Title: Supernova data shows an acceleration of the expansion, implying that the universe is dominated by a new Dark Energy!
1SNAP Introduction
- Supernova data shows an acceleration of the
expansion, implying that the universe is
dominated by a new Dark Energy! - Remarkable agreement between Supernovae recent
CMB.
Credit STScI
2Theoretical Questions
Would be number one on my list of things to
figure out - Edward Witten Right now, not
only for cosmology but for elementary particle
theory this is the bone in the throat - Steven
Weinberg
- What is the Nature of the dark energy?
- Largest component of our universe
- Theory proposes a number of alternatives each
with different properties we can measure. - What is the evolution and fate of the universe?
- Our main achievement in understanding dark
energy is to give it a name Michael Turner - In string theory, to get ? gt 0 but extremely
small is impossible - Ed Witten
Maybe the most fundamentally mysterious thing
in basic science - Frank Wilczek This is the
biggest embarrassment in theoretical physics -
Michael Turner
3Mission Design
- SNAP a simple dedicated experiment to study the
dark energy - Dedicated instrument, essentially no moving parts
- Mirror 2 meter aperture sensitive to light from
distant SN - Photometry with 1x 1 billion pixel mosaic
camera, high-resistivity, rad-tolerant p-type
CCDs and, HgCdTe arrays. (0.4-1.7 mm) - Integral field optical and IR spectroscopy
0.4-1.7 mm, 2x2 FOV
4Simulated SNAP data
5Ground-based measurements will reach systematic
limits
6The Time Series of Spectra is a CAT Scan of the
Supernova
7What makes the SN measurement special?Control of
systematic uncertainties
- At every moment in the explosion event, each
individual supernova is sending us a rich
stream of information about its internal physical
state.
Lightcurve Peak Brightness
Images
?M and ?L Dark Energy Properties
Redshift SN Properties
Spectra
data
analysis
physics
8From Science Goalsto Project Design
Science
- Measure ?M and ?
- Measure w and w (z)
Systematics Requirements
Statistical Requirements
- Identified and proposed systematics
- Measurements to eliminate / bound each one to
/0.02 mag
- Sufficient (2000) numbers of SNe Ia
- distributed in redshift
- out to z lt 1.7
Data Set Requirements
- Discoveries 3.8 mag before max
- Spectroscopy with S/N10 at 15 Å bins
- Near-IR spectroscopy to 1.7 ?m
Satellite / Instrumentation Requirements
- 2-meter mirror Derived requirements
- 1-square degree imager High Earth orbit
- Spectrograph High bandwidth (0.4 ?m to
1.7 ?m)
9SAGENAP (2000)
- Science review by SAGENAP of 260-page proposal,
March 2000. - DOE support commenced after SAGENAP
- Study phase (effort to develop CDR, cost,
schedule, key technologies).
10RD Review
- Recent DOE/Science RD Review (Jan 2001)
- SNAP is a science-driven project with compelling
scientific goals. - SNAP will have a unique ability to measure the
variation in the equation of state of the
universe. - We believe that it is not an overstatement to
say that the Type Ia supernova measurements will
uniquely address issues at the very heart of the
field Implications for string theory - Issues Raised at RD Review
- Look at greatly increasing the near-infrared
capabilities - Is the proposed IR spectrograph throughput
adequate? - Look at a descoped instrument complement Can the
spectroscopy be done by ground-based facilities? - Develop a calibration strategy and plan.
