ML041940257

Catawba - 07/08/04 - Letter from Susan L. Uttal to Administrative Judges Submitting Documents for Inclusion in the Proceeding'S Evidentiary Record

ML041940257
Person / Time
Site:	Catawba
Issue date:	07/08/2004
From:	Uttal S NRC/OGC
To:	Anthony Baratta, Elleman T, Austin Young Atomic Safety and Licensing Board Panel
Byrdsong A T
References
50-413-OLA, 50-414-OLA, ASLBP 03-815-03-OLA, RAS 8124
Download: ML041940257 (30)

Text

RELATED CORRESPONDENCE RAS 8124

• .F,% SEC;& UNITED STATES 4cV <NUCLEAR REGULATORY COMMISSION DOCKETED WASHINGTON, D.C. 20555-0001 USNRC July 9, 2004 (3:50PM)

July 8, 2004 OFFICE OF SECRETARY OFFICE OF THE RULEMAKINGS AND GIENERAL COUNSEL ADJUDICATIONS STAFF Ann Marshall Young, Chair Thomas S. Elleman Administrative Judge Administrative Judge Atomic Safety and Licensing Board Atomic Safety and Licensing Board U.S. Nuclear Regulatory Commission 5207 Creedmoor Rd. #101 Mail Stop: T-3F23 Raleigh, NC 27612 Washington, D.C. 20555 Anthony J. Baratta Administrative Judge Atomic Safety and Licensing Board U. S. Nuclear Regulatory Commission Mail Stop: T-3F23 Washington, D.C. 20555 In the Matter of DUKE ENERGY CORPORATION (Catawba Nuclear Station, Units 1 and 2)

Docket Nos. 50-413-OLA and 414-OLA

Dear Administrative Judges:

In accordance with the Board's Order of May 25, 2004, the Staff submits the following documents for inclusion in the instant proceeding's evidentiary record:

1. "NRC Staff Rebuttal Testimony of Dr. Ralph Landry and Dr. Ralph 0. Meyer concerning BREDL Contention I,";

2. NRC Staff's Proposed Exhibit A, Wolfgang Wiesenack e-mail to Miroslav Hrehor, "Re: Statement in one of our SEGFSM Reports," 6/14/04;

3. NRC Staff's Proposed Exhibit B, F. J. Erbacher, "Cladding Tube Deformation and Core Emergency Cooling in Loss of Coolant Accident of a Pressurized Water Reactor," NuclearEngineeringand Design, 1987, pp. 55-64; and

4. NRC Staff's Proposed Exhibit C, "Decay Heat P6wer in Light Water Reactors,"

ANS standard ANS/ANS-5.1-1994, pp.1, 2, 14, 16.

Susan Uttal Counsel for NRC Staff

Enclosures:

As stated cc with ends: Service List

July 8, 2004 UNITED STATES OF AMERICA NUCLEAR REGULATORY COMMISSION BEFORE THE ATOMIC SAFETY AND LICENSING BOARD In the Matter of )

)

DUKE ENERGY CORPORATION ) Docket Nos. 50-413-OLA

) 50-414-OLA

)

(Catawba Nuclear Station )

Units 1 and 2) )

NRC STAFF REBUTTAL TESTIMONY OF DR. RALPH LANDRY AND DR. RALPH 0. MEYER CONCERNING BREDL CONTENTION I Q1. Please state your name.

Al a. (RL) My name is Ralph Landry. I am a Senior Reactor Engineer employed by the NRC in the Office of Nuclear Reactor Regulation. A statement of my professional qualifications was attached to the NRC Staff Testimony of Undine Shoop, Dr. Ralph Landry and Dr. Ralph 0. Meyer Concerning Contention I, (Staff Prefiled Testimony),' filed July 1, 2004.

Al b. (ROM) My name is Ralph 0. Meyer. I am employed as a Senior Technical Advisor for Core Performance and Fuel Behavior in the Office of Nuclear Regulatory Research at the NRC. A statement of my professional qualifications was attached to the Staff Prefiled Testimony, filed July 1, 2004.

1 The NRC Staff submitted several proposed exhibits with the Staff Prefiled Testimony.

The Staff intends to introduce only the following portions of the documents into evidence: Exhibit 3, "LOCA Test Results for High-Burnup BWR Fuel and Cladding," Y. Yan, et al., pages 1, 17 (unpaginated); Exhibit 4, "Does M5 Balloon More Than Zircaloy-4 Under LOCA Conditions?," N.

Waeckel, et al., pages 1-2, 10; Exhibit 5, Memorandum from F. Eltawila to S. Black, "Response to User Need for Development of Radiological Source Terms for Review of Mixed Oxide Fuel Lead Test Assemblies," February 23, 2004, pages 1-2 and Attachment B, page B-5, Figure 1.

02. What is the purpose of this testimony?

A2. The purpose of this rebuttal testimony is to address the Prefiled Written Testimony of Dr. Edwin Lyman Regarding Contention I, submitted on behalf of the Blue Ridge Environmental Defense League (BREDL) on July 1, 2004.

Q3 In the answer to Question 5 of his prefiled written testimony, Dr. Lyman states that "Appendix K to Part 50...sets forth ECCS 'evaluation models', i.e. assumptions about the behavior of reactor fuel that are to be used in determining whether it complies with the criteria in 10 C.F.R. § 50.46." Is this statement correct?

A3. (RL) No, this is not a correct statement. Appendix K to 10 C.F.R. Part 50 provides the descriptions of the required and acceptable features of the evaluation models as well as the required documentation. Appendix K does not provide assumptions about the behavior of reactor fuel. The topics covered include the sources of heat during the LOCA, the swelling and rupture of the cladding and fuel rod thermal parameters, the blowdown phenomena, and the post-blowdown phenomena. These are all descriptions and specifications placed on phenomena that must be modeled by an acceptable evaluation model. The majority of the specifications provided by Appendix K deal with thermal hydraulic phenomena, that is, heat transfer and fluid flow behavior.

More specifically, only the first few paragraphs of Appendix K address matters related to fuel, such as how the decay heat is to be calculated, how stored energy is to be calculated, and how the heat from the reaction of the cladding material with the cooling water, or steam, is to be calculated. The remainder of the appendix gives specific details and requirements on how the heat removal by the coolant water is to be calculated, and how the movement of the coolant water through the reactor system is to be calculated. Thus, the majority of Appendix K provides details on how cooling of the reactor fuel is to be calculated, along with details on how the movement of the cooling water around the system is to be calculated. Only the early part of the appendix is

concerned with specifying how the amount of heat contained and produced by the fuel are to be calculated.

