ML19210A915: Difference between revisions

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E. G. Case, DRS P. A. Morris, DRL F. Schroeder, DRL C. G. Long, DRL F. W. Karas, DRL D.      s, DEL c File 50-28/
E. G. Case, DRS P. A. Morris, DRL F. Schroeder, DRL C. G. Long, DRL F. W. Karas, DRL D.      s, DEL c File 50-28/
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  ,      [' N &                    " NATIONAL AERONAUTICS AN SPACE ADMINISTRATION
  ,      [' N &                    " NATIONAL AERONAUTICS AN SPACE ADMINISTRATION
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       /                                                    CL  ELAND O so 4413 5                      '.
       /                                                    CL  ELAND O so 4413 5                      '.
             , , , y                    T ELEPHONE: 218 433 4o00      TWX. 218 433-4768 TELEX: C98-S2f 8 m "PLv a uta to 4000 March 3, 1971                1IU                s L.        E h(d, i AIR Mall                                                                          $        .
             , , , y                    T ELEPHONE: 218 433 4o00      TWX. 218 433-4768 TELEX: C98-S2f 8 m "PLv a uta to 4000 March 3, 1971                1IU                s L.        E h(d, i AIR Mall                                                                          $        .
                                                                                                        ''
                                                                                                                       \F 7 Mr. Ray G. Smith                                            -
                                                                                                                       \F 7 Mr. Ray G. Smith                                            -
                                                                        - .
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                                                                                                                           -3 Special Assistant to the Director                                                  <3          0 0 M1 for Standards and Guides                                                              .          d-h'#        %
                                                                                                                           -3
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Special Assistant to the Director                                                  <3          0 0 M1 for Standards and Guides                                                              .          d-h'#        %
Division of Reactor Standards                                                            V, U.S. Atomic Energy Commission                                                                    'O d'#
Division of Reactor Standards                                                            V, U.S. Atomic Energy Commission                                                                    'O d'#
Washington, D.C. 20545
Washington, D.C. 20545
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I would reconnend, also, that a test be required when the installation is finalized to be assured that the timing of the actuation of the components is according to the design philosophy.                      Such a test can be made with pans of aviation fuel distributed along the tunnel and ignited to simulate a fuel fire in the air intake. The. quantity of fuel can be small enough to be safe within the structure of the tunnel, yet provide a continuous path for fire propagation along the tunnel. A narrow pan
I would reconnend, also, that a test be required when the installation is finalized to be assured that the timing of the actuation of the components is according to the design philosophy.                      Such a test can be made with pans of aviation fuel distributed along the tunnel and ignited to simulate a fuel fire in the air intake. The. quantity of fuel can be small enough to be safe within the structure of the tunnel, yet provide a continuous path for fire propagation along the tunnel. A narrow pan
       -xtending the length of the tunnel me.asuring I foot in width and 4 inches in depth should be adequate. This can be made in sections which contact each other to provide a continuous combustible path. Two inches of water should Ile in the bottom of the pan and a 1 inch layer of JP-4 1539 207
       -xtending the length of the tunnel me.asuring I foot in width and 4 inches in depth should be adequate. This can be made in sections which contact each other to provide a continuous combustible path. Two inches of water should Ile in the bottom of the pan and a 1 inch layer of JP-4 1539 207
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2 fuel floated on the water. Extinguishing system response time, the adequacy of the Halon and water deluge rate of flow, and the total quantity of Halon and water for effective extinguishment should be observed. The water deluge should have sufficient capacity to prevent re-flash of the fire.
2 fuel floated on the water. Extinguishing system response time, the adequacy of the Halon and water deluge rate of flow, and the total quantity of Halon and water for effective extinguishment should be observed. The water deluge should have sufficient capacity to prevent re-flash of the fire.
The protection arrangements that are now planned represent an enormous improvement over the first concepts which were described two years ago.
The protection arrangements that are now planned represent an enormous improvement over the first concepts which were described two years ago.
I congratulate the AEC for diligence in this matter.
I congratulate the AEC for diligence in this matter.
Sincerely yours,
Sincerely yours,
                                                          -
                                                    ,
                                             ;
                                             ;
: i. Irving Pinkel Director of Aerospace Safety Research and Data institute
: i. Irving Pinkel Director of Aerospace Safety Research and Data institute B
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B
                                                                                $
                                                             )JO/ IUU
                                                             )JO/ IUU
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Revision as of 05:47, 2 February 2020

