J
Feasibility Evaluation by Analytical Technique

 

By Section:
     1. Gas source mass spectrometry
         a. Noble gases
         b. Nitrogen
         c. Carbon
         d. Oxygen
                  O isotopic composition by static mass spectrometry as CO molecules
                  O isotopes by static gas source mass spectrometry of O2
                        Oxygen in gold
                        Oxygen in diamond
     2. Secondary Ion Mass Spectrometry (SIMS)
             Oxygen Isotopic Analysis by SIMS
     3. Resonance Ionization Mass Spectrometry (RIMS)
     4. Induced Radioactivity

Introduction
This document discusses the laboratory analytical techniques which will be used to analyze returned collector materials. In this section the primary emphasis is on analytical sensitivity and precision. We assume that collector materials are sufficiently pure and that these have been flown and returned without contamination. The validity of these assumptions is considered separately in Document M for bulk purity, and in the Phase A Contamination Control Plan. This Document is organized according to analytical technique. An element­by­element overview is given in Document I. The required measurement accuracy (2 standard deviations) is ±10% for elemental abundances and ±1% for isotopic abundances other than C and O, for which the desired precision is 0.4% and 0.1%, respectively.

We have identified four analytical technique categories and have mapped each of these to the specific measurement objectives, as shown in proposal Table 2-5. These four are:

  1. gas source mass spectrometry (GSMS)
  2. secondary ion mass spectrometry (SIMS)
  3. resonance ionization mass spectrometry (RIMS)
  4. induced radioactivity.
There are likely applications for synchrotron radiation X-ray fluorescence, thermal ionization mass spectrometry (TIMS), and inductively coupled plasma mass spectrometry (ICPMS) as well, but the scope of the present discussion is sufficient.

1. Gas source mass spectrometry

a. Noble gases. Measurement of noble gas elemental and isotopic abundances is one of the highest priority objectives and one of the early science return measurements. This is for the combined reasons of scientific importance and an extremely high probability of success. Collector material purity and surface contamination are not important for the noble gases, and, based on data from C. Hohenberg, extraction blanks should not be important (Hudson et al., 1981). Procedural blanks are quite low, and with detection efficiency approaching unity, meaningful measurements should be possible with 50,000 atoms of Xe or Kr. The principal analytical issue for Xe and Kr rests on the actual number of atoms implanted, not on sensitivity or contamination.

There is no problem meeting (greatly exceeding in most cases) the ±1% (2s) precision requirement except for the rarest isotopes. We discuss the worst case in detail: 126Xe. For the bulk solar wind (BSW) collectors a fluence of 126Xe of 3 x 103 atoms/cm2 is expected. To get the desired 50,000 atoms requires 17 cm2 which is quite feasible. Adopting the maximum amount of material per experiment as 100 cm2, up to 300,000 126 Xe atoms could be obtained. Using a multicollector (channelplate) detector or with the laser resonance ionization time-of-flight system demonstrated by Gilmour et al. (1993) it is possible that ±1% (1s) precision could be approached, although measurements with an actual instrument are required for a more exact estimate of precision. Gilmour et al. demonstrate the analysis of 800 Xe atoms at the counting statistics precision level. Separate extractions for the light (124-130) and heavy Xe isotopes (130-136) would probably be the best approach for a conventional magnetic sector instrument. The heavy isotope measurement would require 1 cm2 or less of collector area.

The greatest challenge occurs in measuring rare isotopes such as 126Xe for the individual regime collector materials (Phase A proposal section II.D.3.g). The science objective here is to assess the amount of fractionation between individual regimes (e.g. between coronal mass ejections, CME, and BSW). The worst case would be the CME collector material where the expected fluences could be as low as 10% of what might occur for the bulk solar wind. Taking this worst case there are only 300 126Xe atoms/cm2, which would require 170 cm2 of foil to get the 50,000 126Xe atom quota. Although possibly feasible, this exceeds our general guideline of 100 cm2 as the maximum amount of material consumed in a single measurement (constrained by upper limits in micrometeorite flux estimates; see Document N). With 100 cm2 of foil the 126Xe counting statistics standard deviation would be a few % which might be sufficiently precise depending on the magnitudes of the fractionations (CME/BSW) seen for the more abundant noble gas isotopes which would obviously be measured first. With 100 cm2 of this worst case CME collector, the 130Xe/136Xe ratio would meet the desired precision, and it is likely that this ratio would be of equal value in assessing CME/BSW fractionation as 126Xe/130Xe. In conclusion, except for the worst cases of the rarest isotope and a low CME fluence (the nominal CME fluence is 16% of BSW), it is feasible to assess fractionations among the noble gas isotopes for the different solar wind regimes.

b. Nitrogen. The expected 2 year fluence (unconcentrated) is 2x1012 atoms/cm2. The N abundance and isotopic composition will be measured by static gas mass spectrometry. Present mass spectrometric techniques (R. Pepin, I. Franchi, private communications) require 10-9 g of N for good (£1 permil) precision, using stepped heating for gas release. Because of the importance of the N isotopic data and the possibility of surface contamination, electrostatic concentration is planned (Document K). Measurement of unconcentrated solar wind would require about 20 cm2 of collector area, which is technically feasible. Because continued improvements in sensitivity with no loss in precision are expected, it is likely that the early science return N isotopic composition measurements can be done on unconcentrated samples. Pyrolysis extraction blanks at the U. of Minn. of 0.02-0.05 ng have been attained. These are almost good enough, and little effort has been put into improving these. Use of a laser desorption extraction technique is planned which should greatly reduce extraction blanks. With either combustion, pyrolysis, or laser desorption, multistep extraction procedures will be used to discriminate between surface contamination and implanted solar wind. Exact procedures are presently being worked out using isotopically labeled nitrogen (pure 14N) artificially implanted at solar wind energies. If necessary, UHV transfer capabilities can be added so that samples can be sputter cleaned, then transferred to the existing system without breaking vacuum.