- Address NASA relationship
11Todays Talk Status of RD
- Science Requirements Definition
- Monte Carlo Event Generator
- Lightcurve generator and fitter
- Cosmology fitter
- SNe Modeling
- Optical Telescope
- Optical Design/Layout
- Optical Quality
- Technology
- Stray Light
- Thermal Design
- NASA IMDC/ISAL Studies
- Spacecraft Packaging
- Mass Power
- Attitude Control/Pointing
- Launch Vehicle
- Orbit
- Instrumentation
- Camera
- Survey Strategy
- CCD Detectors
- Radiation Damage
- NIR Detectors
- Spectrograph
12Tools for Requirements Definition
Monte Carlo implements detailed list of
systematics Event generator - Create an object
list with fluxes. Ingredients Supernova types,
Type Ia subclasses Galactic, host, and gray
dust Gravitational lensing Host galaxy
properties Image simulator and SN extraction -
Measure photometry, spectra from images Data
simulator - Generated calibrated light curves and
spectra S/N calculated based on observatory
parameters Calibration errors Detection
efficiency - Measure contamination of non SNe Ia
and Malmquist bias Light curve and spectrum
fitter - Simultaneously fit key parameters of SN
and dust Cosmology fitter - Determine best fit
cosmological and dark energy parameters
13Simulation Studies Suite
Modeling Theory ? To probe dark energy,
follow SN to z ? 1.5 -- optimal redshift range,
SN distribution, priors Refinement of
observational requirements space from -- SN
observations/templates rise time, line
widths/shifts, UV -- SN explosion modeling
progenitor, C/O, kinetic energy,
metallicity Study of deep, wide field surveys
-- advanced exposure time calculations --
dithering, sampling, pixel strategies Gravitationa
l lensing corrections in data analysis -- cross
correlate SNAP weak lensing map with SN
amplification -- direct fit of microlensing
amplification distribution peak and tail
14Supernova Data Sheet
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19Supernova Requirements
20Advantages of Space
21Primary Science Mission Includes
22Current Optical Configuration
Annular Field TMA Prolate ellipsoid concave
primary mirror, 2 meter diameter Hyperbolic
convex secondary mirror Flat oval 45degree
folding mirror feeds transverse rear axis Prolate
ellipsoid concave tertiary mirror Flat focal
plane Delivers lt 0.04 arcsecond FWHM geometrical
blur over annular field 1.37 sqdeg Effective
focal length 21.66m f/10.8 final focus Provides
side-mounted detector location for best detector
cooling
23OTA geometrical ray traceTMA62 configuration
Compare Airy disk 26 microns FWZ diameter at 1
micron
24OTA Technologies
- Existing technologies are suitable for SNAP
Optical Telescope Assembly - New materials, processes, test evaluation
methods are unnecessary - Mirror materials
- Corning ULE glass extensive flight history, but
expensive - Schott Zerodur glass/ceramic composite lower
cost, widely used in ground based astronomical
telescopes, higher mass optic huge industrial
base - Astrium/Boostec SiC-100 newcomer unproven in
space optics higher CTE adopted for
Herschel/FIRST in infrared - Structural materials
- M55J carbon fiber cyanate ester resin epoxy
adhesive bonds - Mirror finishing technology
- conventional grind/polish/figure using abrasives
- ion-beam figuring available from two vendors
- Mirror surface metrology
- same as other space telescopes, e.g.
cassegrains - standard interferometer setups will do the job
for SNAP - no unusual accuracy drivers have been encountered
25Lightweight ULE Mirror Fab
26OTA THERMAL
- OPTICS Build,Test, Fly Warm like Hubble !
- KEY DESIGN FEATURES
- High Earth orbit (HEO) to minimize IR Earth-glow
loads - GaAs cell - OSR striping of the (hot) solar
array panels - Front surface heat rejection OK
- Optical Solar Reflectors are back silvered
Quartz tiles (a 8, e 80) - Low emissivity silvered mirrors
- Thermal Isolation mounting and MLI blanketing
27Stray Light Baffle Design
28Optical Telescope Assembly (OTA)
TMA-62 Optical Prescription
TMA-62 LIGHT PATH- primary- secondary-
folding flat- tertiary- Giga-Cam- Spectrometer
- add PASSIVE 140K CAMERA DEWAR
29Optical Telescope Assembly (OTA)
- add SECONDARY STRUCTURE low CTE - GFRP
- add OPTICAL BENCH low CTE - GFRP
- add OPTICS COFFIN BELOW low CTE - GFRP- WITH
THREE STIFF METERING TUBES
30Optical Telescope Assembly (OTA)
- add STRAY LIGHT SECONDARY LAMPSHADE
- add STRAY LIGHT PRIMARY STOVEPIPE
- add PASSIVE GIGA-CAM RADIATOR
- add CCD FRONT END ELECTRONICS
31Optical Telescope Assembly (OTA)
- add THERMALLY ISOLATED SOLAR ARRAY PANELS
- add STRAY LIGHT BAFFLE(s)
32Optical Telescope Assembly (OTA)
- add EXTERNAL MLI THERMAL BLANKETS
33NASA GSFC/IMDC Spacecaft Packaging
Secondary Mirror and Active Mount
Optical Bench
Primary Mirror
Solar Array Wrap around, body mounted 50 OSR
50 Cells
Thermal Radiator
Sub-system electronics
Detector/Camera Assembly
Propulsion Tanks
from GSFC - IMDC study
34IMDC Baseline Configuration
- ROM MASS 700 kg (instrument) 500 kg (bus) 250
kg (hydrazine) - ROM POWER 250 w (instrument) 250 w (bus)
- MOSTLY GENERIC SUBSYSYEMS
- EPS (electrical), CDH (command data handling),
Thermal - MISSION UNIQUE SUBSYSTEMS
- ACS (attitude control), SMS (structure
mechanisms), Comm - Evolving Bus Configuration Notes
- 3-axis stabilized, 4 Reaction wheels, tactical
IRUs, no torquer bars - Sun side w/ isolated body mounted solar arrays
anti-sun side radiators - Standard Hydrazine propulsion system, 100 kg to
raise perigee, 10 kg/yr for station keeping,
100 kg for Post Mission Disposal - 2 Tbits SSR storage for imaging spectroscopy
data. (Avg. data rate 52 Mbps lossless
compression plus overhead). - High speed Ka band down link near perigee _at_ 300
Mbps to Northern Latitude ground station
(Berkeley).