Q4 In his answer to Question 18 of his prefiled written testimony, Dr. Lyman states that

"...the Staff claims to have independently verified the adequacy of Duke's LOCA analysis..." Is this statement correct?

A4. (RL) No, this is not a correct statement. The staff does not claim to have performed independent analyses or calculations to verify the submittal of Duke. The staff has stated in its Safety Evaluation (SE): "Based on the NRC review of the information provided, the NRC staff concludes that the effect of four MOX LTAs has been conservatively evaluated and has been demonstrated to be in compliance with the requirements of 10 C.F.R. 50.46." That statement was based on the material submitted by Duke that was reviewed and found to be consistent with the approval the staff has granted with regard to the fuel vendor's LOCA evaluation model and effect on the LOCA analysis of record for the Catawba Nuclear Plant.

Q5. In the answer to Question 6 of his prefiled written testimony, Dr. Lyman explains why he thinks the Appendix-K evaluation models should include consideration of fuel relocation during LOCAs. He bases his explanation partly on your memorandum of February 8, 2001, and on Mr. Thadani's memorandum of June 20, 2002. Do you agree with his response?

A5. (ROM) No. Appendix K has been in effect since 1974, and over the years some extra conservatisms and some non-conservatisms have been identified. To the best of my knowledge, the NRC never contemplated including fuel relocation in Appendix K as mentioned by Dr. Lyman. However, by using Appendix K with its compensating extra conservatisms, Duke has adequately accounted for any non-conservatisms. Furthermore, based on my experience and knowledge, and as is demonstrated in my testimony, I do not agree that certain characteristics of MOX fuel exacerbate the effects of fuel relocation.

06. Inthe answer to Question 12 of his prefiled written testimony, Dr. Lyman states that "Tight bonding has also been observed at the Halden reactor in Norway to retard the rate of balloon formation." Is that statement correct?

A6. (ROM) No. Dr. Lyman accurately interprets a statement made in NEA/CSNI/R(2003)9, but the statement in that report is not correct. No ballooning tests with high burnup fuel rods have been performed at Halden as of this date, and the statement in NEANCSNI/R(2003)9 was merely a suggestion of what might happen rather than a report of what has been experimentally observed. I have verified that this statement is in error by an e-mail exchange with Dr. Wolfgang Wiesenack, who is the general manager of the Halden Project (Exhibit A,Wolfgang Wiesenack e-mail to Miroslav Hrehor, "Re: Statement in one of our SEGFSM Reports," 6/14104). Miroslav Hrehor, who is also mentioned in that e-mail, is the scientific secretary at NEA who is responsible for that report.

07. Inthe answerto Question 12 of Dr. Lyman's prefiled written testimony, he states that

'It has been confirmed that MOX fuel is more resistant to clad failures due to pellet-clad mechanical interaction (PCMI) than LEU fuel, even at high burnups." Is that observation relevant to the behavior of MOX fuel under LOCA conditions?

A7. (ROM) No. First, there is no PCMI during a LOCA. PCMI occurs when the power is increased and thermal expansion of the pellet, which is greater than that of the cladding, causes the pellet to push on the cladding. During a LOCA, power is decreased and the cladding expands faster than the pellet -- actually moving away from the pellet. More fundamentally, though, the additional resistance of MOX fuel to cladding failure by PCMI is the result of the greater plasticity of the MOX pellets. They are softer than LEU pellets. The MOX fuel pellets are thus able to deform somewhat and relax the stress they apply to the cladding. This has nothing to do with bonding between the pellets and the cladding.

Q8. In the answer to Question 12 of Dr. Lyman's prefiled written testimony, he claims that LOCA test results from the Power Burst Facility (PBF) have shown that irradiated rods experience greater deformation (swelling) than unirradiated rods. He then states that there is no way to determine whether Duke's LOCA analysis underestimates or overestimates the degree of cladding swelling. Do you agree with this conclusion?

A8. (ROM) No. As discussed by the I RSN authors in the reference cited by Dr. Lyman (Mailliat and Schwartz at 432), it would appear that the PBFtests showed an enhancement of more than a factor of 2 in balloon size for irradiated rods compared with unirradiated rods. This was said to be the result of more uniform temperatures in the irradiated rods. This is probably not an accurate interpretation of the test results. After the PBF tests were performed, more work was done on the effects of temperature uniformity at the Karlsruhe nuclear research center in Germany by F.J. Erbacher and coworkers. In a review article by Erbacher, the PBF results are discussed along with additional German test results with irradiated and unirradiated rods (Exhibit B, F. J. Erbacher, "Cladding Tube Deformation and Core Emergency Cooling in Loss of Coolant Accident of a Pressurized Water Reactor," Nuclear Engineering and Design, 1987, pp. 55-64). In Figure 2 of this paper, the PBF data are plotted along with other data, and the temperature at the time of bursting for the PBF data is seen to vary from about 800 to 1100 C. Also shown in this figure are curves that show the strong variation of balloon size associated with the temperature at the time of bursting. This well known variation in balloon size is the result of changes in the crystal structure of the cladding, which switches from an alpha-phase to a beta-phase between 800 and 1000 C. The rod that produced the largest balloon ruptured in the alpha phase just below 800 C, right at a temperature where balloon sizes are expected to be their maximum. Thus, it was probably the differences in temperature at the time of rupture of the PBF rods that produced the different balloon sizes rather than the difference in burnup. In Figure 5 of Erbacher's paper, results are shown for a substantial number of ballooning test in the same facility. No systematic difference

is seen between fresh fuel and the irradiated rods. High-burnup effects are being studied in the ongoing NRC research program to further clarify LOCA behavior, but it can be noted again that the variation in balloon sizes just discussed is not related to the use of MOX fuel pellets.

Q9. Inthe answer to Question 14 of Dr. Lyman's prefiled written testimony, he concludes that the recent Electricit6 de France (EDF) presentation at Argonne National Laboratory does not fully address the differences in the size of balloons between M5 and Zircaloy cladding. Do you agree with that statement?