c. Carbon. Both SIMS and gas source mass spectrometry appear feasible for C isotopes. CoI Pillinger uses static CO2 mass spectrometry to analyze small quantities of carbon. Currently the mass spectrometer can reproduce standards to ±0.6 permil (0.06%) on samples as small as 2 x 10-10 moles CO2, equivalent to the solar wind C in 2 cm2 of concentrator target material assuming 20X concentration, or 40 cm2 of unconcentrated solar wind. Carbon is more challenging than nitrogen because of its ubiquitous surface contamination, particularly from organic materials and adsorbed atmospheric gases. Laser heating offers the best way of reducing bulk contamination from the substrate, since it would release carbon only from the near-surface region holding the solar wind. However, the need to oxidize the carbon as it is released would make stepped heating under pure oxygen the most likely to produce quantitative yields. This would also permit good resolution of surface contamination from the trapped carbon. Oxidation extraction blanks as low as 3 x 10-11 moles C have been obtained on the present system. The extraction blank for solar wind collector analysis should be a factor of 10 lower, but this appears feasible. One of the major blank contributions for stepped combustion is the method of O2 generation, which is presently designed for high sample through-put. Alternative methods of O2 generation would clearly lead to reduced blank levels.

d. Oxygen. Both SIMS and gas source mass spectrometry techniques will be developed for O isotopes, although adequate precision and sensitivity need to be documented. The next five paragraphs are based on information and assessments by C. Pillinger and I. Franchi, who propose collecting the solar wind oxygen in a diamond matrix and using GSMS to analyze oxygen in the form of CO molecules. Following that is a proposal from M. Thiemens for analysis in the form of O2 molecules starting from either gold or diamond collectors.

Oxygen isotopic composition by static mass spectrometry as CO molecules. (Pillinger & Franchi) It is well known that meteorite families are readily distinguishable on the basis of identifiable deviations from the terrestrial fractionation line using a plot of 17O/16O vs. 18O/16O. In reality, we need to know the solar oxygen isotopic abundance to decide how the Earth, Mars and the more common meteorite parent bodies differ from the Sun because of heterogeneous accretion of silicate objects. The experience gained from meteorite studies suggests that the precision of solar wind oxygen measurements of ca. ±0.4 permil (2 sigma) is highly desirable to decide which meteorite group is closest to average solar composition; however ±1 permil permits major distinctions (compare Fig. A2, Document A) and has been adopted as the minimum required precision. These precision requirements are a very severe constraint, but nevertheless possible using static vacuum gas source mass spectrometry, provided the oxygen collected during the Genesis mission can be converted to carbon monoxide (or carbon dioxide) for measurements; oxygen itself (O2) is a difficult gas for static mass spectrometry.

For the purposes of demonstrating instrument capability we can take the example of carbon monoxide. This gas is relatively stable under static mass spectrometric conditions, certainly more suitable than carbon dioxide. It produces ions at the same masses as molecular nitrogen (28: 12C16O, 14N14N ); (29: 13C16O, 12C17O, 14N15N). The performance of the Open University static nitrogen mass spectrometer can be used to gauge that of a CO instrument. The N instrument measures 15N/14N for sample and standard gas pairs with a reproducibility of ±0.13 permil or ±0.53 permil from 0.25 nmol or 0.02 nmol of N2 gas respectively, corresponding to roughly 0.1-1.0 cm2 of concentrator target for the same amounts of CO. There is no reason to believe that a comparable instrument, specifically constructed for carbon monoxide, could not give similar results in respect of both 17O and 18O measurements. The instrument in question has a third collector so that, in addition to masses 28 and 29, the ions at mass 30 could be continuously monitored.

Using CO, there are large corrections required at mass 29 for 13C16O interference with 12C17O. These can be made acceptably small if synthetic 13C diamond is used as the collector material. 17O is now measured at mass 30 with corrections from 12C18O much smaller than the analogous situation with diamond of natural isotopic composition. Error propagation calculations were made assuming (a) diamond with 13C/12Cª10 but with the exact ratio known to 0.1 permil, (b) a detection efficiency of 10-4 (CO ions counted/solar wind O atoms extracted), (c) solar wind N and O not separated (to reduce blanks) and (d) blanks for C, N, and O are negligible. These are all reasonable assumptions and lead to a predicted precision (counting statistics standard deviation) of 0.3 permil, significantly exceeding the minimum required precision. Current best purity of 13C is 99.5%. Isotopic composition of the diamond can be accurately determined to 0.05 permil by conventional techniques. The abundance and isotopic composition of N will be accurately known from other studies. The total blank/contamination component from both CO and N2 can be measured at m/z = 28; however, the ratio of 12C16O to 14N2 needs to be determined. It may be possible to determine this by monitoring fragment ions at m/z = 12, 14, and 16, although the accuracy of this needs to be determined. It is probably better to take a small split of the total sample immediately prior to admission to the mass spectrometer (say 5-10%) with which all the CO could be readily converted over hot CuO to CO2 and then separated from the N2. Quantitative determination of the N2 and 12C16O abundances could then be made. Removal of CO and CO2 is part of the standard clean-up procedure for nitrogen measurements already, and the precision for nitrogen yield determinations is certainly <±5%. The CO2 could be measured to better than ±1%, even for the high degree of 13C enrichments. The mass spectrometer background for CO is relatively small, and could be conditioned with pure 13CO to further minimize any effects. Carbon monoxide background is worse than nitrogen, arising from outgasing of the filament; studies of different filament materials to limit background rise rate are in progress.

On the issue of the precision of O isotope measurement on small samples, preliminary experiments are encouraging. Using CO2 in the static mass spectrometer normally used for C isotopes, precisions of ±1.1 permil for 18O/16O on aliquots of 7.5 x 10-10 mol CO2 were achieved, despite the relatively unstable nature of CO2 in the mass spectrometer. This is a factor of 5000 smaller sample than is normally used for O isotopic analysis. An equivalent amount of solar wind oxygen is expected in 6 cm2 of concentrator target material with a concentration factor of ~20x. One of the main problems in this test was interference (or exchange) in the inlet of the instrument; this interference would hopefully be eliminated in a dedicated CO instrument.

