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1. CIRCULATING-FUEL<br />

A few relatively minor changes in<br />

<strong>the</strong> design of some phases of <strong>the</strong><br />

Aircraft Reactor kxperiment have been<br />

made in <strong>the</strong> past quarter. These<br />

changes involved <strong>the</strong> off-gas system<br />

and <strong>the</strong> fuel disposal system, pri-<br />

marily, and are discussed below.<br />

There have been no changes in <strong>the</strong><br />

general design, and detailing of con-<br />

struction and installation designs<br />

has been largely completed. Installa-<br />

tion of equipment in <strong>the</strong> building has<br />

proceeded at an accelerated rate<br />

throughout <strong>the</strong> quarter but has not<br />

yet reached <strong>the</strong> expected peak rate.<br />

Components from outside vendors, as<br />

well as those fabricated in OMNL<br />

shops, are being received in increas-<br />

ing quantity; but some of <strong>the</strong> major<br />

items, notably, <strong>the</strong> heat exchangers,<br />

have not yet been received. It is<br />

expected that all components w i l l be<br />

on hand by <strong>the</strong> end of <strong>the</strong> year.<br />

Component testing is proceeding in<br />

<strong>the</strong> experimental engineering labora-<br />

tories (sec. 2) , but <strong>the</strong> final component<br />

testing is to be done in <strong>the</strong> ARE<br />

Building. It is now planned to by-<br />

pass <strong>the</strong> reactor so that a thorough<br />

system test can be made before <strong>the</strong><br />

nondrainable reactor is tied into <strong>the</strong><br />

circuit. This procedure w i l l make<br />

possible a complete shake-down run<br />

without <strong>the</strong> possibility of incorporat-<br />

ing a nondrainable component in <strong>the</strong><br />

system. The design change necessitated<br />

by this alteration in operational<br />

procedure isminor and will be effected<br />

in <strong>the</strong> field. Considerable effort<br />

during <strong>the</strong> quarter went into <strong>the</strong><br />

preparation of <strong>the</strong> “Hazards I’\eport, ”(’)<br />

which, in addition to serving <strong>the</strong><br />

.--... ... .-....... .-............ ............<br />

(”J. 8. Buck and W. B. Cottrell, Aircraft<br />

Reactor Erper irent Haxards Summary Report,<br />

ORNL-1407 (Nov. 24, 1952).<br />

PERIOD ENDING DECEMBER<br />

AIRCRAFT REACTOR EXPERIM ENT<br />

J. H. Buck<br />

Research Director’s Division<br />

E. S. Bettis<br />

A?P Division<br />

10, 1952<br />

purpose implied in <strong>the</strong> name, provided<br />

<strong>the</strong> first draft of an operations manual<br />

for t he e xp e r i men t .<br />

It is practically impossible to<br />

predict a date for satisfactory opera-<br />

tion of <strong>the</strong> ARE. There are no means<br />

available for predetermination of <strong>the</strong><br />

time required to correct difficulties.<br />

It is not so difficult to attempt to<br />

predict a date for <strong>the</strong> completion of<br />

<strong>the</strong> installation of equipment, and<br />

<strong>the</strong>refore a date for beginning <strong>the</strong><br />

system test in <strong>the</strong> building. At<br />

present it is expected that <strong>the</strong> system<br />

w i l l be ready for initial testing<br />

near <strong>the</strong> first of June 1953. No<br />

uranium w i l l be added to <strong>the</strong> system<br />

until all reasonable checks have been<br />

made to ensure <strong>the</strong> integrity of <strong>the</strong><br />

entire assembly.<br />

FLUID CIRCUIT<br />

G. A. Cri sty, Engineering Dep artment<br />

The previous report ( 2, discussed<br />

design changes necessitated by <strong>the</strong><br />

higher fuel viscosities. In brief,<br />

<strong>the</strong> higher viscosities reduced <strong>the</strong><br />

Reynold’s number of <strong>the</strong> heat exchanger<br />

tuhe side and changed <strong>the</strong> heat transfer<br />

coefficient to such an extent that <strong>the</strong><br />

c a1 c u l ated minimum fi 1 rn temperatures<br />

were in <strong>the</strong> vicinity of <strong>the</strong> freezing<br />

point. Two corrective measures were<br />

discussed; redesigning <strong>the</strong> heat ex-<br />

changers and increasing <strong>the</strong> flow rate<br />

through <strong>the</strong> entire circuit. The first<br />

change has been accomplished. The<br />

need for <strong>the</strong> increased flow rate has<br />

been obviated by an accurate measure-<br />

ment of <strong>the</strong> fuel <strong>the</strong>rmal conductivity;<br />

<strong>the</strong> new value of k i s 1.5 Btu/hr*ft’OF,<br />

whereas 0.5 had been used in earlier<br />

(2)G. A. Cristy, ANP Quar. Prag. Rep. Sept. 10,<br />

1959, OWL-1375, p. 64<br />

7

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