A9. (ROM) I agree that the EDF presentation does not entirely address the differences in the size of balloons between M5 and Zircaloy, but it clearly shows that the large difference claimed by IRSN is a consequence of using inappropriate data. Further, Dr. Lyman's comment about spalling, or flaking of a thick oxide coating, is not relevant. To the best of my knowledge, none of the ballooning tests utilized cladding with spalled oxide, and certainly no spalling is expected in the Catawba core with its modern cladding materials (ZIRLO and M5). With regard to the size of the balloons, it should not be forgotten that ballooning is an M5 cladding issue; it is not a MOX issue. Based on my knowledge and experience, and the testimony I have given, there is no valid reason to expect that the size of the balloons will be affected by the type of fuel inside.

Although confirmatory research on M5 cladding under LOCA conditions is continuing, it is my opinion that the specific concerns raised by Dr. Lyman are not valid. The staff believes the ballooning size has been adequately accounted for in the analysis.

Q10. In the answer to Question 15 of Dr. Lyman's prefiled written testimony, he quotes an IRSN presentation as saying, "The impact of fuel relocation in fuel rod balloons ... is still fully questionable and should be addressed by specific analytical tests with a simulation of fuel relocation." Do you agree?

A10. (ROM) No. As discussed in my answer to Questions 33 and 34 of the Staff's Prefiled Testimony, the diameter of the balloons will not be different for MOX fuel and LEU fuel.

Further, the diameter of the balloons will not be affected by fuel relocation because fuel relocation would occur after the balloons are formed. Thus neither MOX fuel nor fuel relocation will affect flow blockage, which is calculated by the models used by Duke. Therefore, the Duke analysis is not incomplete and is not likely to be non-conservative.

Qi 1. Inthe answer to Question 16 of Dr. Lyman's prefiled written testimony, he points out that Duke's calculations have demonstrated a peak cladding temperature (PCT) that is higher for a MOX fuel rod than for an equivalent LEU rod inthe same position inthe core. He then concludes that the margin is therefore smaller for a MOX rod than for an LEU rod in the same position. Do you agree with that conclusion?

Al 1. (ROM) No. Duke's analysis shows a higher PCT for MOX fuel only because they used the same decay heat curve for MOX and for LEU fuel. In fact, the decay heat is lower for MOX fuel than for LEU fuel at the time of importance for LOCA (Exhibit C, "Decay Heat Power in Light Water Reactors," ANS standard ANS/ANS-5.1-1994, pp.1, 2, 14, 16). Therefore, in reality, the PCT for MOX fuel should be a little lower than the PCT for LEU fuel and the margin will not be reduced.

012. Inthe answer to Question 17 of Dr. Lyman's prefiled written testimony, he states that the only way to fully address the uncertainties associated with the behavior of high-burnup, M5-clad MOX fuel during LOCAs is to conduct integral LOCA tests of such fuel. Do you agree with that statement?

A12. (ROM) No, I do not agree that integral LOCA tests of high-burnup MOX fuel with M5 cladding are needed. The effect of plutonium on LOCA behavior is almost entirely the result of small changes in initial stored energy, fission heat, and decay heat as discussed in the Staff's prefiled testimony in answer to Questions 17, 18, and 24. These changes are well known and

adequately modeled. There has been speculation that MOX fuel would enhance the effect of fuel relocation into balloons during a LOCA, but it is my opinion that there will be no such enhancement (see answer to Question 40 in the Staff's prefiled testimony). It has also been claimed that cladding behavior will be altered by MOX fuel in comparison with LEU fuel, but I have offered testimony that shows there will be no effect of the type of fuel pellets inside on cladding behavior (see answer to Question 34 in the Staff's prefiled testimony). In my opinion, the uncertainties associated with the MOX LTAs for Catawba are adequately understood.

Q. Does this conclude your REBUTTAL testimony?

A. Yes.

UNITED STATES OF AMERICA NUCLEAR REGULATORY COMMISSION BEFORE THE ATOMIC SAFETY AND LICENSING BOARD In the Matter of )

)

DUKE ENERGY CORPORATION ) Docket Nos. 50-413-OLA

) 50-414-OLA

)

(Catawba Nuclear Station )

Units 1 and 2) )

CERTIFICATE OF SERVICE I hereby certify that copies of the "NRC STAFF REBUTTAL TESTIMONY OF DR. RALPH LANDRY AND DR. RALPH 0. MEYER CONCERNING BREDL CONTENTION 1" in the above-captioned proceeding have been served on the following by deposit in the United States mail, first class; or as indicated by an asterisk(*), by deposit in the Nuclear Regulatory Commission's internal mail system; and by e-mail as indicated by a double asterisk(**), this 8th day of July, 2004.

Ann Marshall Young, Chair * ** Office of the Secretary * **

Administrative Judge ATTN: Docketing and Service Atomic Safety and Licensing Board U.S. Nuclear Regulatory Commission Mail Stop: T-3F23 Mail Stop: 0-1 6C1 U.S. Nuclear Regulatory Commission Washington, DC 20555 Washington, DC 20555-0001 (E-mail: HEARINGDOCKET@nrc.gov)

(E-mail: AMY~nrc.gov)

Office of Commission Appellate Anthony J. Baratta * ** Adjudication

• Administrative Judge Mail Stop: 0-1 6C1 Atomic Safety and Licensing Board U.S. Nuclear Regulatory Commission Mail Stop: T-3F23 Washington, DC 20555 U.S. Nuclear Regulatory Commission Washington, DC 20555-0001 Atomic Safety and Licensing Board Panel (E-mail: AJB5@nrc.gov) Adjudicatory File

• U.S. Nuclear Regulatory Commission Thomas S. Elleman* Mail Stop: T-3F23 Administrative Judge Washington, DC 20555 Atomic Safety and Licensing Board 5207 Creedmoor Rd #101 Diane Curran, Esq. **

Raleigh, NC 27612 Harmon, Curran, Spielberg (E-mail: elleman~eos.ncsu.edu) & Eisenberg, LLP 1726 M Street, NW, Suite 600 Washington, DC 20036 (E-mail: dcurran @harmoncurran.com)

Lisa F. Vaughn, Esq ** David A. Repka, Esq. **

Legal Department Anne W. Cottingham, Esq. **

Mail Code - PB05E Mark Wetterhahn, Esq. **

Duke Energy Corporation Winston & Strawn, LLP 426 S. Church Street (EC1 X) 1400 L Street, NW Charlotte, NC 28201-1006 Washington, DC 20005-3502 (E-mail: IfVaughn@duke-energy.com) (E-mail: drepka~winston.com acotting @winston.com) 2 Susan Uttal Counsel for NRC Staff

EXHIBIT A From: Wolfgang Wiesenack <wowi@mail.hrp.no>

To: <Miroslav.HREHOR @oecd.org>, <ROM @nrc.gov>

Date: Mon, Jun 14,2004 8:03AM

Subject:

Re: Statement in one of our SEGFSM Reports

Ralph, I agree that your formulation is more precise and unambiguous. The original addition "thus restraining the rate of clad ballooning" may be seen as stating something experimentally verified or as an inference (the latter was intended).