In general a major difficulty in making oxygen isotope measurements would be producing CO. However, with diamond as a substrate, pyrolysis is expected to produce CO directly, although ion implanted simulations will be carried out to test the fractional release as CO and especially the effects of solar wind H in the collector materials. The concentrator will nominally reject H, but some will still get through. We envisage employing a focused laser, as this form of extraction technique offers the lowest blank levels. Diamond is fairly difficult to heat by laser light because of its transparency over a wide range of wavelengths. However, in a series of trial experiments we have used a pulsed Nd/YAG laser quadrupled to operate at 266 nm (10 mJ per 8 nsec pulse). With a 5 µm spot size, we were able to excavate substantial pits, up to 50 µm in diameter, in a diamond of known carbon isotopic composition heated in the presence of 20 mbar oxygen gas and obtain reproducible isotopic measurements.

Oxygen isotopes by static gas source mass spectrometry of O2 (Thiemens) For any isotopic analysis technique there are two primary limitations 1) The generation of sufficient beam current at the collector to produce a signal significantly above noise levels. This is crucial to provide achieve isotopic measurement precision and accuracy. 2) Development of suitable chemical extraction techniques to provide an essentially pure and unfractionated sample to the mass spectrometer inlet.

The proposed analytical protocol should achieve both of these canonical goals. Given the observed range in oxygen isotopic composition of the different meteorite classes, it must be assumed that the ability to measure d17O and d18O must significantly exceed ±1 permil in precision and accuracy. Ideally, since the observed offset between, for example, the Martian meteorites and terrestrial fractionation line is smaller than 1 per mil, a precision's of 0.5 per mil is needed to address outstanding issues in solar system evolution.

The quantity of oxygen to be analyzed (circa 3 x 10-9 moles) from the returned sample is within the range of sample size measurement ability presently attainable by static source mass spectrometry. Indeed, smaller sample analysis may be possible, or greater precision at the available sample size. Presently, oxygen isotopic analysis is done as CO2, rather than O2. This has two major drawbacks. First, unresolved chemistry is involved. The implanted atomic oxygen must be quantitatively (100%) converted to CO2 or CO. If oxygen is implanted in carbon, for example, it is known that heating releases both CO and CO2, though in variable amounts. Conversion of CO2 to CO is difficult. Oxidation of CO to CO2 introduces oxygen of possibly variable isotopic composition and is probably unacceptable.

Oxygen in gold: From rocket borne cryogenic sampling technology and studies of materials for sample collection and storage, it has been demonstrated that gold is the cleanest available surface for oxygen. The background amounts of oxygen in gold are low and characterizable. Extraction of oxygen may be done utilizing either fluorine or bromine pentafluoride. Cryogenically, bromine pentafluoride is preferred because of its higher melting point (-61.3°C) with respect to fluorine (-219.6°C). From experience with BrF5 utilized in the analysis of small samples, the P-T regime of BrF5 is ideal for cryogenic purification by multiple distillation. The blank level of oxygen in bromine pentafluoride is suitably small and characterizable. Reaction of BrF5 with gold foils possessing oxygen is ideal because a stable product, gold fluoride, is produced with complete release of molecular oxygen. The cryogenic properties of BrF5 and O2 are widely disparate and easily separated, as is routinely done for meteoritic oxygen isotopic analysis.

For mass spectrometry, the anticipated amount of oxygen to be collected is more than adequate to be analyzed by static source mass spectrometry. For example, carbon dioxide samples of this size are routinely analyzed. Analysis as molecular oxygen has the advantage that there are no isobaric corrections to be made, and a triple collector allows all three isotopes to be simultaneously measured at masses 32, 33 and 34 (16O16O, 16O17O, 16O18O), avoiding the necessity to peak jump.

A problem with nano-analysis and handling of oxygen in the past has been its slight, but significant reactivity with stainless steel, which consumes and isotopically fractionates samples in the inlet. Recently, a new proprietary electro-polishing technique has been developed by a corporation known as Quantum Mechanics, in Northern California. Stainless surfaces prepared by this technique have been demonstrated to be inert at unsurpassed levels. Tests have shown that micromolar sized samples may be stored for upwards of a year with no observed isotopic fractionation, to within 0.08 per mil for d18O. Vacuum integrity at 10-10 Torr for periods in excess of 2 years is statically maintained. The inlet and extraction system to the mass spectrometer will be treated by this technique. In addition, the flight tube and metallic optics of the source and collector may also be treated, thus lowering the background of the mass spectrometer significantly below that presently achievable.

In summary, extraction of oxygen implanted in gold, with analysis by static mass spectrometry of O2 may provide the most direct measure of the oxygen isotopic composition of solar wind oxygen. There are few unknowns or assumptions and this method provides the most feasible route for oxygen isotopic analysis at the precision required to address the relevant scientific issues in solar system and planetary science.

Oxygen in diamond: Strategy 1: When oxygen is implanted in diamond, or any carbon structure, it will be removed as CO and CO2 in variable proportions. CO cannot be oxidized with oxygen to CO2 without introduction of very significant unknown error. I would propose to thermally release and collect all CO2. The CO will then be admitted to a small chamber at controlled pressure. At pressures of less than 100 millitorr, in the presence of a discharge (platinum plates, AC current), CO is converted 100% to CO2 via CO* + CO --> CO2 + C. CO* is an electronically excited state, in this case a singlet pi state. This makes the reaction so favorable and fast because it is not spin forbidden. (This reaction has been run in less than 3 minutes. It has 100% yield and is background free. I checked my lab notes as I had used a similar reaction in experiments I did while on sabbatical in Goettingen at the Institut for physical chemistry. The carbon is removed during the reaction as elemental carbon on the electrode; which may be subsequently oxidized and removed prior to the next sample analysis.) The CO2 from the CO disproportionation reaction is then combined with the CO2 from the foil thermolysis and you have 100% yield. 13C diamond is not required because the product CO2 is then admitted to a micro nickel/monel chamber for fluorination. At 837 degrees the reaction will run to 100% completion, to CF4 and O2. To keep blanks down, the fluorine is generated from K2NiF6:KF. Heating of this salt at 400 degrees yields pure fluorine and no oxygen. Following reaction, the CF4 and O2 may be separated using a helium cryostat and temperature programming. At the proper interface of the P-T regime, the O2 is separated quantitatively, and unfractionated. We have done a similar procedure on our really small rocket collected samples. The pure O2 may be then directly admitted to the static mass spectrometer.

