Title: International Standard Problem ISP 42 Simulation Exercise on PANDA Tests
1International Standard Problem (ISP- 42)
Simulation Exercise on PANDA Tests
4th RCM on the IAEA CRP on Natural Circulation
Phenomena, Modelling and Reliability of Passive
Safety Systems that Utilize Natural Circulation
- A.K. Nayak, P.P. Kulkarni, V. Jain and P.K.
Vijayan - Reactor Engineering Division,
- Bhabha Atomic Research Centre,
- Trombay, Mumbai, INDIA - 400 085
Vienna, Austria, Sept. 10-13, 2007
2ISP-42
- The ISP-42 exercise was carried out in the PANDA
facility located at PSI, Switzerland under the
auspices of the OECD NEA committee for the safety
of nuclear installations (CSNI), financed by the
research foundation of Swiss Utilities. - The ISP-42 tests consists of six phases (Phase A
through Phase F) for the simulation and study of
various passive safety systems of the ESBWR,
particularly in the containment during a
postulated LOCA situation. - The test Phases A to F are presently being
simulated using the codes ASTEC and RELAP5
3Description of the PANDA Facility
- PANDA is a large-scale facility constructed at
PSI, mainly to investigate containment phenomena.
Also, the facility is used for the investigation
of both overall system response and key phenomena
of PCCS during the long term decay heat removal
for Advanced Light Water Reactors (ALWRs). - It is scaled 140 with respect to the power and
volume, and 11 with respect to height of the
ESBWR. - The decay heat in the core of the Reactor
Pressure Vessel (RPV) is simulated by
electrically heated rods. - Besides the RPV, the facility simulates the
Drywells (DWs), Wetwells (WWs), Gravity Driven
Cooling System (GDCS) tank, Passive Containment
Coolers (PCCs) along with the pool and the
associated piping.
4Schematic of PANDA
PCC3FEEDL
PCC2FEEDL
PCC1FEEDL
PCC1
PCC3
19800
PC1FEEDL
PEL
PCC2VNTL
PCCDRNL
PCC3VNTL
GDCS
PCC1VNTL
GDCSDRNL
DW1
DW2
MSL1
11700
VB2
MSL2
R P V
MVL1
MVL2
VB1
WW1
WW2
WETLINE2
WETLINE1
000
5PANDA component geometry details
6Summary of Phases
7Computer Code ASTEC
- ASTEC (Accident Source Term Evaluation Code)
- Main capabilities
- Applications to PSA2, including uncertainty
analysis, - Accident management studies,
- Investigations of NPP behaviour in Severe
Accident condition, including source term
evaluation, - Support and interpretation of experiments,
- Basis for a better understanding of Severe
Accident physical phenomena.
8ASTEC Main Modules
- CESAR module for RCS thermal hydraulics
- Water and gas (steam, H2 is the only
non-condensable gas in this version), - 5-equation approach
- DIVA module for core degradation
- RUPUICUV module for Simulation of Direct
Containment Heating effects in cavity through a
semi-empirical approach (correlations). - CORIUM module for Simulation of the behaviour of
corium droplets transported by DCH hot gases into
the containment atmosphere and sump. - MCCI modules for concrete ablation and release of
noncondensable gases - CPA module lumped-parameter approach in a
multi-comp. containment
9RELAP5/MOD3.2 Code
- RELAP5/MOD3.2 is a best estimate code used mostly
for nuclear reactor thermal hydraulic analysis - It is based on one-dimensional two-fluid model
(six-equation model). - The code has been extensively validated with
several test data for integral as well as
separate effect tests. - The code is capable of simulation of condensation
phenomena in presence of non-condensables. - There is evidence of assessment of
non-condensable test data for passive cooling
systems and ability to capture degradation of
heat transfer coefficient in presence of
non-condensables.
10 Simulation Results
- Simulation of Phase A and B has been completed
- Phase C is currently being simulated
- Simplifications
- Heat losses are neglected
- The CESAR module of ASTEC Considers only hydrogen
as the noncondensable gas in place of air
11ASTEC nodalization of PANDA facility
PCCS
GDCS
DW-2
DW-1
RPV
WW-2
WW-1
12RELAP5 Nodalization of PANDA facility
13Phase A Simulation
- Start-up of PCCS
- To study the start-up of passive cooling system
when steam is injected into a cold Drywell filled
with air and to observe the resulting gas mixing
and system behavior. - The specific phenomena observed during the phase
were - Steam jet injection into Drywell
- Air/Steam venting into suppression chamber
- Gas mixing and stratification in Drywell and
Wetwell gas space - Steam condensation on walls of drywell and in
tubes of PCC - System pressurization
14Phase A Configuration
- All vessels are connected.
- GDCS drain line is closed
- Vacuum Breaker (VBL) and Main vent lines (MVL)
are closed.
15Phase A initial and boundary conditions
Initial conditions
- Boundary condition
- The test was carried out at constant 1 MW power
throughout
- Simulation procedure
- All systems including PCCS are valved-in at time
t0 s - Test initiation Switching on RPV heater and
raising it to 1 MW at time t 0 - Test termination Pair or 6000 s test duration
- Transient calculations were continued till 5000 s
16Phase A Sample results
RPV Pressure
RPV Temperature
17Phase A Sample results
Steam Flow Rate From RPV to DW1
Gas Partial Pressure
18Phase B Simulation
- GDCS Discharge
- To investigate the discharge of cold water from
the GDCS tank into the Reactor Pressure Vessel
(RPV) and to observe induced phenomena such as -
- Discharge of cold water into saturated RPV
- Void collapse in RPV,
- Vacuum breaker opening,
- Non-condensable gas entrainment from the SC to
DW, - Resumption of boiling in RPV,
- PCCS start-up.
19Phase B Configuration
- GDCS Drain opened
- Vacuum breaker lines are opened
- Vacuum Breaker Valve opens if ?p 3.2 kPa and
closes if ?p - Remaining configuration same as phase A.
20Phase B initial and boundary conditions
Boundary Condition
Initial Condition
- This phase was carried out with 1.4 MW power for
initial 300 s and then reducing it linearly to22
800 kW in next 1800 s, then keeping it constant
till the end - The GDCS Discharge starts at 48 s and continues
till the GDCS tank is empty (till 1271 s)
21Phase B Sample results
RPV inventory
GDCS inventory
22Phase B Sample results
Steam Flow Rate through MSL1
Drywell Pressure
23Conclusions
- Simulation of ISP-42 test phases A and B has been
carried out using the codes ASTEC and RELAP5. - Predictions are compared with the experimental
data - The deviation in ASTEC simulation of gas partial
pressure can be attributed to the fact that the
CESAR module of ASTEC can model only hydrogen as
non-condensable gas.