Title: PACS
1PACS
- Test Cryostat,
- OGSE and MGSE
Gerd Jakob MPE
2Test Equipment and OGSE Overview
3PACS test cryostat specifications
- Two liquid helium reservoirs 70l for 4.2K and
13l for 1.7K level - 90l liquid nitrogen for thermal shielding
- Optical bench diameter 1060mm, covered by 4.2K
thermal shield with 900mm available height for
PACS FPU test optics - Hold time of each temperature level 48 hours
with full PACS operation (goal) - Specified mechanical, optical and electrical
interfaces to PACS FPU and test equipment - 2 FIR windows for calibration sources input and
for optical alignment checks - 2 window shutter/filter mechanisms at 77K shield
- Cryogenic filters at 77K and 4.2K shields to
provide predicted Herschel telescope background - Representative cryogenic harness with 1100 wires
227 shields for FPU, 124 wires 20 shields
for cryostat and test equipment - Specific mounting rack for different cryostat
operation positions, e.g. 30 tilt for cooler
recycling 90 tilt for shield mounting and
cryostat transport. - Provide clean instrument environment, payload
integration in cleanroom class 1000
4Test cryostat status
- Cryostat built at Cryovac GmbHMPEs design
specifications fulfilled - Cryo harness built, integrated with cryostat and
tested by MPE in cw31/03 - Several cryo tests performed-hold time 77K
level 57h-hold time pumped 1.7K level gt60h,
lowest temperature 1.4K-hold time 4.2K level
56h, but only without 4.2K-shield! - Cryostat failed last acceptance test with
4.2K-shield in cw 42/03 - Optical bench temperature too high (6,3K) 4.2K
LHe-tank hold time 24 hours (48h goal) shield
temp. 25K - Heat dissipation on 4.2K level 1W higher than
without 4.2K-shield - Investigations on a presumable thermal link
ongoing modifications and amendments in progress - Delivery to MPE for optical alignment of test
optics with STM after successful acceptance test,
end Nov.03
FPU integration
evacuation
operation with 20tilt
optical bench dia.1060mm
cryostat transportation
PACS cryostat in different positions Overall
height 2400mm, Mounting rack 1400mm x 2100mm
5Test optics and Herschel telescope simulator
specifications
- Herschel telescope simulator test optics to be
integrated with test cryostat, aligned to PACS
FPU and operated at 4.2K - Image quality goal 3µm wave front error (?PACS),
field distortion less than 1 blue photometer
detector pixel for the total chopped PACS field
of view - Design of a complex opto-mechanical imaging and
baffling system, internal and external
calibration sources - Provision of FIR background based on Herschel
telescope temperature of 70K-90K - 3 cryogenic mechanisms for different internal and
external calibration source selection - 2 internal calibrated cryogenic blackbodies
- TUFIR wavelength calibrator in combination with
an internal integrating sphere - TUFIR input in combination with a point source
simulator - External blackbody, extended or with point source
simulator - Water vapor absorption cell for initial
wavelength calibration
6Test optics schematic and design
3D design of test optics and Herschel telescope
simulator
7Test optics status
- Herschel telescope simulator test optics
designed, built and assembled at MPE - Rigid tripod structure with optics base plate and
stray light reducing housing to be integrated
with test cryostat - Interfaces to cryostat, calibration sources and
test equipment complete - Test optics harness parts under final assembly
- Temperature sensors, positions sensors and read
outs implemented - Test equipment available
- Integration of 10 mirrors, integrating sphere,
mechanisms and optical alignment is ongoing - Optical alignment accuracy goal of test optics to
PACS FPU within /- 1 arcmin by means of a
minimum of 3 cryogenic tests to be performed in
test cryostat
8Test optics status ctd.
