End-to-End Performance
The end-to-end performance of the TRACE instrument incorporates the following:
- Transmission and/or reflectance of all appropriate optical elements,
- Quantum Efficiency of the CCD detector,
- Clear Aperture of the UV Channel, and
- Solid Angle per pixel.
Notes:
- The units on these curves are the product of the above combination of
transmissions, reflectances, quantum efficiencies and geometric
factors. When these units are multiplied against a solar radiance,
the result is a ``spectral count rate'' in units of
electrons/pixel/Å/sec.
- At first glance, the curves look strange. An extreme case is the Ly
Alpha curve, which is dual-peaked. This is a result of the product of a
Lyman Alpha filter peaked at 1216 Å and the multilayer coating
on the primary mirror which peaks at 1550 Å.
- To ease the concern associated with this previous point, we include
curves of sample solar spectra folded through the TRACE instrument in
all channels. The spectrum used here is a curve derived from several
sources:
- The high spectral resolution wavelengths from 1445 Å to 1680
Å is data from the HRTS mission; c.f. Brekke, 1993, ApJ.
Suppl., 87, 443. This data is an ``Active
Region Spectrum'' from the above paper.
- The lower resolution spectrum from 1200-1800 Å is from
the SOLSTICE instrument; e.g. Rottman et al, 1993,
J. Geophys. Res., 98, 10667. This is an
irradiance spectrum averaged
over the full disk. This data was further scaled to match
the UV continuum intensity of the Brekke spectrum.
- The results generated by the above curves are in units of
electrons/pixel/Å/sec. Note this must then be multiplied by an
appropriate factor depending on which CCD amplifier is used;
Amplifier ``A'' is
14 electrons/DN
while Amplifier ``B'' is approximately
53 electrons/DN.
- H I Lyman Alpha Response:
- C IV 1550 Å Response
- UV Continuum (1600 Å and 1700 Å) Response
- White Light Continuum Response
- Visible Calibration notes from Stimulus
Telescope
- Comparison of visible thruput on
different Quadrants
- 1550 Å visible
throughput calculated during spacecraft-level Thermal Balance test
Brian N. Handy
Last modified: Mon Sep 22 10:21:25 PDT 1997