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ORNL-1816 - the Molten Salt Energy Technologies Web Site

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g 010<br />

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a<br />

E O<br />

UNCLASSIFIED<br />

2-01-059-!5<br />

0 1 2 3 4 5 6 7 8 9<br />

THICKNESS (in )<br />

Fig. 12.4. Radiation Heating of a 9din.-Thick<br />

Beryllium Slab by Normally Incident Photons.<br />

In Fig. 12.4 <strong>the</strong> smooth fits to <strong>the</strong> statistical<br />

data are presented for normally incident photons of<br />

energy 0.5, 1.5, and 5.0 mOc2, The effect of <strong>the</strong><br />

reflected photons on <strong>the</strong> energy absorption curve<br />

is readily seen at <strong>the</strong> entrance face of <strong>the</strong> slab.<br />

The value of <strong>the</strong> fraction of energy absorbed per<br />

inch at <strong>the</strong> entrance face for <strong>the</strong> incident photons<br />

can be calculated by multiplying ps, <strong>the</strong> scattering<br />

cross section, by f, <strong>the</strong> average fraction of energy<br />

absorbed by <strong>the</strong> ~naterial.~ These values for 0.5,<br />

1.5, and 5.0 mOc2 are, respectively, 0.118, 0.123,<br />

and 0.089. The large contribution of <strong>the</strong> reflected<br />

component is especially evident for <strong>the</strong> 0.5-m0c2<br />

Dhotons at <strong>the</strong> entrance face as <strong>the</strong> difference be-<br />

tween 0.1 18<br />

12.4. The e<br />

1.5-mnc2 ph<br />

5 060<br />

Z 056<br />

052<br />

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8 040<br />

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g 020<br />

PERIOD ENDING DECEMBER 10,7954<br />

UNC-ASSI~IEO<br />

2-01-059-14<br />

Z 016<br />

8 012<br />

6 008<br />

k 004<br />

$ 0<br />

0 1 2 3 4 5 6 7 8 9<br />

THICKNESS (in )<br />

Fig. 12.5. Radiation Heating of a 9-ireThick<br />

Beryl lium Slab by Slant-inci dent 1.5.m oc2 F'hoton s.<br />

induced injury with time. Just recently <strong>the</strong> ANP<br />

Medical Advisory Group (ANP-MAG) issued recom-<br />

mendations' which made some concessions in this<br />

direction in that increased total doses were allowed<br />

for schedules which distributed <strong>the</strong> radiatilon over<br />

longer times. It has been demonstrated9 that <strong>the</strong><br />

ANP-MAG recommendations can be expressed to<br />

within 4% by a ma<strong>the</strong>matical formulation with three<br />

parameters based on a model of partly irreparable<br />

injury and partly injury which recovers exponen-<br />

tially with time, The model was previou:jly sug-<br />

gested by Blair.10'12 The ma<strong>the</strong>matical formula-<br />

tion is much more flexible than <strong>the</strong> Biological<br />

Planning Chart which expresses <strong>the</strong> ANP-MAG<br />

recommendations, since it gives a unique value of<br />

'"Yjnutes of <strong>the</strong> 3rd ANP-MAG Meetin - 11-12 May<br />

1954, School of Aviation Medicine, 5-18,862.<br />

Several Weeks, UR-312 (Feb. 10, 1954).<br />

145

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