- FIR black coating according KT72-process applied
to test optics housing and components - 7 temperature sensors on motors, pupil P1,
mirrors, structure - Thermal I/F and cooling straps for PACS FPU
manufactured and available - The MPE developed cryo torquer motor was
successfully operated at 4.2K - Motor life time test with gear box successful at
4.2K - Chopper wheel performance test at 4.2K to be
repeated with reduced friction of angular ball
bearing in order to achieve the goal for chopping
frequencies up to 2Hz - Flip mirror mechanisms to be tested at 4.2K in
combination with motor/gear - Alignment and integration is performed in
cleanroom class 1000
Test optics and PACS FPU STM
Cryo flip mirror Mechanism1 assembly with gear
box and cryo torquer motor
9Internal calibration source cryogenic blackbody
- Design and manufacturing of 2 identical cryogenic
blackbodies for absolute flux calibration and
background devices selected or chopped by test
optics chopper wheel - 18mm opening of cavity adapted to test optics
pupils P4 and P5 - FIR coating acc. KT72-process applied
- Operational temperature range 4.2K 80K
- Typical temperatures of 10K 60K can be
stabilized within 35 minutes by a heaterpower of
100mW with controller LS370 - Power dissipation typically 12.5mW at 30K and
35mW at 50K - Absolute temperature accuracy /-20mK at 20K and
/-35mK at 50K with integrated calibrated
temperature sensor CX-1070 and contr. LS370 - Thermal stability requirement of lt/-1.25mK at
30K and lt/-5mK at 50K feasible - Status final assembly ongoing, test equipment
available, tests at cryogenic temperature to be
performed during test optics alignment checks
MPE design of a cryogenic blackbody
10External calibration source TUFIR and I/F
- TUFIR (tunable high resolution coherent FIR
radiation source) used for final wavelength
calibration and spectral ghost detection - I/F implemented in test optics designinput
through cryostat windows 1 and 2 selected by
cryo-mechanisms - Window 1-4.2K-aperture for 300K background
reduction-f/4.4 light cone for TUFIR beam
collection-integrating sphere dia. 80mm for
homogenous illumination of pupil P3 and for
filling the telescope simulator beam-background
heater to simulate Herschel telescope
temperatures of 70K-90K - Window 2-point source mask in combination with
TUFIR located in external focus F2 PACS chopped
field of view completely covered-Herschel
telescope background simulated by attenuation
filter sets on different temperature levels - Status test optics I/F available, TUFIR I/F to
be defined
Test optics with integrating sphere,
4.2K-aperture and background heater for TUFIR
input through cryostat window1
11External calibration source blackbody
- External blackbody in combination with scannable
point source simulator for point spread function
and grating alignment investigations - Design of X/Y translation stage and point source
simulator finished - Scanning area covers the complete field of
external focus F2 - Reproducibility goal 20µm
- Point source simulation pattern to be PC
controlled and synchronized with PACS data
read-out - Calibrated blackbody source and controller
available, temperature range 300K 750K, maximum
cavity opening dia. 25mm - Hot plate alternatively foreseen
- Status manufacturing has been started
Schematic of external blackbody set-up
(above) and 3D design with point source mask on
X/Y translation stage, aligned with cryostat
window2
12External calibration source water vapor source
- Design of a water vapor absorption cell for
initialwavelength calibration - 300mm absorption pathlength and typical
watervapor pressure of10-25mbar provide
appropriate absorptionlines in the
PACSwavelength range - Alternative gas CO foreseen
- Hot plate provides background, temperature range
300K 600K - Alignment with external focus F2 at test cryostat
window 2 - Status final design finished end of Nov.03
schematic of the water vapor source set-up
(above) and 3D design of absorption cell aligned
with cryostat window 2
13Mechanical ground support equipment MGSE
Crane with fine drives installed in MPE
PACS cleanroom class 1000, 07/03
Hoisting device for PACS FPU available, used
for STM integration 06/03
Pumping unit available, containing oil free
vacuum and helium pumps,pressure gauges,gas
flow meters and vacuum assembly 10/03
14Mechanical ground support equipment MGSE ctd.
- PACS FPU class 1000
- transportation container
- with shock absorber,
- shock and tilt indicators,
- venting ports
- design complete,
- manufacturing starts
- 11/03