SALT RSS-NIR MID-TERM REVIEW MAY 20 & 21, 2009

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SALT RSS-NIR MID-TERM REVIEW MAY 20 & 21, 2009 Functional Performance Requirements, Expected Performance and Science/Engineering Trades ANDREW SHEINIS UNIVERSITY OF WISCONSIN

FPRD OCCD defines the scientific requirements of the instrument and describes operational scenarios. These are translated into technical requirements in FPRD Controlled document signed by the Instrument PI and SALT PS All functional requirements must be testable Functional requirements are the criteria for acceptance of the instrument May 20 & 21, 2009 RSS-NIR MTR 2

Optical Field Size: 8 arcminutes linear Plate Scale: 76 microns/arcsec, 4.22 pixels/arcsec Wavelength Coverage: 0.8-1.7 um Slit Widths: 0.5-1.25 Spectral Resolution: R=7000/arcsecond in z, J or H band System sensitivity: J=20.2, H short =18.7, in 3600 s at SNR=10 Scattered Light: below 2% of total input radiation Ghost Images (focusing optics): <5e-4 at 2 from parent image Polarimetruic Sensitivity: TBD Calibration: SALT facility, PenRay lamps:ar-hg,xe,ne, Kr Increase in RMS spot radius: <10 um spectroscopic, 15 um imaging Telescope Alignment: < 1% of primary DIA on grating Focusing: L4-L5 group May 20 & 21, 2009 RSS-NIR MTR 3

Optical continued The total amount of thermal background light at the science detector must less than the intra-oh sky background at an R=7000 using one of the 3 wavelength cutoff filters. (not including dust) Throughput: of 40% at peak blaze and 28% at the edge of the order if SolGel coatings are used and 35% at peak blaze and 25% at the edge of the order if conventional AR coatings are used, including grating, dichroic and filter losses. Filters: shall have a bay of 12 filters, which will be changeable with no impact to the optical system during the daytime operations support. Coatings: All optics will have conventional dielectric AR coatings or hardened SolGel. All coatings shall be unaffected by repeated thermal cycling over the operating, storage, and transportation temperature ranges. May 20 & 21, 2009 RSS-NIR MTR 4

Detector Readnoise: RSS-NIR will employ read noise reduction techniques, to achieve an effective read noise of < 20 e. Dark Current :The RSS-NIR detector should have a dark current < 0.1 e s 1 pix 1 with a goal of < 0.01 e s 1 pix 1 Bias variations shall be less than the read noise for t= 3600 s,. Gain variations shall be less 1% for t=3600s. The detector shall be mounted such that, once adjusted, it can be removed and reinstalled without necessitating optical realignment. May 20 & 21, 2009 RSS-NIR MTR 5

Mechanical Flexure: Residual image motion < 1 pixel rms over 3600 s integration Where adequate mounting precision cannot be provided by dead reckoning, convenient means will be provided to measure the misalignment of optical components of the spectrograph under ambient conditions, and then adjust their alignment with a precision that allows the optical performance specification to be met. Where thermally induced misalignment is significant, theoretically derived compensation will be applied. Cool Down Time: The RSS-NIR cryogenic cooling system shall have the capability to cool the instrument from room temperature to operating conditions in 7.2 hours or less. The RSS-NIR Pre-Dewar cooling system shall have the capability to cool the instrument from room temperature to operating conditions in 2.5 hours or less. May 20 & 21, 2009 RSS-NIR MTR 6

Mechanical Warm Up Time: RSS-NIR shall not require more than 7.2 hours to warm up the entire instrument from operating conditions to room temperature. Thermal Stability of cryogenic Dewar: The RSS-NIR detector assembly shall have an active temperature control system providing a variable temperature to be set at the optimum temperature for the detector between 100 K and 140 K, with a stability of ± 0.1 K. Thermal Stability of Pre-Dewar: The interior volume of the Pre- Dewar in which the optical system is mounted shall have an active temperature control system providing a variable temperature to be referenced to the center of the cold work surface between -33C and - 40C with a stability of ±0.5 K. Limiting Rate of Temperature Change-cryogenic Dewar: the temperature control system shall limit the rate of change at the detector to 0.5 K per minute. May 20 & 21, 2009 RSS-NIR MTR 7

Mechanical Limiting Rate of Temperature Change-Pre-Dewar: the temperature control system shall limit the rate of change in the Pre-Dewar to 0.5 K per minute. Warming Up of the Dewar: If the thermal characteristics of RSS-NIR are such that warming up by turning off the cryo-coolers will not meet the requirement in section 6.6.2, the temperature control system shall actively heat the detector and the cold plate to speed the warming up, so that RSS-NIR meets this requirement, but the rate of change of temperature shall be limited to 0.5 K per minute. Warming Up of the Pre-Dewar : If the thermal characteristics of RSS-NIR are such that warming up by turning off the Pre-Dewar chiller will not meet the requirement in section 6.6.2, the temperature control system shall actively heat the Pre-Dewar to speed the warming up, so that RSS-NIR meets this requirement, but the rate of change of temperature shall be limited to 0.5 K per minute. May 20 & 21, 2009 RSS-NIR MTR 8

