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
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).
O- bombardment |
Cs+ bombardment (X- or XO-) | ||
| 10+ | Ca,Li,Na,K,Rb,Sr,Cs | 10+ | F,Cl,Br,I |
| 5 | Ti,Ba | 5 | O,S |
| 2 | B,Mg,Al,V,Cr,Ga,In,Mo,Ru | 1 | Si,C,H |
| 1 | Si,Be,Mn,Zr,Nb,Rh | 0.1 | B,As,Se,Ir,Pt,Au |
| 0.5 | Fe,Re | 0.02 | Be,N,Ge,Te,TaH,Os |
| 0.2 | Co,Pd,Hf,Ta,W,Os | 0.01 | Al,V,Nb |
| 0.1 | Ni,Cu,Ge | 0.005 | P,Mg,Ni,Cu,Sb,W,Th |
| 0.05 | Th,P | 0.002 | Ti,Co,Rh,Ag,Sn |
| 0.02 | Zn,As,Sn,In,Ir,Pb | 0.001 | Cr,Fe,Ru,Bi |
| 0.01 | H,Ag | 0.0005 | Mn,Ca,Pb |
| 0.005 | Se,Sb,Bi | 0.0002 | Mo,Ta,Re |
| 0.002 | C,Cd,Te,Hg | <0.0001 | Zn,Ga,In,Zr,Cd,Hf,Hg,Ba |
| 0.001 | O,Pt | ||
| 0.0005 | S | ||
| <0.0001 | N,Au | ||
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.
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.
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.
Fig. J1 Comparison of estimated SIMS detection limits
(in parts per 1012) with
expected solar wind abundances for elements Li-Ce
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.
Fig. J3 Comparison of SARISA RIMS detection limits
with expected solar wind abundances.
| 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 |
| 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 |
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.