35ACS Driving Requirements
- Pointing Accuracy
- Yaw Pitch 1 arc-sec (1?)
- Boresight Roll 100 arc-sec (1?)
- Attitude Knowledge
- Yaw Pitch 0.02 arc-sec (1?)
- Boresight Roll 2 arc-sec (1?)
- Jitter/Stability -Stellar (over 200 sec)
- Yaw Pitch 0.02 arc-sec (1?)
- Boresight Roll 2 arc-sec (1?)
- Sun Avoidance - VERY RELIABLE SAFE HOLD !
- Earth Avoidance (mostly in orbit choice)
- Moon Avoidance (mostly in orbit choice)
36ACS Issues and Concerns from IMDC
- Jitter
- Isolate fundamental wheel frequency through
detailed analysis from manufacturer - Must tune wheel isolators - type, size and
interface - Flexible Mode Analysis
- Require extensive analysis to avoid
control/structure resonance - Solar Wind Tipping, given the Large Baffle Cp-Cg
offset - Smaller offset will minimize thruster firing
frequency and propellant required for daily
momentum unloading (est. 30 Nms wheels) - 3? Pointing jitter values
- Use current Star tracker with a very accurate
Kalman Filter - Augment Star Tracker data with instrument data
(on focal plane guider) for fine pointing - May need to replace gyro with SKIRU-DII
- Use of Instrument guide data
- Possible mitigation by use of more sophisticated
focal plane-sensors
37Launch Vehicle Study
Atlas-EPF Delta-III Sea Launch
38Orbit Optimization
- High Earth Orbit
- Good Overall Optimization of Mission Trade-offs
- Low Earth Albedo Provides Multiple Advantages
- Minimum Thermal Change on Structure Reduces
Demand on Attitude Control - Excellent Coverage from Berkeley Groundstation
- Outside Outer Radiation Belt (elliptical 3 day -
84 of orbit) - Passive Cooling of Detectors
- Minimizes Stray Light
Chandra type highly elliptical orbit
Lunar Assist orbit
39Ground Station Coverage
Orbit perigee remains over Berkeley for 3 years
without adjustment. 6 hour ground pass over
Berkeley
40Camera Assembly
GigaCam
Shield
Heat radiator
41GigaCAM
- GigaCAM, a one billion pixel array
- Approximately 1 billion pixels
- 140 Large format CCD detectors required, 30
HgCdTe Detectors - Smaller than H.E.P. Vertex Detector (1 m2)
42Imaging Strategy
43Focal Plane Layout with Fixed Filters
44Survey Strategy
45Filter Wheel Concept
46LBNL CCD RD Status
- Goals already met
- Quantum efficiency from 350 nm to 1000 nm.
- Dark current
- Read noise
- CTE for variety of pixel sizes
- Proton radiation tolerance
- 60Co radiation tolerance
- Commercialization of fabrication process
- Active projects
- Intrapixel response
- Device thinning at commercial foundry
- Packaging for ground based observatories
- Multistage outputs
- Readout electronics specification and technology
assessment
- Future work
- Backup plans for device thinning
- Further rad hardening by defect engineering
- SNAP design optimization
- Number of pixels
- Pixel size
- Thickness
- Output MOSFET structure
- SNAP specific packaging
- Design of integrated electronics running cold
adjacent to CCDs
47High-Resistivity CCDs
- New kind of CCD developed at LBNL
- Better overall response than more costly
thinned devices in use - High-purity silicon has better radiation
tolerance for space applications - The CCDs can be abutted on all four sides
enabling very large mosaic arrays - Measured Quantum Efficiency at Lick Observatory
(R. Stover)
48LBNL SCP Group Supernova Spectrum at NOAO
49LBNL CCDs at NOAO
Science studies to date at NOAO using LBNL CCDs
- Near-earth asteroids
- Seyfert galaxy black holes
- LNBL Supernova cosmology
Cover picture taken at WIYN 3.5m with LBNL 2048 x
2048 CCD (Dumbbell Nebula, NGC 6853) New
instrument at NOAO available in shared risk mode
using LBNL CCDs Multi-Aperture Red
Spectrometer (MARS) LBNL CCDs scheduled for 37
nights during 2002A (Jan July 2002)
See September 2001 newsletter at
http//www.noao.edu
50Radiation Damage Comparison to Conventional CCDs
CTE is measured using the 55Fe X-ray method at
128 K. 13 MeV proton irradiation at LBNL 88
Cyclotron Degradation is about 1?10-13
g/MeV. SNAP will be exposed to about 1.8?107
MeV/g (solar max).