Strategy 2: In this case, the diamond is directly fluorinated. The products will be CF4 and O2, which are difficult to separate. In this case, two passes through a helium cryostat can be used. According to the P-T curves, the CF4, while in great excess, may be reduced by 3 orders of magnitude at liquid nitrogen temperature making the final purification more tractable. The final passes through the cryogenic system then, with proper temperature programming yields pure O2. This strategy has unknowns in that the yields of CF4 are not known, but these are determinable experimentally.

2. Secondary Ion Mass Spectrometry (SIMS)

SIMS uses a primary beam of 5-20 keV ions, usually either Cs+, O2+, or O-, to sputter material from the surface to be analyzed. Of the material removed, a fraction, typically 10-2 to 10-4, of the atoms comes off as singly-charged ions, which can be accelerated into a mass spectrometer section. The advantages of SIMS are a) relatively good sensitivity for a wide range of elements, b) a surface analysis technique with excellent depth resolution (~20 nm), and c) small analysis areas required (see Zinner, 1983, 1989, or Shimizu and Hart, 1982 for overviews). Items b) and c) minimize problems due to materials purity and surface contamination, since SIMS can essentially analyze only the portion of the collector containing the solar wind to the exclusion of both surface and bulk contamination. Analysis of small areas also allows areas of possible micrometeorite contamination ( Document N) to be avoided.

The ion yields for individual elements vary widely depending on the substrate and primary ion beam. Approximate ion yields for different elements relative to Si are summarized in Table J1 (e.g., Novak and Wilson, 1990). Positive ions are generated by an O- primary beam, and negative ions by a Cs+ primary. The highest positive yields are generally given by elements on the left side of the Periodic Table, while the highest negative yields are from the right side, just to the left of the noble gases. These electronegative elements are poorly measured by RIMS (Section 3 below). Using these efficiencies, calculated SIMS detection limits have been plotted in Fig. J1, alongside expected solar wind values, assuming that relative solar wind abundances are approximately represented by the solar system abundances of Anders and Grevesse (1989; primarily from CI chondrites). It appears possible with present techniques to measure elemental abundances to 10% or better for all elements lighter than Nb with the exception of As, Be, N, and the noble gases (not shown on Fig. J1). Among heavier elements it should be possible to determine Mo, I, and Ba, the latter two of which are key elements (Document C).

 

Table J1: Relative Ion Yields, Si=1

YIELDS OF POSITIVE IONS
O- bombardment
YIELDS OF NEGATIVE IONS
Cs+ bombardment (X- or XO-)
10+Ca,Li,Na,K,Rb,Sr,Cs 10+F,Cl,Br,I
5Ti,Ba 5O,S
2B,Mg,Al,V,Cr,Ga,In,Mo,Ru           1Si,C,H
1Si,Be,Mn,Zr,Nb,Rh 0.1B,As,Se,Ir,Pt,Au
0.5Fe,Re 0.02Be,N,Ge,Te,TaH,Os
0.2Co,Pd,Hf,Ta,W,Os 0.01Al,V,Nb
0.1Ni,Cu,Ge 0.005P,Mg,Ni,Cu,Sb,W,Th
0.05Th,P 0.002Ti,Co,Rh,Ag,Sn
0.02Zn,As,Sn,In,Ir,Pb 0.001Cr,Fe,Ru,Bi
0.01H,Ag 0.0005Mn,Ca,Pb
0.005Se,Sb,Bi 0.0002Mo,Ta,Re
0.002C,Cd,Te,Hg <0.0001 Zn,Ga,In,Zr,Cd,Hf,Hg,Ba
0.001O,Pt   
0.0005S   
<0.0001 N,Au   



Fig. J1 Comparison of estimated SIMS detection limits (in parts per 1012) with expected solar wind abundances for elements Li-Ce

These estimates assume a background count rate of 10-2 /sec for all masses, a sputtering rate of 3 x 1012 atoms/sec, and a Si detection efficiency of 10-3. These parameters may be slightly optimistic. The calculations also assume that instrumental background does not contribute to the background. For volatile species such as oxygen and halogens, instrumental background due to re-adsorption on the sample surface during analysis is by far the largest limitation to detection. However, this is not an issue for non-volatile elements. For elements lighter than Cu, much better than 10% precision may be possible, and measurement of the isotopic abundances of major isotopes to better than 1% might be possible, especially for Mg and Si.

The sensitivity is available to measure C isotope ratios. O is discussed as a special case below. The Rb isotopic abundance may be measurable at the 1-2% level, although cm2 of collector areas would be required. If the solar wind Li/Si ratio is similar to the chondritic value, the Li isotopic composition can be precisely measured. Even if Li is depleted by the factor of 50 suggested by the photospheric Li abundance, by using the concentrator target material it should still be possible to distinguish between spallation (7Li/6Li = 2) and the terrestrial ratio of 12.5. It may not be possible to distinguish higher ratios expected on the basis of preferential 6Li destruction.