Notifies of Completed Review of TMI-1 Amended Air Intake Protective Devices Sys.Improvement Enormous.Makes Recommendations Re Halon Agent & post-installation Testing
ML19210A915
Person / Time
Site: Three Mile Island Constellation icon.png
Issue date: 03/03/1971
From: Pinkel I
NATIONAL AERONAUTICS & SPACE ADMINISTRATION
To: Rich Smith
US ATOMIC ENERGY COMMISSION (AEC)
References
NUDOCS 7911010626
Download: ML19210A915 (3)


Text

"

e DISTRIBUTION:

E. G. Case, DRS P. A. Morris, DRL F. Schroeder, DRL C. G. Long, DRL F. W. Karas, DRL D. s, DEL c File 50-28/

1ECQ fJU/

^n BOD' 7911010 b 26 g

m

= 4 Niy .

, [' N & " NATIONAL AERONAUTICS AN SPACE ADMINISTRATION

_I g j LEWIS RESEARCH CENTER

/ CL ELAND O so 4413 5 '.

, , , y T ELEPHONE: 218 433 4o00 TWX. 218 433-4768 TELEX: C98-S2f 8 m "PLv a uta to 4000 March 3, 1971 1IU s L. E h(d, i AIR Mall $ .

\F 7 Mr. Ray G. Smith -

Q #g... % c. d c;

-3 Special Assistant to the Director <3 0 0 M1 for Standards and Guides . d-h'#  %

Division of Reactor Standards V, U.S. Atomic Energy Commission 'O d'#

Washington, D.C. 20545

Dear Mr. Smith:

I have reviewed the amended air intake protective devices system for the Three Mile Island Nuclear Station, Unit No. 1, and I find my confidence in the design has increased considerably. While I cannot assess the effectiveness of the water deluge and Halon distribution arrangements, I assume that the proposal uses existing criteria for effective application. With regard to the Halon distribution system, I would recommend that the quantity of Halon agent in each zone be adequate to render the total air intake tunnel volume safe from fire.

Since no mention is made of the quantities of Halon agent in each zone, I assume that the Intended quantity is enough to raise the con-centration of Halon gas to the 5% level for effective extinguishment in a volume equal to that of the zone only. I am afraid that such a criterion would be marginal since the Halon discharged in one zone would flow into the adjacent zones and decrease the Halon concentration below the effective value.

I would reconnend, also, that a test be required when the installation is finalized to be assured that the timing of the actuation of the components is according to the design philosophy. Such a test can be made with pans of aviation fuel distributed along the tunnel and ignited to simulate a fuel fire in the air intake. The. quantity of fuel can be small enough to be safe within the structure of the tunnel, yet provide a continuous path for fire propagation along the tunnel. A narrow pan

-xtending the length of the tunnel me.asuring I foot in width and 4 inches in depth should be adequate. This can be made in sections which contact each other to provide a continuous combustible path. Two inches of water should Ile in the bottom of the pan and a 1 inch layer of JP-4 1539 207

2 fuel floated on the water. Extinguishing system response time, the adequacy of the Halon and water deluge rate of flow, and the total quantity of Halon and water for effective extinguishment should be observed. The water deluge should have sufficient capacity to prevent re-flash of the fire.

The protection arrangements that are now planned represent an enormous improvement over the first concepts which were described two years ago.

I congratulate the AEC for diligence in this matter.

Sincerely yours,

i. Irving Pinkel Director of Aerospace Safety Research and Data institute B

)JO/ IUU

/

- . . . .