But I also wonder what the difference would be between a 400cm and a 40cm rod.

Miroslav: I suggest to change the document accordingly.

Wolfgang

> Date: Wed, 09 Jun 2004 16:09:55 -0400

> From: "Ralph Meyer" <ROM~nrc.gov>

> To: <wolfgang.wiesenack @hrp.no>, <Miroslav.HREHOR @oecd.org>

> Cc: "Harold Scott" <HHS.twf5_po.TWFN-DO~nrc.gov>

Subject:

Statement in one of our SEGFSM Reports

> Wolfgang, Miroslav,

> On p. 79 of "Ongoing and Planned Fuel Safety Research in NEA Member States" it says:

> "Halden have carried out axial gas flow studies in fuel rods over a range of burn-up and test have shown a severe restriction in volume flow at high burn-up thus restraining the rate of clad ballooning."

> I think the last part of this statement is not correct. I know that Halden has carried out axial gas flow studies that show severe restriction in flow at high burnup, but I don't think any of these were tests with LOCA clad ballooning. Shouldn't the statement say "... thus suggesting that the rate of clad ballooning might be restrained."?

> This statement has been quoted by Lyman in the MOX hearing that is underway here.

> Ralph

> P.S. I will be away from the office until Tuesday, June 15 CC: <wolf gang.wiesenack@ hrp.no>

EXHIBIT B Nuclear Engineering and Design 103 (1987) 55-64 55 North-Holland, Amsterdam CLADDING TUBE DEFORMATION AND CORE, EMERGENCY COOLING IN A LOSS OF COOLANT ACCIDENT OF A PRESSURIZED WATER REACITOR F.J. ERBACHER Institut flr Reaktorbazuelemente, Keriforschungszenltrun Karlsruhe, Postfach 3640, D-7500 Karlsruhe, Fed Rep. Germany Received 4 November 1986 The paper summarizes the dominant effects which finally ensure the core coolability of a pressurized water reactor in a loss-of-coolant accident (LOCA).

The main results are summarized as follows:

- The cooling effect of the two-phase mixture which is intensified during reflooding increases temperature differences on the cladding tube circumference and thus limits the mean circumferential burst strains to values of about 50%.

- An unidirected flow through the fuel rod bundle during the refill and reflooding phases causes maximum cooling channel blockage of about 70%.

- The coolability of deformed fuel elements can be maintained up to flow blockages of about 90%.

All effects investigated indicate that in a LOCA no impairment of core coolability and public safety has to be expected.

1. Introduction prevented only if the emergency cooling systems, de-spite the reductions in flow sections, guarantee reliable In the licencing procedure under the Atomic Energy cooling of the fuel elements and no further major rise in Act evidence must be provided that the consequences of temperature occurs.

all conceivable pipe ruptures in the primary circuit Within the framework of safety analysis and licens-resulting in loss of coolant can be controlled. For these ing procedures, providing evidence for the following so-called loss-of-coolant accidents the double rupture of items is of particular importance: number of burst fuel a main coolant line between the main coolant pump rod cladding tubes, size of the burst circumferential and the reactor pressure vessel is presently considered strain, axial displacement of the burst points, maximum as the design basis for core emergency cooling systems. coolant channel blockage and coolability of deformed After rupture of a main coolant line the reactor is fuel elements.

shutdown automatically, even without actuation of the The research activities conducted under the Nuclear shutdown rods. But the decay heat still generated after Safety Project (PNS) by various institutes of the Karls-suspension of the chain reaction necessitates reliable ruhe Nuclear Research Center (KfK) served the primary long-term cooling of the fuel element cladding tubes. purpose of elaborating the relevant experimental and This is achieved by core emergency cooling systems theoretical fundamentals. The out-of-pile and in-pile which, after evacuation of the reactor pressure vessel, experiments started from the design data of the emer-feed into the reactor core the borated emergency cool- gency cooling systems and the fuel elements for ing water stored in accumulators and pools so as to pressurized water reactors built by Kraftwerk Union cover the reactor core again with coolant and ensure (KWU). The Zircaloy-4 cladding tubes used were in reliable long-term cooling of the fuel elements. conformity with the KWU specification; they had been However, before emergency cooling'becomes fully cold worked and stress relieved; the external diameter effective, fuel element cooling deteriorates temporarily. was 10.75 mm, the inner diameter 9.3 mm.

Zircaloy fuel rod claddings may attain temperatures at It has been proved in the COSIMA experiments that which they balloon or burst under the impact of the under realistic boundary conditions of a loss-of-coolant internal overpressure. This narrows locally the coolant accident no noticeable cladding tube deformations have channels. Further damage to the fuel elements can be to be expected in the blowdown phase [1]. Therefore, 0029-5493/87/$03.50 < Elsevier Science Publishers B.V.

(North-Holland Physics Publishing Division)

56 F.J. Erbacher/ Cladding tube deformation and core emergency cooling only the refill and reflooding phases are important for of incidents involving small leaks (small load due to deformation and coolability. differential pressure) and to take account of develop-In the following sections some of the most important ments resulting in an increase in target burnup (high results will be compiled of fuel rod and fuel element load due to differential pressure), the deformation and behavior during the refill and reflooding phases of a burst behavior was investigated for a wide pressure loss-of-coolant accident. range in single-rod experiments. However, the investiga-tions concentrated on the range of burst pressure of about 50 to 70 bar which must be supposed in a design basis accident of pressurized water reactors.