This discussion has so far not considered the issue of interferences. During SIMS analysis, molecular clusters and multiply-charged ions cause numerous interferences at multiples and fractions of the abundant species. A Si wafer was analyzed (courtesy of Charles Evans & Assoc.) over the 1-200 amu mass range using an O- beam without energy filtering and at low mass resolution, illustrating the ubiquity of interferences produced by this substrate. A large number of molecular interferences were observed, including SiO, Si2, SiO2, Si2O, SiO3, Si3, Si2O2, SiO4, etc. Molecular clusters tend to have a significantly higher mass than the single atoms of equivalent mass number. Implanted H will also tend to form hydride species. Using present SIMS instruments, most molecular species for A < 60 can be adequately resolved from atoms by analysis at higher mass resolution. In addition, suppression of the molecular interferences can be done by energy filtering; however the accompanying losses in sensitivity probably would not be acceptable for solar wind collector analysis. In many cases mass resolution of M/DM = several thousand may be sufficient to resolve molecular interferences. The most recent SIMS instruments, such as the Cameca 1270 at UCLA and the SHRIMP presently being installed at Stanford, achieve resolutions up to 6,000 with no loss in sensitivity. At this mass resolution, such an instrument also has up to fifty times higher transmission than the older Cameca 3F models. A major goal of the SIMS portion of our work is thus to determine experimental detection limits for elements with molecular ion interferences as a function of instrument mass resolving power for both Ge and Si substrates. Rb, Sr and Ba are the most important elements to test, since Si (and Ge) substrates will have interferences with the O- primary beam needed for their measurement. We presently have Rb implanted samples waiting to be analyzed on the UCLA Cameca 1270 SIMS instrument for this purpose.

Regardless of these advances, collector materials for SIMS analysis need to be chosen which will give the fewest possible interferences in the mass ranges to be studied. In general, substrates of higher atomic mass will give fewer interference peaks, since most of the interference is from ion clusters, while multiply-charged ions are relatively rare. For this reason, Ge is a better substrate than Si for SIMS analysis. In addition, a 133Cs+ primary will give much fewer interferences than a 16O- sputtering beam. Interferences from Ge, Cs, and their clusters are limited to masses 70-76, 133, and 140-152. Another potential substrate of even higher mass is Au foil, which, with a Cs beam, would have no interferences but for Au and Cs themselves. Since both elements are monoisotopic with odd mass numbers, double and even multiply-charged ions would not interfere at integer mass numbers. In Phase B a substantial effort will go into evaluating exactly which substrates can and cannot be used for each element based on analyses of ion implanted samples, including samples loaded with H.

O isotopic analysis by SIMS is not limited by sensitivity but by the presence of instrumental background due to adsorbed constituents from the residual gases, primarily CO, of the instrument vacuum system. For the common Cameca 3F instrument we measured apparent O concentrations of the order of thousands of atomic ppm (ppma) on high purity Au and Pt, where for comparison the concentrator target is expected to have about 600 ppma O in the outer 100 nm. With the state-of-the-art Cameca 1270 instrument at UCLA we measured much lower apparent concentrations on the same materials, down to 1 ppma for a single crystal Au sample, presumably reflecting the much better vacuum of the 1270. However, in achieving the lower detection limits very high primary Cs ion beam currents were used in order to rapidly clean the sample surface. With this approach, the sputter rates were such that the entire solar wind O profile would be sputtered away in seconds. Such rapid data acquisition is possible in principle with a multicollector instrument, but it is far better to see the profile develop on a time scale compatible with human comprehension. What is needed for O isotopic analysis of collector materials is an instrument with a means of removing adsorbed gas layers independently of the SIMS primary ion beam. A variety of techniques are possible but two are mentioned here. One is simply to heat the sample before and during analysis. A temperature of 100-200o C may be sufficient to reduce adsorption by several orders of magnitude. A second promising technique is to use an infrared laser tuned to the primary vibrational frequency of CO. In collaboration with Charles Evans and Assoc. we propose to test these schemes on one of their existing SIMS instruments measuring the factors by which O surface contamination is decreased. For actual collector material analysis, we propose that an advanced instrument be built which will have ultra-high vacuum, a surface desorption system, and at least 3 isotope multicollector detector capabilities.

Mass fractionation corrections are necessary for SIMS isotopic analyses. Transient fractionation is a special case of fractionation which occurs until a sputtering steady state is achieved, only affects at most the outer ~10 nm and can be at least partially accounted for by calibration experiments. The bulk of the solar wind is implanted to depths of ~50 nm, and very little solar wind should be affected by transient fractionation in the outer 5-10 nm for substrates such as Si and Ge. Even when steady state is achieved, there is still a mass fractionation which is both element and substrate specific, so that calibrations must be made on the same element with a standard of similar composition to the substrate to be analyzed. For O, implantation is the best way to produce standards which can be calibrated precisely by other analytical techniques, such as dynamic mass spectrometry. A major Phase C effort will be made to demonstrate that a suitable oxygen isotope standard can be produced. Implanting a sufficient quantity of oxygen for conventional gas mass spectrometric analyses may require several cm2 of material, since the dosage must be kept low enough to avoid radiation damage and resulting diffusive losses. However, many ion implantation facilities, e.g. the one we have used at Hughes, Malibu, scan the ion beam to produce implants with a high degree of uniformity over areas of many cm2. Thus, although separate 18O and 16O implants are required, it should be possible to produce high dose ion implants with a uniform 18O/16O ratio, which will then be calibrated by GSMS. Because SIMS can analyze submillimeter spots, the isotopic uniformity of the implant can readily be checked.

One of the recent developments in commercial SIMS instruments promises a significant advantage for solar wind analysis. Typically SIMS analyses consist of a single spot of up to ~100 microns diameter where the primary beam excavates target material for analysis. Since the solar wind fluence is very low, analyses of many such spots would be required to acquire a sufficient number of counts for the desired statistical accuracy. For 17O this is true even in a concentrated sample of the solar wind. For example, with a concentration factor of ~40--near the center of the concentrator target--with a SIMS primary beam size of 100 µm, the combined statistics from ~50 spots would be needed to achieve the desired two-sigma uncertainty of 0.1%. A dynamic transfer optics (DTO) package enables the analysis of a much larger area (~500 µm square) by rastering the primary beam and tailoring the optics so the area from which ions are extracted coincides with the beam location at any given time. This technique could drastically cut the number of SIMS analyses required for the solar wind and improve the quality of analyses. Rather than 50 analysis spots, the 0.1% precision could be achieved with only 2-3 analysis spots. The result could be further constrained by additional analysis spots. The DTO feature is available for testing on several nearby SIMS instruments, including UCLA and Livermore. The value of DTO for volatile elements such as O is coupled to the workability of an independent means of surface desorption as discussed above because the outer margins of the rastered primary beam are presumably the source of most of the instrumental background.

