ngst — june 19991 what will ngst be? who is involved? what will esa contribute? what will ngst do?...
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NGST — June 1999 1
NGST — June 1999
What will NGST be?Who is involved?What will ESA contribute?What will NGST do?Schedule
What happens during the next year?Then what?
Bob Fosbury, ST–ECF
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NGST — June 1999 2
NGST at a glance
8m primary mirror 0.6–10+µm wavelength range
Zodi-limited -> ~ 12µm
Diffraction-limited @ 2µm 5 year lifetime, 10 year goal Passive cooling to <50K L2 Orbit — 1.5Mkm from Earth
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NGST — June 1999 3
Who pays what? NASA part of construction
$500M (FY96)
ESA contribution before launch ~$200M (a “Flexi-mission”)
CSA contribution ~ $50M
Total, including launch, operations, grants, tech. dev., inflation…
~ $2B (ie, 1/4 HST)
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NGST — June 1999 4
The Observatory
Key document is by Bély et al. Nov. 98“Implications of the Mid-Infrared
capability for NGST”
Three options1. Near-infrared optimised2. Mid-infrared compatible3. Mid-infrared optimised
ConclusionMid-infrared compatible solution —
with passive cooling to 30K (instrument) and 40K (optics) — is preferred
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NGST — June 1999 5
Launch and orbit
The Yardstick launch configuration: 3300kgAtlas IIAS or EELV Med.
Events on the way to L2Deployment while warm~3 months to L2 halo orbit
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NGST — June 1999 6
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NGST — June 1999 7
BackgroundsRadiation from back of sunshield is critical
Sunshield temperature of 90K gives Zodi limit to ~ 12µm
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NGST — June 1999 8
The background advantage
Upper curve:Mauna Kea, 1mm water
Lower curvesZodi @ 1AU and 3AU with 50K optics
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NGST — June 1999 9
Science goals
Observe the origin & evolution of galaxies
Study structure & chemical enrichment of Universe
Study star and planet formationIn practice, these goals are
represented by the Design Reference Mission (DRM) — revised this spring by the ASWG
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NGST — June 1999 10
Science oversight
Ad hoc Science Working Group (ASWG)Team in the US with European &
Canadian participation, responsible for the DRM and the selection of instrumental capabilities. Will be replaced in ~2 years with a flight SWG
ESA Science Study Team (SST)Science oversight of ESA studies.
Contributes members to ASWG(+)
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NGST — June 1999 11
The top-ranked DRM progs.
CORECORE
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NGST — June 1999 12
ESA–NASA collaboration
Partnership concept1. HST after 20012. Europe -> NGST
NGST collaboration on ‘HST model’Instrumentation, spacecraft h/w,
operationsFinancial target $200M15% min. observing time for ESA
membersIndustrial studies to identify
potential ESA contributions
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NGST — June 1999 13
NASA funded studies
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NGST — June 1999 14
ESA-funded studiesTelescope and payload suite (750kEur)
Dornier, Alcatel, LAS, UKATC
Multi-object/Integral field spectrograph (200)
LAS, Dornier (+ Durham, ESO, Leiden, MPE)
Visible wavelength camera/spectrograph (150)
Matra-Marconi, Dornier, Leicester, MSSL, LAS, UCL, Obs. Paris
On-board data management (150)Laben, Dornier, IFC (Milan) Arcetri, LAS,
Leicester, UCD
Other spacecraft systems ESA (in house)
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Instrument studies overview
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NIR camera concept
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MIR spectrograph concept
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NIR spectrograph concept
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NGST — June 1999 20
The science instrument moduleTotal mass: ~500kgPower dissipation <~ 200mW
(~50mW per instrument)Implies serious limitations on
mechanisms, electronics and operational strategies
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NGST — June 1999 21
NGST sensitivitySensitivity of an NGST deep field (106 sec, 30% bandwidth, 10 detection
Blue: starburst of 106M_sun for 106yrRed: Older population of 108M_sun @ 1Gyr
NICMOS HDF also shown
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NGST — June 1999 22
Comparison (MIR)Imaging sensitivity of NGST in the MIR for a 1arcsec2 sourceThe SED (black) shows 1% of Arp220 @z=2
Only ALMA has similar sensitivity to such enshrouded regions
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NGST discovery spaceThe relative speed of NGST broadband, widefield imaging compared with other observatories
HST = NICMOS + ACS
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Comparison with 8m gb AO
ImagingNGST uniqueness (x100 better) for high resolution imaging for wide field (4’ x 4’) and single sources
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NGST — June 1999 25
Spectroscopy (R~1000)Moderate resolution spectroscopy comparison with gb 8m
For higher resolution spectroscopy at shorter wavelengths the comparison is very sensitive to detector dark current
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Instrument selection process
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Instrument selection process1. NASA, ESA and CSA instrument
study reportsMid-99
2. Huchra IFS/MOS committee report1 Sep 99
3. Woods Hole Exposition13–16 Sep 99
4. ASWG+ and ASWG– recommendations
1 Dec 99
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Contd.
5. Public comment on ASWG reportJan 00 AAS with deadline 21 Jan 00
6. NASA, ESA and CSA management agree on boundaries of instrument responsibility
Apr 00 — “ringfencing the AO’s”
7. ESA SPC approval of participation proposal
Before end 2001
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Current instrumental issuesMulti-object vs.
Integral Field spectroscopy‘Red-leaks’ in wide bandpass
instrumentsImplications of short wavelength
capabilityCooling requirements for MIR
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NGST — June 1999 30
Technology development
Prime contractor selection mid-2001Development Comparative Active
Telescope Testbed (DCATT)Deployable OTA (DOTA)Inflatable sunshield
ISIS — STS-107 (2000)
Controlled optics flight experimentNEXUS mission (3.6m)