2. Deformation mechanism of Zircaloy cladding tubes The following figures show the experimental results compared with the calculated values. The calculated In order to record the consequences both of a rup- values traced as curves has been obtained with a com-ture of the main coolant line (design basis accident) and puter code developed under the REBEKA task [2].

engineering burst stress, MPa Fig. 1. Burst temperature vs. burst stress of Zircaloy claddings.

t i

F.J. Erbacher/ Cladding tube deformation and core emergency cooling 57 2.1. Burst temperature exactly, the agreement of all experimental data can be termed good. No influence of nuclear parameters on the Experimental data for the burst temperature among burst temperature has been found [4,5].

other factors provide an important basis for the number Therefore, it can be assumed that with this informa-to be determined of burst cladding tubes and for the tion the number of defective fuel rods can be de-fission product release resulting from them. termined with adequate accuracy in a loss-of-coolant Fig. 1 shows the burst temperature versus the en- accident if the temperature and pressure development gineering burst stress with the heating rate as the of the fuel rods is known. Accordingly, with the present parameter. At the same heating rate a higher rod inter- inner pressures and burnups, the-cladding tubes will fail nal pressure causes the burst temperature to become through burst when temperatures of about 8000 C are lower. The results of the REBEKA single rod tests attained.

represented as plots show a marked influence of the heating rate on the burst temperature, i.e., high heating 2.2. Burst circumferentialstrain rates lead to higher burst temperatures than low heating rates. Similar experiments performed in the FABIOLA testing facility have confirmed the relationships de- The scope of burst circumferential strain of the scribed and, moreover, have shown that fission products Zircaloy cladding tubes determines inter alia decisively simulated by iodine do not exert an influence on the the coolant channel blockage and the coolability in the deformation behavior [3]. fuel element.

The same figure shows a comparison with out-of-pile Fig. 2 shows the burst circumferential strain versus bundle tests and with various in-pile tests. Taking into the burst temperature with the heating rate as the account the differences in the experimental conditions parameter. The calculated values traced as curve de-and the difficulty of determining the burst temperature scribe the burst circumferential strains measured in 200 150 C

.4-

.2 100 U,

C_

-D C

LCU 50 E

C-

.U 0.

burst temperature (0C]

Fig. 2. Burst strain vs. burst temperature of Zircaloy claddings.

58 F.J. Erbacher/ Claddingtube deformation and core emergency cooling REBEKA single rod tests on the cladding tube cir-cumference at uniform temperature. The strain maxima at 8200C and approx. 10000C can be attributed to the superplasticity of Zircaloy [6]. They occur to a remarka-ble extent only at nearly uniform temperature on the cladding tube circumference and with symmetric defor-mation of the cladding tube. These idealized conditions were specifically provided by a heated tube in the

'U neighborhood in order to have a systematic and funda-mental experimental study performed of the deforma- 16 tion behavior in single rod experiments.

The averaged values from out-of-pile bundle tests and in-pile single rod and bundle tests entered in the figure indicate a marked reduction in the burst cir-cumferential strains to values around 50%. This limi-tation is due to temperature differences on the cladding tube circumference. Lowering of the burst circumferen-tial strain due to failure by embrittlement as a result of stress corrosion cracking has not to be expected under the boundary conditions of a loss-of-coolant accident

[7]. The measured values of out-of-pile and in-pile tests REBEKA- ' . E K E- urs ct entered in the figure do not suggest any impact of A singe ro'tes ... 1urve nuclear boundary conditions on the burst circumferen- bundle lestsl 3 tial strain.

Under representative thermohydraulic boundary

'.razimuthal claaddng .r.emnperature differences K 0 -- _ .1 i0si/_s'..

z*-

tt j;

conditions of a loss-of-coolant accident heat flows from the pellet through the gap to the cladding tube and Fig. 3. Burst strain vs. azimuthal temperature difference of coolant are clearly established in a fuel rod. Tolerances Zircaloy claddings.

in the dimensions of the pellets and cladding tubes as well as eccentricities of the pellets in the cladding tube lead to differences in gap widths along the cladding burst circumferential strain. These relationships can be tube circumference and, consequently, to different heat explained by bowing of the Zircaloy cladding tubes transfer coefficients in the gap between the pellets and observed in a number of experiments in the a- and in the cladding tube. In case of external cooling this causes the (a + P) ranges in case of deformation and azimuthal temperature differences on the cladding tube cir- temperature differences. Tube bowing represented in cumference (azimuthal temperature differences). fig. 4 produces the effect that the gap between the pellet In REBEKA single rod tests in which temperature and the cladding tube closes on the hot side and opens differences were allowed to develop on the cladding on the opposite cold side. This causes the azimuthal tube circumference it has been proved that in case of temperature differences to become larger during clad-deformation of Zircaloy cladding in the a- and early ding tube deformation.

(a + 13) phases of the Zircaloy a systematic relationship This deformation behavior of Zircaloy cladding tubes exists between the burst circumferential strain and the is caused by the texture produced in cladding tube azimuthal temperature difference: Small azimuthal tem- fabrication in the hexagonal, densely packed structure.

perature differences cause a relatively uniform reduc- The majority of hexagonal prism shaped crystals have tion in cladding tube wall thickness on the cir- their longitudinal axis and their prism planes oriented cumference and give rise to relatively high burst cir- parallel to the cross sectional plane of the cladding cumferential strains; great azimuthal temperature dif- tube. During plastic deformation under internal over-ferences result in a preferred reduction of wall thickness pressure the strain behavior of these structures is aniso-on the hot part of the cladding tube circumference and tropic; this is characterized by the fact that the tube to relatively low burst circumferential strains. resists weakening of the wall thickness and, conse-Fig. 3 shows in quantitative terms the dominant quently, axial material flow takes place into the de-influence of azimuthal temperature differences on the formed zone which is paralleled by shortening of the

F.J. Erbacher/ Cladding tube deformation and core emergency cooling 59 DIREBEKA-burst criterion.

I lii I .-

Fig. 4. Bowing of Zircaloy tubes during deformation under azimuthal temperature differences and cooling.

0 tube in the course of deformation. If the wall thickness :imuthaldifference o max.xclad temperaturP[K]

is weakened due to azimuthal temperature differences preferably on the hot side of the cladding tube, axial Fig. 5. FR 2 in-pile tests: Burst strain vs. azimuthal tempera-ture difference of Zircaloy claddings.

material flow and tube shortening are intensified on this same side. This causes bowing of the tube which implies that the hot cladding tube side contacts the pellets and the opposite colder cladding tube side moves away from 2.3. Sensitivity to temperature of the Zircaloy cladding the pellets. This is the reason why the deformation tube deformation continues on the hot side as weakening of the wall thickness. As only the hot part of the cladding tube In all experiments performed it has been found that circumference undergoes deformation, this results in the deformation and burst behavior of Zircaloy clad-relatively low circumferential strains of the burst ding tubes responds very sensitively to the cladding Zircaloy cladding. tube temperature and that even temperature differences In representative deformation experiments tempera- of less than 10 K exert a decisive influence on the ture differences of 30 K on the average were measured deformation behavior.