3. Resonance Ionization Mass Spectrometry (RIMS)

Resonance ionization mass spectrometry is a relatively new technique which has only been used for materials analysis in the last decade. The basic idea is to use laser beams to pump atoms of the desired element to an excited state. From there they can be easily ionized by one or more additional photons. Since the intermediate resonant state is unique to the given element, only atoms of the selected element will be ionized, eliminating interfering isobars. A second advantage of RIMS is its high ionization efficiency. RIMS has the possibility of ionizing within the ballpark of 100% efficiency. In practice, ion extraction geometry and timing considerations associated with beam pulsing (used to reduce secondary ion background) and incomplete transmission by the mass analyzer result in detection efficiencies of 1-20%. However, this is a great improvement over SIMS where at best 0.1% is achieved. These two features--elimination of interferences and high ionization efficiency--make RIMS extremely attractive for low-level detection such as is needed for solar wind analysis.

Isotopic analysis of a given element is complicated by even-odd isotopic selectivity (e.g., Spiegel, 1994, Wunderlich et al., 1992). Nonlinear mass discriminations of up to 50% can occur (e.g., Spiegel et al., 1991; Wunderlich et al., 1992). At present, gross isotopic differences can be detected with corrections for both linear and non-linear mass fractionations by the use of standards. Further work is being done by a number of groups to study the problem of isotopic selectivity (e.g., Whitten and Ramsey, 1990; Wunderlich et al., 1992), while some isotopic studies are already being carried out by RIMS (e.g., Spiegel et al., 1992; Ma et al., 1995; Nicolussi et al., submitted). If this problem can be overcome, RIMS would be capable of providing solar wind isotope ratios for nearly all of the elements lighter than and including Zn; however, our emphasis at present is on the use of RIMS for elemental analysis.

Because of the uniqueness of the energy levels of a given element, each element must be analyzed by a different ionization scheme. The feasibility of ionizing a specific element depends on 1) the energy level of the first excited state, 2) the quantal character of accessible lower-lying states, and 3) the magnitude of the ionization potential (Hurst et al., 1978). A few elements, namely He, Ne, Ar, and F, do not have low enough first excited states, or the transition from the ground state to the lowest excited state is forbidden by quantum mechanical selection rules. For a number of other elements the ionization potential is high enough to require three steps. This is generally true of elements with ionization levels above ~10 eV since tunable dye lasers, most commonly used for RIMS experiments, operate over most of the range of wavelengths corresponding to ~1.6-5.7 eV with frequency doubling (e.g., Hurst et al., 1978). There are numerous schemes for achieving ionization, some of which can use the same wavelength for more than one step, reducing the number of laser beams required.


Fig. J2 RIMS Ionization Schemes; vertical axis represents energy

 
Fig. J2 gives a schematic illustration of some of the different paths to ionization. Scheme 1 shows single photon non-resonant ionization. Any element with an ionization potential less than the photon energy (represented by the length of the arrow) will be non-resonantly ionized. Scheme 2 shows resonant ionization in which two different photons of the same color are used to boost the atom first to an intermediate excited state and from there into the ionization continuum. Since photons of this color are too low in energy to ionize atoms directly, and the resonance level is unique to the desired element, only atoms of the desired element are ionized. Two different wavelengths can also be used in the same way, as shown in scheme 3. Three-step resonant ionizations are shown in schemes 4 and 5. In scheme 4 one of the first two colors is used for the third step, while in scheme 5 all three photon inputs are from different lasers.

Atoms must be removed from the sample surface to be ionized by the laser. Two techniques have been used: (a) sputtering and (b) laser ablation. Both have excellent depth resolution optimizing the ability to distinguish surface contamination from implanted solar wind.

With an ion beam as a sputter source using the SARISA IV instrument at Argonne National Laboratory, we have made a first-order estimate as to which elements can presently be analyzed by RIMS. These estimates are based on measured backgrounds and sensitivity from a three-color RIMS analysis of Zr in Si (Hansen et al., 1996). In Fig. J3 we compare the estimated detection limits with the calculated solar wind concentrations from a two-year exposure averaged over the top 100 nm. The RIMS detection limits (signal/noise = 3) were calculated using 5 x 105 pulses, a Zr sensitivity of ~3 ppm/count/pulse (useful yield = 1.5%), and the measured backgrounds at the respective masses. Allowing for future instrument improvements, assuming this sensitivity for all elements should be conservative. The backgrounds were measured with lasers set for Zr while sputtering a Si substrate; however, these backgrounds should be reliable for other elements, assuming the same substrate, because the background was dominated (>90%) by non-photoion sources.


Fig. J3 Comparison of SARISA RIMS detection limits with expected solar wind abundances.

Also included in Fig. J3 are two estimates of detection limits that assume improvements to the present instrument. The solid line predicts what the detection limits would be if a high-current ion source (100ľA) was installed in the present instrument and if the resolution of the present mass spectrometer of SARISA IV was increased by a factor of ten. Both these improvements are possible with current technology, and so, the solid line is our best estimate of the detection limits for today's state-of-the-art RIMS instrument. In fact, if noise does not rise linearly with increased current, detection limits may even be below the solid line. The dashed line predicts the detection limits that could be reasonably anticipated in the future when laser repetition rates increase to the point that larger numbers of averages (108 pulses) are achievable in a reasonable time frame (a few hours). This is also a conservative estimate since laser technology is improving continually and no other improvements from the present state-of-the-art instrument have been incorporated into this estimate.

