the performance of a continuous supersonic expansion discharge source

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The Performance Of A Continuous Supersonic Expansion Discharge Source Carrie A. Kauffman , Kyle N. Crabtree, Benjamin J. McCall Department of Chemistry, University of Illinois June 24th, 2010

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The Performance Of A Continuous Supersonic Expansion Discharge Source. Carrie A. Kauffman , Kyle N. Crabtree, Benjamin J. McCall Department of Chemistry, University of Illinois June 24th, 2010. Outline. 1. Motivation. 2. Source Design. 3. Results. 4. Conclusion. Motivation. Motivation. - PowerPoint PPT Presentation

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Page 1: The Performance Of A Continuous Supersonic Expansion Discharge Source

The Performance Of A Continuous Supersonic Expansion Discharge

Source

Carrie A. Kauffman, Kyle N. Crabtree, Benjamin J. McCall

Department of Chemistry, University of IllinoisJune 24th, 2010

Page 2: The Performance Of A Continuous Supersonic Expansion Discharge Source

Outline1. Motivation 2. Source Design

3. Results 4. Conclusion

Page 3: The Performance Of A Continuous Supersonic Expansion Discharge Source

Motivation

Page 4: The Performance Of A Continuous Supersonic Expansion Discharge Source

Motivation

Interstellar medium:Diffuse Molecular Clouds

Temp ~ 60 KDensity ~ 101–103 cm-3

Dense Molecular CloudsTemp ~ 20 KDensity ~ 104–106 cm-3

Page 5: The Performance Of A Continuous Supersonic Expansion Discharge Source

Sensitive Cooled Resolved Ion BEam Spectroscopy

For more on SCRIBES, please stay for RE06.

Page 6: The Performance Of A Continuous Supersonic Expansion Discharge Source

Production of Cold Molecular Ions

Trot ~ 110-180 K

Trot ~ 300+ K

Page 7: The Performance Of A Continuous Supersonic Expansion Discharge Source

Production of Cold Molecular Ions

Trot ~ 110+ K

-No spectral intensity dilution, reduced spectral congestion -> easy spectral assignment-Astrophyiscally relevant temperatures-> molecular fingerprint for astronomers

Page 8: The Performance Of A Continuous Supersonic Expansion Discharge Source

Continuous Supersonic Expansion Discharge Source

High Pressure Gas

Small Orifice Trot ≈ 5-30 K

Low Pressure

Page 9: The Performance Of A Continuous Supersonic Expansion Discharge Source

Continuous Supersonic Expansion Discharge Source

Leybold 3-Stage Pumping SystemPumping speed ~ 3600 L/s

Page 10: The Performance Of A Continuous Supersonic Expansion Discharge Source

Basic Design

Anode

Macor Spacer

Cathode

Macor Cap

Gas InputHigh Temp

Silicone O-rings

Page 11: The Performance Of A Continuous Supersonic Expansion Discharge Source

H3+

R(1,0) R(1,1)u R(2,2)l

McCall, B.J. Ph.D. Thesis, University of Chicago, 2001.

Rotational Constant:43.56 cm-3

Page 12: The Performance Of A Continuous Supersonic Expansion Discharge Source

Experimental Set-up

Page 13: The Performance Of A Continuous Supersonic Expansion Discharge Source

Source Conditions

• 2-3 bar of backing pressure

•Orifice Size: flared like a trumpet 0.5 to 4.1 mm in diameter

•Typical Chamber Pressure 200-300 mTorr

•Negative voltage applied to cathode and anode held at ground

•Current: 10-130 mA

Page 14: The Performance Of A Continuous Supersonic Expansion Discharge Source

Sample Spectra

Page 15: The Performance Of A Continuous Supersonic Expansion Discharge Source

Results

• ↑ column density with increasing discharge current.

•↑ in rotational temperature with increasing discharge current.

•Operated for over 150 hours without source failure.

Low Current Regime

Page 16: The Performance Of A Continuous Supersonic Expansion Discharge Source

Results

High Current Regime

• ↑ column density

•No change in rotational temperature

•50 hours of operation

Page 17: The Performance Of A Continuous Supersonic Expansion Discharge Source

Comparison

This Work Xu et al.1 Tom et al.2 Davis et al.3

Type of Source

Continuous nozzle

Continuous slit-jet corona

Pulse Nozzle Pulsed Slit

Rotational Temperature (K)

50-110 77 60-100 Not Reported

Ion Density (cm-3)

8 × 1010 to 2 × 1012

Not Reported 1 x 1011 5x1010

3. Davis et al. Chem. Phys. Lett. 2001, 344, 23-30.

1. Xu et al. Chem. Phys. Lett. 1995, 242 126-131.

2. Tom et al. J. Chem. Phys. 2010, 132, 081103.

Page 18: The Performance Of A Continuous Supersonic Expansion Discharge Source

Summary

• Rotational temperatures in the range of 50-110 Kelvin.

•Robust & durable design capable of operating for an extended period of time.

•Ion densities comparable to pulsed sources Increased sensitivity!

•Plans for improving this design will be tested by studying the ν1 fundamental band of HN2

+.

Page 19: The Performance Of A Continuous Supersonic Expansion Discharge Source

Acknowledgments

For more information visit the McCall Research Group at http://bjm.scs.uiuc.edu