on the cladding tube circumference at the time of burst. Fig. 6 shows calculated circumferential strains as a This reduces the burst circumferential strains to values function of the time for constant cladding tube temper-less than 50%. atures of 790'C, 800 0 C and 810'C at a constant tube Anisotropic strain behavior of Zircaloy and reduc- inner pressure of 60 bar. The figure illustrates the tion of burst circumferential strains by temperature extreme sensitivity to temperature of Zircaloy deforma-differences on the cladding tube circumference were tion. Differences of not more than 10 K in the cladding also observed in the FR 2 in-pile experiments. It is tube temperatures imply changes of the burst time by visible from fig. 5 that also in the course of nuclear fuel about 30 s.

rod deformation substantial azimuthal temperature dif- Because of the efficiency of emergency cooling the ferences occur. No influence has been proved to exist of time at maximum cladding tube temperatures is limited:

the fragmented fuel of burnt up rods and neither an even small temperature differences on the Zircaloy clad-influence of the degree of burnup on the deformation ding tubes decide upon whether the tubes will burst behavior of Zircaloy cladding tubes. after large ultimate strains or whether deformation at a

60 F.J. Erbacher/ Cladding tube deformation and core emergency cooling the primary goal of the REBEKA bundle tests per-formed to study systematically the influence of thermo-hydraulics on cladding tube deformation.

It has been a general and important finding of the 80 - - -

bundle tests that the deformation behavior of the 6 REBEKA-burst 790E Zircaloy cladding tubes in the rod bundle assembly 60 criterion model follows the same laws of Zircaloy deformation as ob-( 0curves) served in the single rod experiments. The burst tempera-p=60 bar tures and burst pressures as well as the dependence of C-onstant circumferential strain on the azimuthal difference of cladding tube temperatures agree well with the respec-Tzcon st ant tive values from single rod tests (see figs. 1 and 3).

0 20 40 60 80 100 120 1 0 160 180 time Is) 3.1. Influence of heat transfer on cladding tube deforma-Fig. 6. Sensitivity of temperature of Zircaloy cladding tube tion deformation.

. It has been proved that the burst circumferential temperature plateau lower by about 10 K will cause the strain of the Zircaloy cladding tubes becomes smaller tubes to deform by just a few percent without burst. the higher the heat transfer from the cladding tube to Even if the burst conditions are attained for all cladding the coolant is. This is attributable to tube bending tubes in a rod bundle, with the given unavoidable occurring as a result of azimuthal differences in clad-temperature differences the great differences in burst ding tube temperatures and external cooling (see fig. 4).

time prevent strong mechanical interactions from occur- As the hot cladding tube side contacts more or less ring between neighboring cladding tube and hence also closely the heat source and the opposite cold side bends greater deformation and damage propagation. continuously off the inner heat source, intensified exter-The high sensitivity to temperature of Zircaloy de- nal cooling gives rise to an enhancement of the dif-formation makes evident that a precise deterministic ferences of the azimuthal cladding tube temperatures prediction of cladding tube deformation in a fuel ele- and, as a result, to a reduction in burst circumferential ment is not possible on the basis of the thermohydraul- strain.

ics computer codes available today because the accuracy Fig. 7 makes evident that bundle tests which are necessary for predicting cladding tube deformation of performed with very low heat transfer, for instance low about 10 K cannot be achieved by these codes.

This underlines the importance of bundle tests to be performed under representative geometric and thermo-hydraulic boundary conditions so that the empirical information about the behavior of fuel elements in a loss-of-coolant accident which is needed for a scope of damage analysis can be derived.

3. Influence of thermohydraulics on cladding tube defor-niation and cooling channel blockage In order to be able to assess the coolability of fuel elements in a loss-of-coolant accident burst experiments were performed on rod bundles in many countries. Very different burst strains and coolant channel blockages were found. These differences were considered for a long time as discrepancies not amenable to an explana-tion. However, it was supposed that they can be attri-buted to differences in the thermohydraulic boundary Fig. 7. Influence of heat transfer on Zircaloy cladding defor-conditions of the experiments. Therefore, it had been mation.

F.J. Erbachler/ Cladding tube deformation and core emergency cooling 61 steam cooling, necessarily will lead to relatively great temperatures. However, up to the next spacer in the burst circumferential strains, whereas bundle tests in direction of flow, the degree of superheat increases which heat transfer coefficients greater than 50 W/m2 again which leads to the development of an axial tem-K dominate which are typical of the flooding phase of a perature profile and a temperature maximum between loss-of-coolant accident yield relatively low burst cir- two spacers.

cumferential strains. The direction of flow in the reactor core during a In all experiments performed under typical heat loss-of-coolant accident depends on the design and transfer conditions average differences in the azimuthal availability of the emergency core cooling systems and cladding tube temperatures of about 30 K developed at on their interaction with the primary circuits. Besides the time of burst which limit the mean burst cir- local differences in flow and steam/water counterflows, cumferential strain to values of approx. 50%. two characteristic and limiting flow directions exist in the reactor core as regards cladding tube deformation 3.2. Influence of the flow direction on -coolant channel and coolant channel blockage in a combined injection mode into the cold and hot legs: flow reversal from the blockage refill to the reflooding phases and unidirected flow during the refill and reflooding phases.

The coolant channel blockage caused by ballooned Fig. 8 illustrates the impacts of a flow reversal on the and burst cladding tubes in the fuel element depends, circumferential strain of the Zircaloy cladding tubes besides on the maximum circumferential strain of the and the resulting coolant channel blockage. In the ex-deformed cladding tubes, also on the axial displacement periment (REBEKA 5) the rod bundle was passed by of the burst points between the spacers. If the burst steam flow from top to bottom during the refill phase points are displaced over a rather large axial zone, the coolant channel blockage is relatively low, but if the burst points occur rather closely to each other, the resulting coolant channel blockage is greater for the same mean burst circumferential strain.

As plastic deformation of Zircaloy cladding tubes responds very sensitively to the cladding tube tempera-ture, the axial displacement of the burst points is de-termined crucially by the axial profile of the cladding tube temperature of the individual fuel rods at the moment of failure and by its temperature maximum between two spacers. The cladding tube temperature profile inter alia is the result of the thermodynamic non-equilibrium in two-phase flow and its being in-fluenced by the spacer grids.