Detection limits published in the literature appear to be consistent with our predictions. Ma et al. (1991) report a two-color detection limit of 50 ppt for Ru, while Pappas et al. (1989) gave a 9 ppt detection limit for In. The two-color Ru detection limit is consistent with the detection limit in our three-color set-up, probably because photoions do not contribute to the background in thie mass range. The In detection limit is significantly lower, as expected, since a much larger ion gun was used (50 µA instead of 2 µA). If one accounts for the increase in sensitivity due to the larger ion current, the In results also appear to agree with our estimates in Fig. J3. The detection limit for 56Fe of 20ppt (Pellin et al., 1988), where a three-color ionization scheme was used, is nearly the same as our prediction in Fig. J3, indicative that non-photoion background is minimal.

Comparison of Figs. J1 and J3 is somewhat unfair, since the SIMS detection limits (Fig. J1) are theoretical based on the latest commercial instrument, while the RIMS detection limits (Fig. J3) are experimental, obtained from what is no longer considered a state-of-the-art instrument. (Note also that Fig. J3 does not contain the abundant, more easily analyzed, elements below mass 50 and does contain the low abundance nuclei in the mass 100-120 mass range). Fig. J3 represents the SARISA IV instrument operating in its simplest configuration, and although improvements of 10-1000 in detection limit are required for solar wind analysis, such factors are possible. The principal reasons why RIMS detection limits were not lower are: (a) a relatively low analysis rate, and especially (b) higher general background levels than SIMS. There are a variety of options for major improvements in both factors, as discussed below.

(a) RIMS is a relatively efficient atom counter when compared to other beam techniques due to its high ionization efficiency. From our recent study (Hansen et al., 1996) where Zr was measured in Si, assuming a sputtering current of 3 ľA, a Si sputtering yield of 1.5, and a pulse duration of 800 ns, 4500 Zr atoms were sputtered from the target during 105 pulses (about an hour with present lasers). A total of 75 counts were detected in the Zr mass region, 68 above background, giving a detection efficiency of 1.5%. The efficiency is much higher than SIMS, but the total number of counts is low. Since the efficiency is within a factor of 3-5 of the best that could be expected, improvements in the detection limit are unlikely by increases in detection efficiency are unlikely. However, negligible sample is consumed for the analysis conditions just described. Thus, our measured detection limits are, in part, rate- or time-limited rather than sample-limited. Two options available for increasing the number of counts detected are to either increase the amount of material desorbed per pulse or to improve the duty cycle. As demonstrated by Pappas et al (1989), detection limits can be improved by a higher primary ion fluence because the signal is proportional to the primary ion current. Signal counting rates are also heavily influenced by laser duty cycle, and it is likely that laser duty cycles will increase substantially in the next few years. From these two improvements much higher counting rates, and thus improved detection limits, can be obtained as shown by the solid and dashed lines in Fig. J3. Any improvements beyond this will be dependent upon reducing background levels.

(b) Background sources can be grouped into roughly four categories. These are 1) background signal due to secondary ions, 2) background signal dependent on laser light, 3) detector dark current, and 4) instrumental contamination. We will examine each of these in turn, but #3 is much less important.

1) Secondary ions as a source of background come from two sources. Secondary ions directly produced during the sputtering process is the present major source of noise (70% or the total). These are suppressed in SARISA by maintaining a high electric potential on the target during sputtering, then dropping the potential during extraction of the photoions. Secondary ions then have excess energy and do not pass the spherical energy analyzers. The rejection ratio in this method depends both on the voltage of the electrical pulse and its fall time. This past year an order of magnitude improvement in SARISA's rejection ratio was obtained by upgrading the target pulse capability from the 300 V / 100 ns fall time previously available to a 3 kV / 20 ns pulse created with new solid state high voltage switches (Behlke).

The second source background ions is scattered ions that reach the detector after several bounces via a path other than the normal ion flight path. With the recent reduction in secondary ion background in SARISA, this source of noise is now about 30% of the total noise. Since these ions reach the detector by some path other than through the mass spectrometer, it should be possible to nearly eliminate it by constructing shielding between the detector and the sample target.

2) Undesired photionization as a source of background is especially difficult to eliminate since it has the same time signature as signal. It usually arises from non-resonant ionization of higher concentration, isobaric species in the desorbing flux (often it is molecular in nature, e.g., Si2 interference with Fe). As discussed above, the use of a large number of low energy photons can dramatically reduce the background, especially from non-resonant molecular ions. The three-color resonant ionization scheme used to measure Zr and to calculate the detection limits in Fig. J3 contributes < 10% to the total background.

3) Dark counts in the detector constitute a third souce of background. After installing new microchannel plates in the detector this past year, this noise source is now <1% of the secondary ion noise. Even lower-noise detectors can be obtained.

4) Instrumental contamination comes from two sources. One important source of contamination comes from what is usually called "sample memory effects." Deposition of the element of interest on the interior walls of the chamber during previous use is the start of this process, e.g. by analysis of a high concentration target. Then, during subsequent analysis of the sample this impurity is transported onto the sample surface or into the laser beam paths. The material that composes the Faraday cup used to measure primary beam characteristics and the target material used to align and calibrate the instrument are the primary memory sources. The SARISA instrumental design has several patented features to reduce this contamination. Recent experiments on Ca in Si using the SARISA instrument have demonstrated that the memory effect caused by aligning and calibrating the instrument using a pure Ca target can be eliminated by covering over the sputter deposited Ca by extended sputtering (1 hour) of a Si target before loading the sample into the instrument. (Calaway et al. to be published). Similar work with Zr in Si has resulted in lower measured values than reported in Hansen et al. (1996). In addition, we propose to machine Faraday cups of different materials which can be inserted and removed in the same manner as a sample to reduce this contamination.

The second source of surface contamination occurs prior to sample loading. The recent calcium study and others at ANL suggest that contamination of samples during transport and loading into the SARISA IV instrument must be carefully controlled. To minimize this, we plan to add a small class 10 handling area around our sample loading cell.

