The Galileo Energetic Particles Detector
From Space Science Reviews
LEMMS
The Low Energy Magnetospheric Measurements System
The LEMMS telescopes are designed to measure low to
medium energy ion and electron fluxes with wide dynamic
range and high angular (<20 deg) and temporal (1/3 to 4/3 s)
resolution. As stated previously, a full 4pi coverage of the
unit sphere is obtained by the use of a stepping platform in
conjunction with satellite spin.
The LEMMS detector head is a double-ended telescope
containing eight heavily shielded silicon solid state
surface barrier totally depleted detectors providing
measurements of electrons from 15 keV to > 11 MeV, and ios
from 22 keV to eV to ~55 MeV, in 32 rate channels.
Detail of the EPD LEMMS detector head. |
LEMMS Channel Descriptions
Channel Species Energy Range Geometric Factor Name (MeV) (cm**2 sr) -------------------------------------------------------------------------------- A0 Z >= 1 0.022- 0.042 0.006 A1 Z >= 1 0.042- 0.065 0.006 A2 Z >= 1 0.065- 0.120 0.006 A3 Z >= 1 0.120- 0.280 0.006 A4 Z >= 1 0.280- 0.515 0.006 A5 Z >= 1 0.515- 0.825 0.006 A6 Z >= 1 0.825- 1.68 0.006 A7 Z >= 1 1.68 - 3.20 0.006 A8 Z >= 2 3.50 - 12.4 0.006 B0 Z = 1 3.20 - 10.1 0.006 B1 electrons ~1.5 - 10.5 0.006 B2 Z = 2 16.0 -100. 0.006 DC0 Z >= 1 14.5 - 33.5 0.5 DC1 Z >= 1 51. - 59. 0.5 DC2 electrons >~ 2. 0.5 DC3 electrons >~11. 0.5 E0 electrons 0.015- 0.029 0.006* E1 electrons 0.029- 0.042 0.020* E2 electrons 0.042- 0.055 0.030* E3 electrons 0.055- 0.093 0.033* F0 electrons 0.093- 0.188 0.028* F1 electrons 0.174- 0.304 0.007* F2 electrons 0.304- 0.527 0.016* F3 electrons 0.527- 0.884 0.018* AS singles all counts 0.006 in detector BS singles all counts 0.006 in detector CS singles all counts 0.5 in detector DS singles all counts 0.5 in detector EB1 background sidewise penetrators EB2 background E1E2 coincidences FB1 background Sidewise penetrators FB2 background F1F2 coincidences * Geometric factor determined from table in paper by Y. Wu, T.P. Armstrong.
The geometric factor of the collimator and magnetic optics system has been analyzed by extensive computer modeling (Wu and Armstrong, 1988). The energy dependent aperature-integrated geometry factors for detectors E1 and F1 are shown here.
Response of the EPD LEMMS low energy electron detectors. The geometric factor, as calculated from a detailed simulation shown as a function of energy. |
A diagram of the LEMMS analog electronics is included
next. The unbuffered preamp tail-pulse output signals are
sent down the polytwist wiring harness to three LEMMS analog
boards, where the signals are amplified and shaped. All
signal processing in the LEMMS channels is done in the
linear domain. Comparator-like discriminator circuits
assigned to each of the eight channels fire whe pre-defined
threshold levels are exceeded.
The resulting discriminator outputs are sent to the rate
logic electronics, where combinatorial logic is used to
define 32 rate channels (event bins).
LEMMS data also are processed through a pulse height
analyzer (PHA) that produces 13 46-channel energy spectra
per major frame.
Block diagram of LEMMS analog electronics. |
The detector heads are mounted on a platform and rotated by a stepper motor contained in the main electronics box. The stepper motor positions as seen looking down onto the top of the EPD along the motor rotation axis can be seen in the figure below
The combination of the satellite spin and the stepper
motor rotation (nominally stepping to the next position
after each spacecraft spin) provides 4pi steradian coverage
of the unit sphere. The zero degree ends of the two
telescopes have a clear field of view over the unit sphere
and also can be positioned behind a foreground shield/source
holder for background measurements and in-flight
calibrations. The 180 degree ends experience obscuration
effects in motor positions 4, 5 and 6 caused by the
magnetometer boom and foreground shield.
The primary elements of the system are the LEMMS/CMS
detector heads with their analog electronics, the motorized
scanning system, the digital support electronics, and the
data system. The following figure shows a functional block
diagram of the EPD.
EPD functional block diagram. |
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Technologies Home Page.
Updated 8/23/19, Cameron Crane
QUICK FACTS
Mission Duration: Galileo was planned to have a mission duration of around 8 years, but was kept in operation for 13 years, 11 months, and 3 days, until it was destroyed in a controlled impact with Jupiter on September 21, 2003.
Destination: Galileo's destination was Jupiter and its moons, which it orbitted for 7 years, 9 months, and 13 days.