The heat transfer between the rods and the mixture of steam and water droplets is achieved almost exclu-sively by convection. As the heat flow from the cladding tube wall to the steam is much stronger than the heat flow from the steam to the water droplets, a thermody-namic non-equilibrium develops during the flooding phase in two-phase flow which means that the steam is superheated along the coolant channel. In the bundle tests steam temperatures of up to about 600'C were measured which corresponds to about 450 K superheat.

At the spacer straps the incident water'droplets are split up into smaller droplets so that on account of the greater droplet surface a more effective heat sink is 165 17 1:77 .1X831-: 'A-95' ,',0i' 207 ',173 21 22; .5 distance from fop ofheated zonetIml produced for the highly superheated steam. Together with the enhanced turbulence downstream of each spacer Fig. 8. Zircaloy cladding deformation and coolant channel this leads to a reduction in steam and cladding tube blockage under reversed flow (REBEKA 5).

62 F.J. Erbacher/ Cladding tube deformation and core emergency cooling and from bottom to top during subsequent reflooding to a relatively low maximum coolant channel blockage with water in order to simulate flow reversal. So, during of 52%.

the refill phase the cladding tube temperature maximum Fig. 9 shows the deformation pattern for ulidirected initially moves downward towards the spacer provided flow in the rod bundle. In this experiment (REBEKA 6) below the midplane as a result of the downward di- the flow direction of the coolant from bottom to top rected steam flow; In the subsequent flooding phase the was maintained during the refill and reflooding phases.

temperature maximum is displaced in the direction of Unlike the REBEKA 5, the temperature maximum was flow with the flooding time getting longer, towards the moved from the very beginning of the experiment to-spacer provided above midplane, i.e., the temperature wards the upper of the two medium spacers. After this maximum between the spacers at different times occurs temperature profile had developed during the refill at different axial positions. But due to inhomogeneities phase, the temperature maximum continued to occur at in the rod bundle resulting from locally differing rod approximately the same axial positions. This leads auto-powers and cooling, not all the rods are heated up matically to a local concentration of the burst points uniformly which gives different burst times. In RE- and, consequently, to a stronger coolant channel bloc-BEKA 5 the burst time interval of the individual kage. The figure exhibits a pronounced displacement of Zircaloy claddings was about 24 s. During this time the burst points in the direction of flow towards the interval there was a shift in the temperature maximum upper spacer and illustrates the small cladding tube which automatically led to an axial displacement of the strains at spacers. The burst points are displaced only burst points over a rather large range. It is evident from over an axial zone of about 14 cm because the flow the figure that the burst points are spread over some 24 direction has been maintained which results in a greater cm of axial length around the midplane which gives rise coolant channel blockage of 60%.

In the REBEKA 7 experiment the flow direction was likewise maintained, but the cooling conditions during flooding were set in such a manner that a maximum coolant channel could be expected. In this test the greatest coolant channel blockage to be expected under representative flooding conditions was approx. 70%.

4. Coolability of deformed rod bundles The coolant channel blockage caused by ballooned cladding tubes in a rod bundle changes the cooling mechanism and induces two counteracting effects on the local heat transfer:

- Effect of lateral bypass flow of the blockage: This reduces the mass flow through the blocked zone and diminishes the heat transfer.

- Effect of passage through the blockage: This causes droplet atomization, flow acceleration and turbulence intensification and increases heat transfer.

In the FEBA program [8] forced flooding experi-ments were performed on a S X S rod bundle. Ballooned cladding tubes were simulated by conical sleeves fixed to electric heater rods. In the blocked area blockages of 62% and 90% were realized.

It was found that with a 62% blockage the effect of water droplet atomization by which heat transfer is improved dominates so that the cladding tube tempera-ture is even lower in the blocked area than in the Fig. 9. Zircaloy cladding deformation and coolant channel unblocked area. Fig. 10 shows the values measured for a blockage under unidirected flow (REBEKA 6). 90% blockage. Under these extreme conditions the ef-I i

F.J. Erbacher/ Claddingtube deformation and core emergency cooling 63 p = 4.1 bar 1000 -

v = 3.8 cm/s FEBA Test 239 800 0L T I II[I 1925mm cJ 600 -

`-.--Start of Reflooding 1 I- 212 mm

[tJ 4

ai 400-EL E

Gw I,iI III 200 -

O.

0 50 100 i50 200 250 300 350 Time , s 90% blocked Fig. 10. Cladding temperatures in the 90% partly blocked rod bundle.

fect of lateral bypass flow of the blockage is dominat- - A unidirected flow during the refill and reflooding ing. Still, the temperature rise in the blocked zone and phases leads to the greatest possible coolant channel the extension of the rewetting period are insignificant. blockage of about 70%.

This allows the conclusion to be drawn that the - The coolability of deformed fuel elements can be coolability in deformed fuel elements can be maintained maintained up to a coolant channel blockage of up to coolant channel blockages of about 90%. More- about 90%.

over, it has been proved in the REBEKA program that All effects described underline that in a loss-of-burst cladding tubes improve the coolability even fur- coolant accident no impairment whatsoever must be ther [9]. expected of the coolability of the fuel elements and that the safety margin applied in assessing the coolability is greater than predicted by most of the computer codes.

5. Summary and conclusion Therefore, it can be assumed that the safety of the population is fully guaranteed in the event of a loss-of-Work performed on cladding tube deformation and coolant accident.

core emergency cooling has provided sufficiently vali-dated knowledge of the major mechanisms so that the safety of a pressurized water reactor can be assessed. Acknowvledgement Partial aspects which are still unanswered do not put in This report has been prepared from contributions by doubt the results obtained and their application in the licensing procedure. many colleagues.

The most important results can be summarized as The research activities were carried out under the Nuclear Safety Project (PNS). Special thanks are due to follows:

- The number of the burst cladding tubes and their Mr. A. Fiege, PNS, for the support and promotion of burst circumferential strain can be determined with these activities.

sufficient accuracy if the temperature and pressure development of the fuel rods is known.

References

- The cooling effect of the two-phase flow which is intensified during flooding increases the temperature [1] G. Glass, R. Meyder and E. Stratmanns, Die COSIMA-Ex-differences on the cladding tube circumference and periments und ihre Nachrechnung, eine Datenbasis zur limits in this w(ay' the mean burst circumferential Oberpridfung von Rechenprogramnmen fMr Zweiphasen-strains to values of about 50%. strbmungen, K!K 4002 (December 1985).

