Next: 2.3.6 DEA Hardware
Up: 2.3 Instrument Subsystems
Previous: 2.3.4 Door
Suitable sources have been provided by Isotope Products in convenient
packages (the A-2, a 0.5" diameter cylinder, 0.25"
high).
All three sources will be composed of radioactive 55Fe. One source
will directly
illuminate the focal plane with Mn K and K
X-rays from the
55Fe. In each of the other two sources, X-rays from the 55Fe will
illuminate a metallic target. The source geometry is such that fluorescent
characteristic X-rays from the target illuminate the focal plane. Viewed
from the source, each CCD subtends
ster. Details of
the sources are shown in Table 2.6. Note that the output of
each source will decay with a half-life of 2.7 years.
Serial No. | 55Fe Activity | Target | Principal Line | Flux | Other lines |
mCi(date) | Material | (Energy) | ct s-1 CCD-1 | (keV) | |
(measured) | (August 1998) | ||||
SN301 | 0.055 (8/96) | none | Mn K (5.9,6.4) | 45 | Mn L(.64-.67),Au M(2.2) |
SN802 | 11 (5/97) | Ti | Ti K (4.5,4.9) | 25(est) | Mn K(6.4) |
SN702 | 93 (5/97) | Al | Al K (1.5) | 22(est) | Mn K(6.4) |
55Fe is a highly compatible calibration source for the ACIS.
It causes no CCD background problems and
is routinely
used in lab calibration. A 500 Ci source will provide 160 cts/sec over
a single CCD chip. The needed collimation will reduce this slightly.
Tests were conducted at the MIT CCD lab by exposing chips to this flux level
to search for long term radiation damage
effects on the CCD chip. The total dose at the CCD was found to be less than
10 rads for the entire mission life.
The low Z material collimator (aluminum) is sufficient to ensure that
little fluorescence is caused by the source.
(Low Z reduces the collimator fluorescent yield.)
Two other sources of X-ray calibration lines are available only early in the mission. A contamination monitor source for the HRMA is mounted on the front cover of the mirror assembly. This source will not be visible to ACIS after the sunshade (and front mirror cover) is opened during the Orbital Verification phase, within the first 30 days of on-orbit operations. ACIS will, however, make a measurement of this source in order to measure any mirror contamination up to that point.
The HRMA contamination sources consist of 16 separate sources (one on each of four mirror shells and one on each mirror quadrant). Each source will be a combination of 109Cd and 55Fe, producing the characteristic L lines of Ag (near 3.0 keV), K lines of Mn (near 5.9 and 6.5 keV) and L lines of Mn (near 0.64 keV). Spectra were collected by ACIS from this source during XRCF HRMA/ACIS calibration.
The ACIS Internal Contamination Monitor source is mounted on the interior
surface of the detector assembly door. The primary purpose of the source is
to check for gross contamination of the ACIS blocking filter and focal
plane during initial on-orbit operations.
The 10 Ci 55Fe source (measured in August, 1996)
emits Mn L (645-670 eV) and Mn K (5.9 and 6.4 keV)
X-rays in a fixed flux ratio (about 300:1, as detected with the ACIS UV optical
blocking filter in place.)
In order to minimize scattering
of the emitted X-rays when the door is open, the ICM is equipped with a
collimator. The collimator allows only a small
fraction of detectors S2 and S3 to be illuminated when the door is closed.
The ACIS door can in principle be closed to utilize this source,
but the operational risk of failure to reopen is likely to prevent
this use in any situation except for extreme emergencies.
John Nousek