DESCRIPTION |
Instrument Overview
===================
The Ion Composition Instrument is a novel spectrometer for measuring
the ionic composition of the solar wind from the ICE (ISEE-C, ISEE3)
spacecraft. The resolution and dynamic range of the instrument are
sufficient to be able to resolve up to twelve individual ions or groups
of ions. This will permit the solution of a number of fundamental
problems related to solar abundances and the formation of the solar
wind. The spectrometer is composed of a stigmatic Wien filter and
hemispherical electrostatic energy analyzer. The use of curved
electric field plates in the filter results in a substantial saving of
weight with respect to a conventional filter of the same resolution and
angular acceptance.
The spectrometer is controlled by a microprocessor based on a special
purpose computer which has three modes of operations: full and partial
survey modes and a search mode. In the search mode, the instrument
locks on to the solar wind. This allows four times the time resolution
of the full survey mode and yields a full mass spectrum every 12.6 min.
SCIENTIFIC OVERVIEW
===================
ION COMPOSITION studies in the solar wind are essential for
understanding the dynamics and energetics of the solar wind
acceleration region, and are an important source of solar abundance
information. The ion composition of the solar wind is, however, poorly
known because of the technical difficulties associated with the
separation of the different ions over the wide dynamic range involved.
With electrostatic energy analyzers, the He+2 /H+ abundance ratio has
been studied extensively in the solar wind, and large variations found.
During quiet low-temperature conditions, ions other than H+ and 4He+2
have been separated with this technique and the presence of heavy ions
has been demonstrated. In addition, some information about abundances
and charge state distributions has been obtained.
The foil collection technique has been used to determine the abundances
of the isotopes of He, Ne, and Ar in the solar wind. Although this
method has yielded precise abundance data, its time resolution is
limited.
The ICE spacecraft will be continuously in the solar wind and thus
affords an opportunity for a comprehensive uninterrupted composition
study. With a continuous record of such a large number of ions,
fundamental problems concerning the origin of the solar wind and solar
composition can be investigated. Some of these are discussed below.
1) A number of momentum transfer mechanisms for the acceleration of
heavy ions into the solar wind have been proposed. Under the inferred
conditions in the solar wind source region, coulomb collisions would be
sufficient to transfer momentum from protons to heavy ions with high
Z**2/M ratios. Momentum transfer by waves has also been proposed as an
efficient mechanism.
To assess the relative importance of the various mechanisms,
measurements of solar wind ions over a large range of M and Z under
varying conditions in the corona and solar wind are necessary.
2) Bame et al. (1978) have recently proposed that the He/H ratio of
0.04-0.05 typically found in fast solar wind streamers be equated with
the He/H ratio in the outer convective zone of the sun. This is a
factor of two lower than the generally accepted value and, if
correct, would reduce the calculated boron neutrino flux. A
comprehensive investigation of the ion abundance variations should lead
to a better understanding of ion fractionation processes in the solar
corona, and in turn should yield accurate estimates of the He/H ratio.
3) A correlation between the He/H ratio and solar wind speed has been
observed but the mechanism is unknown. By extending correlation studies
to other ions it may be possible to uncover the mechanism.
4) Local temperatures and temperature gradients in the corona can be
estimated from measurement of the charge distribution of Fe ions and
the charge states of 0 and Si. To test the validity of the various
solar wind expansion models, the experimentally derived temperatures
and gradients can be compared to those derived from the models.
5) An average 4He/3He ratio of 2350 +- 120 has been derived from the
five Apollo solar wind foil experiments , however, the ratio appears to
be highly variable. In one instance, a ratio of 500 was observed over
a two-day period With the mass spectrometer on ICE (ISEE-C), 3He will
be continuously monitored, permitting an accurate determination of the
solar surface abundance of this cosmologically important nucleus. The
relation between anomalous 3He abundances in the solar wind and the
small 4 He/3He ratios in some solar flares can also be studied.
Calibration
===========
The sensor was calibrated at the test facility of the Physikalisches
Institut of the University of Bern. This facility consists of a
vacuum chamber in which a homogeneous monoenergetic mass separated
beam of ions can be produced and directed at the sensor mounted on a
test platform which can be rotated about two axes perpendicular to the
direction of the ion beam. Sweep circuits were used to synchronously
change the voltages on the plates of the filter and analyzer while the
outputs of each of the three CEM's strobed a multi-channel analyzer
operating in the pulse-height-analysis mode. Calibrations were
performed with H2+ and He+ at nominal velocities of 300, 400, 500, and
600 km/s. The orientation of the sensor with respect to the incident
ion beam was changed in small increments over a range of +- 8 degree in
the horizontal plane and +- 14 degree in the vertical plane. Angular
acceptances derived from these functions are in good agreement with
theory, whereas the experimental resolution always exceeds that
predicted. The absolute values of the transmission determined at normal
incidence for H2+ and 4He+ at the four different values of ion velocity
are in excellent agreement with theory. The ability of the instrument
to reject stray ions which create ghost peaks by scattering from the
outside plates of the analyzer and contribute to the background was
measured. In all cases, the ratio of ghost peak counts to counts in
the main peak was less than 10**-4 with the ghost peaks always
appearing at energy values 7 percent less than those of the
corresponding main peaks. Because of the large difference in M/Z
between 4He and 3He, interference of 4He+2 at the position of the 3He+2
peak is less than 10**-5 of the 4He signal.
Operational Considerations
==========================
The input voltages to the power supplies which provide the potential to
the electric field plates of the Wien filter and energy analyzer are
obtained from 12-bit digital-to-analog converters. The digital
inputs to the converters come from the microcomputer-based processor.
The full parameter range covered by the experiment is 300-600 km/s in
velocity, 840- 11720 eV/Z in energy per charge, and 1.5-5.6 in mass per
charge. The velocity range is divided into n steps and the energy
per charge range into m steps, with both being logarithmically
related.
V(1s), (n, m) = R1**(m-1)*R2**(n-1)*V1(1,1), energy analyzer
V(2s),(n) = R2** (n -1)*V2 (1), Wien filter
1 < n < 24, 1
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