1L.Cawley, C.Hanley, WFC3 Detector
Characterization Report 1 CCD44 Radiation Test
Results, Space Telescope Science Institute
Instrument Science Report WFC3 2000-05,
Oct.2000 2 T. Hardy, R. Murowinski, M.J. Deen,
Charge transfer efficiency in proton damaged
CCDs, IEEE Trans. Nucl. Sci., 45(2), pp.
154-163, April 1998
51Dark Current Degradation
Dark current is measured with one thousand or
more second exposures. The gaussian charge
distribution in the active region of the CCD is
compared with the gaussian change distribution in
the overscan region.
208K
Fit gives expected Si bandgap, so no new dark
current sources are developing. The plateau at
right is not identified yet, but could be surface
leakage currents.
158K
52Packaging prototypes
2k x 2k back-illuminated mount. 2k x 4k mount
similar, extending along wire-bond edge.
First back-illuminated image with new mount. CCD
is engineering grade used for assembly practice.
53NIR sensors
- HgCdTe
- Working with Rockwell
- Tracking developments within WFC3
- Dark current ok
- Read noise larger than expected
- QE being addressed in a new growth of crystals
- Future activities
- Acquiring our own RSC mux in May
- Acquiring our own RSC sensor in Summer 2002
- Explore alternative technologies there may be
none.
54Shortwave HdCdTe Development
- Hubble Space Telescope Wide Field Camera 3
- WFC-3 replaces WFPC-2
- CCDs IR HgCdTe array
- Ready for flight July 2003
- 1.7 mm cut off
- 18 mm pixel
- 1024 x 1024 format
- Hawaii-1R MUX
- Dark current consistent with thermoelectric
cooling - lt 0.5 e/s at 150 K
- 0.02 e-/s at 140 K
- Expected QE 60 0.9-1.7 mm
- Individual diodes show good QE
NIC-2
WFC-3 IR
55Integral Field Unit Spectrograph Design
SNAP Design
Camera
Detector
Prism
Collimator
Slit Plane
56Mirror Slicer Stack RD
57Diffraction Analysis
Throughput better than 90.6 (reflectance
diffractionedge)
58Technology readiness and issues
- NIR sensors
- HgCdTe devices are begin developed for
WFC3 and ESO with appropriate wavelength cutoff. - Read noise and QE not yet demonstrated.
-
- CCDs
- We have demonstrated radiation hardiness
that is sufficient for the SNAP mission - Extrapolation of earlier measurements of
diffusion's effect on PSF indicates we can get to
the sub 4 micron level. Needs demonstration. - Industrialization of CCD fabrication has
produced useful devices need to demonstrate
volume - ASIC development is required.
-
- Filters we are investigating three strategies
for fixed filters. - Suspending filters above sensors
- Direct deposition of filters onto
sensors - Filter Wheel
59Technology readiness and issues
- On-board data handling
- We have opted to send all data to ground
to simplify the flight hardware and to minimize
the development of flight-worthy software. - Ka-band telemetry, and long ground
contacts are required. Goddard has validated
this approach. - Calibration
- There is an active group investigating
all aspects of calibration. -
- Pointing
- Feedback from the focal plane plus
current generation attitude control systems may
have sufficient pointing accuracy so that nothing
special needs be done with the sensors. -
- Telescope
- Thermal, stray light, mechanical
control/alignment - Software
- Data analysis pipeline architecture
60Status
- Dark Energy a subject of the recent National
Academies of Science Committee on the Physics of
the Universe (looking at the intersection of
physics and astronomy). One of eleven compelling
questions What is the Nature of the Dark
Energy? - HEPAP subpanel strong endorsement for continued
development of SNAP - APS/DPF held Snowmass meeting part of 20 year
planning process for field - resource book on SNAP science out on CDROM
- International collaboration is growing, currently
15 institutions. - 18 talk 7 posters at recent AAS meeting
61SNAP Collaboration
G. Aldering, C. Bebek, W. Carithers, S. Deustua,
W. Edwards, J. Frogel, D. Groom, S. Holland, D.
Huterer, D. Kasen, R. Knop, R. Lafever, M. Levi,
S. Loken, P. Nugent, S. Perlmutter, K. Robinson
(Lawrence Berkeley National Laboratory) E.