64 F.J. Erbacher/ Cladding tube deformation and core emergency cooling

[2] H.. Neitzel and H.E. Rosinger, The development of a [6] M. Bocek, P. Hofmann and C. Petersen, Superplasticity of burst criterion for Zircaloy fuel cladding under LOCA Zircaloy-4, STP 633, ASTM (1977).

conditions, KfK 2893, AECL 6420 (October 1980). [7) P. Hofmann and J. Spino,'Stress corrosion cracking of

[3] A. Lehning, K. MUller, D. Piel and L. Schmidt, Berstver- Zircaloy-4 cladding at elevated temperatures and its rele-suche an Zircaloy-Hi-llrohren unter kombinierter mecha- vance to transient LWR fuel rod behaviour, J. NucI. Mater.

nisch-chemischer Beanspruchung (FABIOLA), Reaktorta- 125 (1984) 85-95.

gung 1980, Berlin. [8] P. IhWe and K. Rust, FEBA - Flooding experiments with

[4] E.H. Karb, M. Priussmann, L. Sepold, P. Hofmann and G. blocked arrays, Evaluation Report, KfK-3657 (March 1984).

Schanz, LWR fuel rod behavior in the FR-2 in-pile tests [9] FJ. Erbacher, P. Ihle, K. Wiehr and U. Muller, Reflood simulating the heatup phase of a LOCA, Final Report, heat transfer in PWR fuel rod bundles deformed in a KfK 3346 (March 1983). LOCA, International Symposium on Heat Transfer, Oc-

[5] P.D. Parsons, E.D. Hindle and C.A. Mann, The deforma- tober 15-18, Beijing, China.

tion, oxidation and embrittlement of PWR fuel cladding in a loss-of-coolant accident - A state of the art report, to be published as CSNI-Report.

II i

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Secretariat American Nuclear Society Prepared by the American Nuclear Society Standards Committee Working Group ANS-5.1 Published by the American Nuclear Society 555 North Kensington Avenue La Grange Park, Illinois 60525 USA Approved August 23, 1994 by the American National Standards Institute, Inc.

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Time after Decay heat power uncertainty One sigma shutdown F(t,.) AF(t,-) uncertainty t(s) (MeV/fissionY)" (MeV/fission) (percent) 1.OE+00 1.238E+010 0.036E+01 2.8 1.6E+OO 1.201E+01 0.030E+01 2.5 2.OE+00 1.170E+01 0.028E+01 2.4 4.OE+00 1.084E+01 0.024E+01 2.2 6.OE+00 1.026E+01 0.022E+01 2.1 8.0E+0O 9.834E+00 0.197E+00 2.0 1.OE+01 9.497E+00 0.190E+00 2.0 1.6E+01 8.886E+00 0.169E+00 1.9 2.OE+01 8.460E+00 0.161E+00 1.9 4.OE+01 7.463E+00 0.134E+00 1.8 6.OE+01 6.892E+00 0.124E+00 1.8 8.OE+01 '6.497E+00 0.117E+00 1.8 1.OE+02 6.202E+00 0.112E+00 1.8 1.5E+02 6.700E+00 0.103E+00 1.8 2.OE+02 6.373E+00 0.097E+OO 1.8 4.OE+02 4.671E+00 0.084E+00 1.8 6.OE+02 4.2B7E+00 0.077E+00 1.8 8.OE+02 4.013E+00 0.072E+00 1.8 1.OE+03 1.6E+03 3.799E+00 3.411E+00 0.068E+00 0.061E+00 1.8 1.8 E 2.OE+03 3.140E+00 0.057E+00 1.8 4.OE+03 2.638E+00 0.046E+00 1.8 6.OE+03 2.238E+00 0.038E+00 1.7 8.OE+03 2.048E+00 0.035E+OO 1.7 l.OE+04 1.912E+00 0.033E+00 1.7 1.5E+04 1.688E+00 0.030E+00 1.8 2.OE+04 1.649E+00 0.028E+OO 1.8 4.OE+04 1.262E+00 0.023E+00 1.8 6.OE+04 1.121E+OO 0.021E+00 1.9 8.OE+04 1.033E+00 0.021E+00 2.0 l.OE+05 9.729E-01 0.195E-01 2.0 1.6E+05 8.772E-01 0.176E-01 2.0 2.0E+05 8.191E-01 0.164El01 2.0 4.OE+05 7.012E-01 0.140E-01 2.0 6.OEt05 6.368E-O1 0.127E-Ol 2.0 8.OE+05 6.906E-01 0.118E-O1 2.0 l.OE+06 6.547E-01 0.111EO1 2.0 1.6E+06 4.904E-01 0.098E-01 2.0 2.OE+06 4.463E-01 0.089E-01 2.0 4.OE+06 3.494E-01 0.073E-01 2.1 6.OE+06 3.020E-01 0.064E-01 2.1 8.OE+06 2.717E-01 0.057E-O1 2.1 e

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ANS 5.1 94 _ 0724818 0202211 633 C American National Standard ANS/ANS-6.1-1994 Table S. Tabular data for standard decay heat power for thermal friion of "Pu following an irradiation of lOts seconds One sigma Is Time after Decay heat power uncertainty One sigma shutdown F(t,-) AF(t,o) uncertainty (sec) (WeV/fission)rl (MeV/fission) (percent) 1.OE+oo 1.027E+01(' 0.046E+01 4.5 1.5E+00 1.003E+01 0.042E+01 4.2 2.OE+00 9.822E+00 0.993E+00 4.0 4.OE+00 9.213E+00 0.250E+00 3.8 6.OE+00 8.802E+00 0.326E+00 3.7 8.OE+00 8.494E+00 0.314E+00 3.7 l.OE+01 8.250E+00 0.297E+00 3.6 1.6E+01 7.801E+00 0.281E+00 3.6 2.OE+01 7.483E+00 0.269E+00 3.6 4.OE+01 6.713E+00 0.242E+00 3.6 6.OE+01 6.257E+00 0.225E+00 3.6 8.OE+01 5.935E+00 0.214E+00 3.6 1.OE+02 6.691E+00 0.205E+00 3.6 1.6E+02 5.268E+00 0.190E+00 3.6 2.0E+02 4.988E+00 0.180E+00 3.6 4.0E+02 4.363E+00 0.167E+00 3.6 6.0E+02 3.999E+00 0.148E+00 3.7 8.0E+02 3.733E+00 0.138E+00 8.7 1.OE+03 16E+03 2.OE+03 3.622E+00 3.134E+00 2.864E+00 0.130E+00 O.119E+00 0.112E+00 3.7 3.8 3.9 I

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