project work /
Examensarbete (30 hp)
Rosetta LAP
operations at the target comet
Student: Kristoffer Hultgren, Luleå Technical
University and Université Paul Sabatier/Toulouse III
Supervisor:
Anders Eriksson
Period: Spring
2009
Abstract
The ESA Rosetta
mission is currently en route to comet 67P/Churyumov-Gerasimenko, where
it will arrive in 2014. Among the instruments onboard, the Langmuir
probe instrument LAP of the Rosetta Plasma Consortium can be expected
to be particularly sensitive to early activation of the comet, as it
can detect small plasma density changes even at the very low densities
typical of the solar wind plasma. By running various operational modes,
LAP can also characterize the denser plasmas expected to appear as the
coma develops, and monitor the plasma dynamics around the comet all
through the mission. In order to be able to exploit these possibilities
from the start of operations at the comet, it is essential to define
useful operational modes in advance. The objective of this project was
to prepare for LAP operations at the comet by simulating LAP
measurements in the plasma environment expected at the comet, and for
what can be regarded as typical operational scenarios for the
spacecraft itself. To do so, results of an ESA-sponsored modeling
activity at the International Space Science Institute formed the
background, combined with a simulation of the LAP measurements. The
results show that for heliocentric distances less than 2 AU, the LAP
probe currents are appropriate to follow the dynamics of the plasma,
but to extract the electron density and temperature dependence so to
give an absolute value of the former we need other instruments, e.g.
MIP designed to measure the electron density and temperature, in
particular inside the contact surface of the comet. The results also
show that around 2 AU, Rosetta has a good chance of occasionally being
located close to the contact surface which creates a very good
possibility of gaining interesting data.
Example plot
An example plot obtained in this project, assuming Rosetta in a
circular orbit of 10 km radius in the terminator plane around the
comet, at 2.0 AU heliocentric distance. The plasma density and B-field
intensity maps at right show that the MHD model in the ICES package
here predicts that this orbit skims the contact surface, giving rise to
the peculiar patterns observed in the magnetic field (top left) and LAP
probe bias sweeps (bottom left; colour code is probe current in nA).
Theta is a phase angle around the comet, while the time axis gives the
orbital time assuming a Kepler orbit around the comet.
Initial project
description
The objective of
this project is to prepare for LAP operations at the comet by
simulating LAP measurements in the plasma environment expected at the
comet, and for what can be regarded as typical operational scenarios
for the spacecraft itself. To do so, results of an ESA-sponsored
modelling activity at the International Space Science Institute (the ISSI
model) and/or
simulations performed at IRF in Kiruna will form the background, to be
combined with a simulation of the LAP measurements. The project
involves gathering of relevant model data, definition of test
scenarios, coding a LAP measurement simulator, running the model,
analyzing the data and assessing the results. The expected project
duration is 20 weeks.
Resources
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