AMPTE
The Mission
The Active Magnetospheric Particle Tracer Explorer mission was designed to
- Investigate the transfer of mass and energy from the solar wind to the
magnetosphere
- study the interaction between artificial and natural space
plasmas
- to establish the composition and dynamics of the charged
population in the magnetosphere over a broad energy range.
The Spacecraft
This was a three-nation project consisting of three satellites, the German Ion
Release Module (IRM), the US Charge Composition Explorer (CCE) and the UK
Subsatellite (UKS). All three satellites were launched by a single Delta
rocket on 16th August 1984. IRM and UKS were placed in nearly identical orbits
of high eccentricity that carried them regularly through the magnetopause and
bow shock and into the solar wind. CCE was placed in a near-equatorial orbit
with smaller eccentricity to maximize coverage of the ring current.
CCE IRM UKS
Apogee 8.8Re 18.7Re 18.7Re
Period 15.6hrs 44.3hrs 44.3hrs
Inclination <5deg 28.8deg 28.8deg
Mass 242kg 705kg 77kg
For further general information you may wish to connnect to
the Ampte page of the U.S.A.'s
National
Space Science Data Center.
IRM, the largest of the three satellites (with a mass of 705 kg at launch), was
built by the Max Planck Institute for Physics and Astrophysics.
As its name suggests it was equipped with
16 canisters of either Lithium or of Barium which, on being ejected and
'opened' (a safe distance from the spacecraft!) generated clouds of
neutral atoms which were quite rapidly ionised by sunlight. The ions then
interact with their local space plasma environment. Comets generate
a neutral gas cloud too (called the coma) when they come 'close' to the
Sun, which is also ionised by sunlight, thus studies of the releases have
helped us to understand some of the processes of cometary interactions
with the solar wind. The ion releases were performed in the solar wind,
magnetosheath and geomagnetic tail. UKS monitored the process from close
range while CCE was stationed (during dayside releases) downstream of IRM so
as to detect ions any ions which penetrated the magnetopause. Lithium and
Barium are good 'tracer ions' since they are unusual in naturally occuring
space plasmas, so a detection would almost certainly indicate that IRM had
been the source). It was hoped that the record of when and where
detections occurred would tell us about how ions are transported from the
magnetosheath into the magnetosphere, and throughout the magnetosphere.
CCE (mass 242 kg) developed by the Applied Physics Laboratory of The Johns
Hopkins University, observed the ring current and plasma sheet. It carried out
sensitive measurements of plasma composition as well as having a special role
in the attempt to detect ions released by IRM when IRM was upstream of CCE.
For further information about CCE, its instruments and data archive you may
wish to connect to
The AMPTE Science Data Center at the Johns Hopkins University/Applied
Physics Laboratory in the U.S.A.
UKS was developed by the Mullard Space Science Laboratory and the
Rutherford-Appleton Laboratory. At 77 kg it has a mass virtually a tenth that
of the IRM! It carried an electron
spectrometer, an ion spectrometer, a particle correlator, a magnetometer
and a plasma wave detector. During the chemical releases, the proximity of UKS
and IRM meant that instruments aboard UKS saw the magnetic cavity created by
the ionized gas. Differences
in observations at IRM and UKS were used to infer the spatial structure and
evolution of the comet-like gas cloud.
All three satellites were also used independently to study the magnetosphere,
magnetosheath, solar wind and the boundaries between them. The Geophysical Data
Facility at Rutherford-Appleton Laborotory contains a database of AMPTE-UKS and
IRM data. (As noted above CCE data is stored in the U.S.A.).
The AMPTE UKS Ion Instrument
Built by the Mullard Space Science Laboratory, this comprised two electrostatic
analysers.
The instrument measured ions in the energy range 10 eV to 20 keV. The energy
range was divided up into either 30 or 60 logarithmically space energy levels.
The instrument achieved all-sky coverage each spin, returning data from 4 polar
sectors and 8 azimuthal sectors (i.e. 32 patches of the sky).
High telemetry rates allowed the transmission of fully 3-d ion distributions
every 5s spin period. Thus the
instrument provided high time, energy and angular resolution for its time, and
even by todays standards.
Different operational modes modified the angular and energy resolution to suit
the type of observation required and telemetry limitations. A special solar
wind mode concentrated measurements around the solar direction, while still
monitoring the rest of the sky in the usual way. Thus the instrument could
make good quality measurements of both foreshock ions and the solar wind
simultaneously. The instrument was used principally for observations of the
low-latitude boundary layer, magnetopause, magnetosheath, bow shock,
foreshock and solar wind and observations related to the chemical releases.
References
A.J.Coates, J.A.Bowles, R.A.Gowen, B.K.Hancock, A.D.Johnstone and S.J.Kellock,
The AMPTE UKS Three-Dimensional Ion Experiment,
IEEE Trans. Geoscience and Remote Sensing, vol.GE-23, no.3, p. 287, May
1985.
All three spacecraft and their instruments are described in papers in the same
volume.
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