T of all optical materials 1% R coatings Grating superblaze predicted by Kolgelnik approximation Hawaii-2RG-1.7µm measured QE Beletic et al. 2008 SPIE INSTRUMENT THROUGHPUT May 20 & 21, 2009 RSS-NIR MTR 9

PERFORAMCE MODEL Instrument throughput from previous slide Telescope Primary mirror: R = 89% 4 SAC mirrors: R = 96% each Thermal backgrounds predicted by ASAP Night sky spectrum from Maunea Kea airmass = 1.5 H 2 O = 1.6 mm Δλ = 0.04 nm (R ~ 33750) Smooth to our spectral resolution and find continuum level between lines at specific wavelengths May 20 & 21, 2009 RSS-NIR MTR 10

BACKGROUNDS May 20 & 21, 2009 RSS-NIR MTR 11

LIMITING VEGA MAGNITUDES TextJ med = 20.9 H med = 20.3 J med = 20.9 H med = 20.0 R = 7000 T amb = 0 o C R = 7000 T amb = +20 o C J med = 21.3 H med = 20.8 J med = 21.3 H med = 20.6 R = 4000 T amb = 0 o C R = 4000 T amb = +20 o C May 20 & 21, 2009 RSS-NIR MTR 12

COMPARISON TO OTHER INSTRUMENTS Telesco Instrumen Resolutio pe t n A Ω N Δλ λ/δλ N obj N Δλ λ/δλ SALT RSS-NIR 4000 4.41E+04 1.12E+06 4.50E+07 RSS-NIR 7000 4.41E+04 3.95E+06 1.58E+08 Keck MOSFIRE 3270 5.09E+06 2.21E+06 9.92E+07 Subaru MOIRCS 500 5.32E+06 2.50E+05 1.00E+07 MOIRCS 1600 5.32E+06 2.56E+06 1.02E+08 Subaru FMOS 500 1.34E+08 7.03E+04 2.81E+07 FMOS 2200 1.34E+08 1.36E+06 5.45E+08 VLT X-shooter 5000 5.90E+02 2.50E+07 2.50E+07 GTC EMIR 4000 7.34E+06 1.60E+07 7.20E+08 LBT LUCIFER 10000 2.39E+06 1.38E+07 3.16E+08 LUCIFER 5000 2.39E+06 7.19E+06 1.65E+08 Magellan FIRE 6000 2.32E+02 3.65E+07 3.65E+07 FIRE 2500 1.99E+03 6.33E+06 6.33E+06 MMT ARIES 2000 3.80E+05 3.15E+06 1.89E+07 ARIES 30000 3.80E+05 2.98E+08 1.79E+09 May 20 & 21, 2009 RSS-NIR MTR 13

COMPARISON TO OTHER INSTRUMENTS P = & ' 2 R $ % ' 1 t #! " R = spectral resolution λ 2 = longest wavelength in FSR λ 1 = shortest wavelength in FSR t = time to S/N=10 Å -1 for H AB = 19.5 Telescope Instrument Resolution Time (s) P (single) P (MOS) SALT RSS-NIR 4000 652.17 6.58 263.21 RSS-NIR 7000 1125.45 6.74 269.67 Keck MOSFIRE 3270 127.52 31.36 1411.25 Subaru MOIRCS 1600 21493.27 0.21 8.27 VLT X-shooter 5000 4586.19 6.90 6.90 GTC EMIR 4000 524.93 21.17 952.50 Magellan FIRE 6000 6698.35 2.53 2.53 MMT ARIES 2000 7219.09 0.58 3.48 ARIES 30000 1846.29 23.14 138.83 May 20 & 21, 2009 RSS-NIR MTR 14

Science-Engineering Trade Wavelength,!m Cost Impact 0.85 0.90 0.95 1.00 1.05 1.10 1.15 1.20 1.25 1.30 1.35 1.40 1.45 1.50 1.55 1.60 1.65 1.70 k$ Predewar Cooling Ambient $280k -40 C $0 < -40 C $75-125k Slit Cooling T Ambient R = 7000 86% OF THE TIME 47% 7% R = 4000 100% OT THE TIME 74% 29% T Ambient - 30 C R = 7000 100% OF THE TIME 90% 41% R = 4000 100% OF THE TIME 99% 69% T Ambient - 30+ C R = 7000 100% OF THE TIME 90%+ 41%+ R = 4000 100% OF THE TIME 100% 69%+ $0 $150-200k $175-250k Cooled Collimator Ambient $0 T Ambient - 30 C DETECTOR CUTOFF LIMITED $275-375k Long Slits No coating $0 Gold Coating $150-300/ea Multi-object Slits No coating $0 Gold Coating $150-300/ea Resolution Cost Impact 500 600 700 800 900 1,000 1,500 2,000 2,500 3,000 3,500 4,000 4,500 5,000 5,500 6,000 6,500 7,000 k$ Number of Gratings 5 $0 6 $25k