In summary, background source #4 can be minimized by proper and well defined contamination avoidance procedures; background source #3 can be easily minimized with higher quality detectors; source #2 can essentially be cured by developing multi-step ionization scheme and using enough lasers to implement them. Therefore, the near term design challenge is to reduce background source #1.

Laser ablation, as an alternative to ion beam sputtering, has attractive features. Laser ablation offers control on the atom removal rate. However, as with ion sputtering, laser desorption can produce non-resonantly ionized species in greater numbers than the secondary ions from ion beams if the laser intensity is not carefully controlled. With experience it should be possible to obtain an adequate ablation rate with minimal amounts of non-resonant ionization background. Undesired resonantly-excited neutral atoms are also produced, which can contribute to the background when ionized by the lasers intended to ionize only the element of interest. Since 1995 we have had a half-time post-doctoral appointee, resident at Argonne, working specifically on improving detection limits for both the ion-initiated instrument (SARISA) and the newer CHARISMA laser desorption instrument for the eventual analyses of solar wind samples.

4. Induced Radioactivity

A variety of specific techniques has been considered in this category, but only one of the most familiar, radiochemical neutron activation analysis (RNAA), appears generally useful. The amount of radioactivity produced by reactor irradiation of the element to be analyzed is proportional to the amount present. Subsequent to irradiation, contamination is not a problem, because the radioactive nuclei analyzed do not exist naturally. Consequently, if necessary, chemical separation can be performed on the irradiated collector material to concentrate the product of interest. Contamination prior to irradiation must be avoided, however.

RNAA is generally a bulk analysis technique. But for solar wind it is necessary to analyze only the top ~100 nm rather than the whole thickness of the substrate. As mentioned above, such a separation can be done subsequent to irradiation. Fortunately, a large amount of research has gone into controlled etching of Si, although at present most efforts are directed mostly at "dry" etching techniques (gas-phase etching, ion-beam and e-beam lithography). Wet etch (e.g., Takenaka et al., 1994) is needed in our case because the etchant is what must be analyzed. While this is not expected to be a problem, experimentation will be done in Phase B to carefully quantify etch depths. A very light etch can be used to remove surface contamination with the implanted solar wind removed in the second etch.

Table J2

ELEMENTS ANALYZABLE BY NEUTRON ACTIVATION

I. Full energy peak efficiency = 50%
Collector area 1 square centimeter or less Sc,Cr,Mn,Fe,Co,Cu,Zn,Ge,Br,Rb,Ir,Au
Collector area between 1 and 10 square centimeters Ga,As,Mo,Ru,Te,Cs,Sm,Eu,Tb,Yb,Hf,Os
Collector area between 10 and 100 square centimeters Ni,Ag,Sb,Ba,La,Ce,Nd,Ho,Tm,Lu,Ta,Hg,Th

II. Full energy peak efficiency = 25%
Collector area 1 square centimeter or less Sc,Cr,Mn,Fe,Co,Cu,Zn,Ge,Ir
Collector area between 1 and 10 square centimeters As,Br,Rb,Cs,Au
Collector area between 10 and 100 square centimeters Ni,Ga,Mo,Ru,Ag,Sb,Te,Ba,Ce,Sm,Eu,Tb,Ho,Tm,Yb,Hf
Assumptions: 10% or better counting statistics; peak background, 10-4 cps or less; neutron flux 1014 / cm2-sec; irradiation to saturation activity or 30 days, whichever shorter; counting times up to 30 days; 100% radiochemical yield.

Table J2 is a summary of detectable elements (10% counting statistics error) in terms of the required collector area assuming two different detector full energy peak efficiencies. These estimates assume a thermal neutron flux of 1014 n/cm2 ­sec and optimization of gamma­ray detector shape and volume to give the assumed peak counting efficiency. A background rate under full energy peaks of 10-4 cps was assumed. For 76Ge double beta decay studies, low level Ge detector counting systems have already been built (e.g. by Battelle) that would satisfy the 25% efficiency assumption. The elements in Table J2 include some of considerable cosmochemical interest including many of the rare earth elements, especially Eu, and most of the Pt­group elements.

It should be emphasized that the estimates made in Table J2 are based on the most advanced low level counting systems proposed to date. No planetary materials analysis laboratory in any country has access to such facilities. Highly optimized irradiation and counting conditions for each element are assumed, and the usual multi-element data obtained from neutron activation analysis would not necessarily be obtained. This is only a problem from the point of view of available collector area, which, at worst, may require some prioritization of elements.

The feasibility of measuring such small numbers of atoms by neutron activation has been demonstrated by the analysis of cosmic-dust samples as small as 0.2 ng total mass (Lindstrom, 1990). A comparison of these data shows that all of the following elements had as few as or fewer atoms in at least one cosmic dust analysis than is expected in 100 cm2 of substrate with a 2-year solar wind exposure: Na, K, Sc, Cr, Fe, Co, Ni, Zn, As, Se, Ag, Sm, Ir, Au. There are several reasons why this list is shorter than in Table J2. For a number of elements the Lindstrom detection limits were well below the expected solar wind fluence, so that the solar wind analysis is feasible, but the cosmic-dust samples simply had more atoms than the solar wind. Secondly, no attempt was made to analyze elements with very short half-lives, such as Mn. Also, no chemical separations were done, so that elements which produced a high beta brehmstrahlung background, or which had overlapping or interfering gamma signals could not be analyzed. In spite of these factors, two of the elements listed in the Table J2 bottom line for 50% efficiency and four bottom line elements for 25% efficiency had measured cosmic dust atom counts lower than expected from the solar wind. Note that the comparison with IDPs is realistic in that the processed solar wind samples need not require a large volume for counting. In summary, the Lindstrom (1990) results support the list of elements estimated to be analyzable by RNAA, particularly considering the improvement of facilities between 1990 and 2004.

References

 

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