Further Investigation of Spectral Temperature Feedbacks. Drew E. Kornreich TSA-7, M S F609

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LA URApproved for public release; d/strfbution is unlimited. Title: Author@): Submitted to Further Investigation of Spectral Temperature Feedbacks Drew E. Kornreich TSA7, M S F609 Transactions of the American Nuclear Society f o r the Nov. 1997 Meeting 19980330 017 Los Alamos NATIONAL LABORATORY Las Alamos National Laboratory, an affirmativeaction/equal opportunity employer, is operated by the University of California for the US. Department of Energy under contract W7405ENG36. By acceptance of this article, the publisher recognizes that the U.S. Government retains a nonexclusive, royaltyfree license to publish or reproduce the published form of this contribution, or to allow others to do so, for U S. Government purposes. Los Alamos National W r a t o r y requests that the publisher identify this article as wofk performed under the auspices of the U S. Department of Energy. The Las Alamos National Laboratoly strongly supports academic f r e m and a researcher s right to publish; as an institution, however, the Laboratory does not endorse the viewpoint of a publication or guarantee its technical correctness.

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FURTHER INVESTIGATION OF SPECTRAL TEMPERATURE FEEDBACKS Drew E. Kornreich TSA7, MS F609 Los Alamos National Laboratory Los Alamos, New Mexico 87545 INTRODUCTION A renewed interest in the phenomenon of possible positive temperature reactivity feedback coefficients in dilute fissile solutions has occurred over the past ten years.. Examination of the geologic disposal of fissile materials often includes the study of the possibility of autocatalytic reactions (those with positive feedback coefficients of reactivity) as the result of the different effective multiplications for fissile material in wet and dry ground. However, another postulated autocatalytic reaction occurs for dilute solutions of plutonium. Such solutions have been seen, through calculations, to have positive temperature reactivity feedback coefficent~.~.~ Including a non llv neutron poison like gadolinium enhances the effect (although larger feedback coefficients are unimportant if criticality cannot be achieved). This paper serves two purposes: (1) to introduce some new calculations of the temperature coefficients for uranium solutions, and (2) to examine some simplified calculations based on earlier work.4 Uranium solutions, while never having positive temperature coefficients, show trends in the feedback coefficient as a function of solution concentration that are similar to those seen for plutonium solutions. For both the plutonium and uranium solutions, the feedback coefficient experiences a local minimum near the overlunder moderation transition point. The earlier work on the simplified calculations is expanded to include better treatment of cross sections and to include strict numerical integration techniques.

BACKGROUND The temperature coefficient of reactivity feedback has essentially two components, the feedback from density changes as a function of temperature and the feedback from changes in the thermal neutron spectrum that result from temperature changes. The latter effect is the result of the energydependent cross sections for neutron interactions; as the thermal neutron spectrum is altered by changes in the macroscopic temperature of the system, different nuclear interaction cross sections are encountered by the neutrons. This causes increases or decreases in the fission and parasitic absorption rates, which directly translates to a reactivity feedback mechanism. The change in reactivity, R, as a function of temperature is given formally by The first term in Eq. (1) describes the (geometrydependent) reactivity feedback as a result of density changes as a function of temperature, and the second term in Eq. (1) describes the (materialdependent) reactivity feedback that results from neutron spectral shifts as a function of temperature. It is this second term that is of interest in this paper. If the system contains large amounts of hydrogen, then the neutron spectrum will be very thermalized. If the thermal flux can be approximated by a Maxwellian distribution, then the thermal neutron flux is given by where C is a constant and k is Boltzmann s constant. Using the standard four factor formula definitions for a thermal system ( E = 1,p = l), the reactivity, which is defined as usual as (kl)/k, is 2

R = I 1 1 loet loet C ~ eed b l ( Tn ~, Ea (E> d~ em(e,tn)vxjte> (3) where ET is the upper limit of the thermal region (assumed to be 0.4 ev) and the usual definitions of the macroscopic cross sections are used. Eq. (3) clearly exhibits the temperature dependence of the reactivity. Differentiating Eq. (3) with respect to the neutron temperature yields the spectral temperature feedback coefficient as with Z(X) = and Z (C) = loet de c ( E )E ee kg loet de z ( E ) E ~ ~ ~ ~ Eqs. (4)and (5) allow for a simplified analysis that can be performed to estimate the spectral reactivity feedback coefficient in dilute solutions of fissile material. RESULTS A simple algorithm has been constructed to perform the calculations implied by Eqs. (4)and (5). The microscopic cross sections are fit to appropriately defined curves based on experimental data up to 0.4 ev (ET). Integrals were evaluated using Romberg integration5 or iterative GaussLegendre quadrature, where successively larger quadrature orders are used until two or more calculated values of the integral are within a prescribed tolerance. 3

The spectral temperature coefficient is essentially a property of the material: however. the critical assemblies are of finite size. The effects of density changes in a finite geometry can be included in a total temperature coefficient calculation for a critical system by first estimating the radius of the critical system using standard onegroup theory.6 This would yield a total temperature coefficient of reactivity. Several calculations have been performed to determine the accuracy of the aforementioned treatment. First, the infinitemedium effective multiplication is easily determined using Eq. (3). A comparison of the simplified treatment discussed here to a detailed 69group calculation using DANTSYS is shown in Figure 1. At small concentrations, the agreement is close, but as the concentration increases, results from the two methods diverge. The inability of the simplified model to treat the effects of over and undermoderation is the most likely explanation, and is readily visible when the infinite multiplication factors for the two models are compared. Also, the spectral temperature coefficient is not independent of the geometry, as the critical and infinitemedium 69group calculations indicate. 4

REFERENCES 1. W. E. KASTENBERG, et al., Considerations of Autocatalytic Criticality of Fissile Materials in Geologic Repositories, Nuclear Technology, 115, 298 (1996). 2. C. D. BOWMAN, and F. VENNERI, Underground Supercriticality from Plutonium and Other Fissile Material, Science & Global Security, 5, 279 (1996). 3. D. E. KORNREICH, Reactivity Feedback Mechanisms in Aqueous Fissile Solutions, Nuclear Science and Engineering, 115, 50 (1993). 4. T. SUZAKI, Y. MIYOSHI, and H. HIROSS, Evaluation of Temperature and Void Coefficients of Reactivity in Homogeneous Solutions Fuel Assemblies, International Seminar on Nuclear Criticality Safety, Tokyo, Japan (1987). 5. D. ZWILLINGER, Handbook ofhtegration, Boston: Jones and Bartlett Publishers, 1992. 6. J. R. LAMARSH, Introduction to Nuclear Engineering, Reading, Massachusetts: AddisonWesley Publishing Company, 1983. 7. R. E. ALCOUFFE, R. S. BAKER, F. W. BRINKLEY, D. R. MARR, R. D. O DELL, and W. F. WALTERS, DANTSYS: A Diffusion Accelerated Neutral Particle Transport Code System, Los Alamos National Laboratory, LA12969M (1995). 5

h Y \ 1.5~10~! v c c.a,.0 1.ox1o / /!~ I / 4 3 1.9 1 Group k, :1.8 i 1.7 DANT k, c a, o 0 E 8)!i c. 0 a (/> i 1.6 5.0~10~! ; 1.5 0 : DANT Inf. Medium : 50x105 1.0~10~: 1.5~10~ 1 i : 1.2 Group Approximation. i :1.4. : 1.3 ** i i _ i_1.1 : 1 Fig. 1. The spectral temperature coefficient and multiplication factors for 69group and 1group models. 6

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