Commins, D. Curtis, G. Goldhaber, J. R. Graham,
S. Harris, P. Harvey, H. Heetderks, A. Kim, M.
Lampton, R. Lin, D. Pankow, C. Pennypacker, A.
Spadafora, G. F. Smoot (UC Berkeley) C. Akerlof,
D. Amidei, G. Bernstein, M. Campbell, D. Levin,
T. McKay, S. McKee, M. Schubnell, G. Tarle , A.
Tomasch (U. Michigan) P. Astier, J.F. Genat, D.
Hardin, J.- M. Levy, R. Pain, K. Schamahneche
(IN2P3) A. Baden, J. Goodman, G. Sullivan
(U.Maryland) R. Ellis, A. Refregier (CalTech) J.
Musser, S. Mufson (Indiana) A. Fruchter
(STScI) L. Bergstrom, A. Goobar (U. Stockholm) C.
Lidman (ESO) J. Rich (CEA/DAPNIA) A. Mourao
(Inst. Superior Tecnico,Lisbon)
62SNAP Reviews/Studies/Milestones
Mar 2000 SAGENAP-1 Sep 2000 NASA Structure and
Evolution of the Universe (SEU) Dec 2000 NAS/NRC
Committee on Astronomy and Astrophysics Jan
2001 DOE-HEP RD Mar 2001 DOE HEPAP Jun
2001 NASA Integrated Mission Design Center July
2001 NAS/NRC Committee on Physics of the
Universe Nov 2001 CNES (France Space Agency) Dec
2001 NASA/SEU Strategic Planning Panel Dec
2001 NASA Instrument Synthesis Analysis Lab Mar
2002 SAGENAP-2 NOW ------------------------------
------------------------------ July
2002 DOE/SC-CMSD RD (Lehman) Sept 2002 NASA/SEU
Releases Roadmap Oct 2002 CNES Review
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65Roadmap for Particle Physics
- Timelines for Selected Roadmap Projects.Approximat
e decision points - are marked in black.RD is marked in
yellow,construction in green,and - operation in blue.
66A Resource for the Science Community
67SNAP at the American Astronomical Society
Meeting, Jan. 2002
- Oral Session 111. Science with Wide Field Imaging
in Space - The Astronomical Potential of Wide-field Imaging
from Space S. Beckwith (Space Telescope Science
Institute) - Galaxy Evolution HST ACS Surveys and Beyond to
SNAP G. Illingworth (UCO/Lick, University of
California) - Studying Active Galactic Nuclei with SNAP P.S.
Osmer (OSU), P.B. Hall (Princeton/Catolica) - Distant Galaxies with Wide-Field Imagers K. M.
Lanzetta (State University of NY at Stony Brook) - Angular Clustering and the Role of Photometric
Redshifts A. Conti, A. Connolly (University of
Pittsburgh) - SNAP and Galactic Structure I. N. Reid (STScI)
- Star Formation and Starburst Galaxies in the
Infrared D. Calzetti (STScI) - Wide Field Imagers in Space and the Cluster
Forbidden Zone M. E. Donahue (STScI) - An Outer Solar System Survey Using SNAP H.F.
Levison, J.W. Parker (SwRI), B.G. Marsden (CfA) - Oral Session 116. Cosmology with SNAP
- Dark Energy or Worse S. Carroll (University of
Chicago) - The Primary Science Mission of SNAP S.
Perlmutter (Lawrence Berkeley National
Laboratory) - The Supernova Acceleration Probe mission design
and core survey T. A. McKay (University of
Michigan - Sensitivities for Future Space- and Ground-based
Surveys G. M. Bernstein (Univ. of Michigan) - Constraining the Properties of Dark Energy using
SNAP D. Huterer (Case Western Reserve
University) - Type Ia Supernovae as Distance Indicators for
Cosmology D. Branch (U. of Oklahoma) - Weak Gravitational Lensing with SNAP A.
Refregier (IoA, Cambridge), Richard Ellis
(Caltech)
68Conclusion
SNAP will provide space observations of thousands
of supernovae needed to characterize the dark
energy accelerating the expansion of the
universe and may lead to a fuller understanding
of gravity space-time.