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ORNL-1771 - Oak Ridge National Laboratory

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Four years of work on the ANP Project at ORtdL<br />

have led to the belief that the circulating-fluoride-<br />

fuel reactor with reflector moderation and a spheri-<br />

cal-shell heat exchanger can be developed into<br />

an aircraft power plant of exceptionally high per-<br />

formance.' This view has been supported in<br />

recent months by the results of studies by USAF<br />

contractors. The question has now became how<br />

best to bridge the gap between the ARE and a<br />

prototype aircraft power plant.<br />

It was proposed about a year ago that a 50-Mw<br />

reactor be built so that the feasibility of con-<br />

structing and operating a circulating-fuel reflector-<br />

moderated reactor could be investigated and its<br />

performance characteristics, particularly with ref-<br />

erence to control, shielding, heat transfer, and fluid<br />

flow, could be determined. Preliminary estimates<br />

indicated that a power of at least 25 Mw would<br />

be required to disclose the more important control<br />

characteristics. Other studies indicated that an<br />

output of 50 Mw would be required for the lowest<br />

powered aircraft likely to be tactically useful (for<br />

radar picket ships, patrol bombers, etc.), while<br />

an output of 150 to 200 Mw would be required (with<br />

chemical-fuel augmentation) to power a strategic<br />

bomber. Preliminary reactor test unit designs and<br />

cost estimates indicated that the time and cost<br />

involved would be roughly proportional to the rated<br />

output of the reactor (largely because the size<br />

and cost of the heat exchangers, pumps, and heat-<br />

dump equipment vary directly with reactor power).<br />

After much analysis and discussion it was decided<br />

that 60 Mw represented a good compromise for the<br />

power rating and that such a reactor, to be called<br />

the Circulating-Fuel Reactor Experiment (CFRE),<br />

should be built by QRNL, with the aid of the<br />

Pratt & Whitney Aircraft Division. This test unit<br />

is to embody the basic features and proportions<br />

that have made the circulating-fuel reactor ottractive<br />

for aircraft use, but the details of the<br />

pumps, radiators, and auxiliary equipment w~ll not<br />

have to meet aircraft requirements of size, weight,<br />

etc. An operating life of 500 hr, of which a sub-<br />

stantial portion should be at or near 60 Mw, was<br />

'A. P. Fraas and A. W. Savolainen, <strong>ORNL</strong> Azrcra/t<br />

Nuclcnr Power Planf Deszgns, <strong>ORNL</strong>-1721 (in press].<br />

2. REFLECTOR-MODERATED REACTOR<br />

A. P. Fraas<br />

Aircraft Reactor Engineering Division<br />

PERIOD ENDING SEPTEMBER 70, 7954<br />

considered to be a desirable goal. The information<br />

gained from this project should serve to provide<br />

a sound basis for the design of the full-scale<br />

aircraft reactor.<br />

As has been the case with the ARE, the CFRE<br />

will require a major supporting effort on the part<br />

of various groups in the QRNL organization to<br />

obtain much essential information not yet avail-<br />

able. The program on fuel chemistry, for example,<br />

will continue along the lines it has followed. The<br />

results of research on Loth the basic chemistry<br />

and the in-pile and out-of-pile corrosion tests are<br />

obviously vital to the project. Metallurgical re-<br />

search on promising alloys, welding and brazing<br />

techniques, strength properties at various tempera-<br />

tures and in various ambients, and related work<br />

will help greatly to increase the reliability, and<br />

possibly the operating temperature, of the system.<br />

Tests under way at the Tower Shielding facility<br />

coupled with further Lid Tank Shielding Facility<br />

tests will provide a more complete basis for the<br />

aircraft shield design. Multigroup calculations<br />

coupled with critical experiments should provide<br />

additional information on the static physics of<br />

the reactor. Much test work in experimental engi-<br />

neering will be required to validate key features<br />

of the design.<br />

DESIGN OF THE CFRE<br />

A. P. Fraas R. W. Bussard<br />

Aircraft Reactor Engineering Division<br />

The design of the CFRE is still preliminary,<br />

but some tentative data can be presented at this<br />

stage. As presently conceived, the CFRE will<br />

i nc lude a react or, heat-exchanger, pres sure-she I I ,<br />

and shield assembly, as described in previous<br />

report^.^^^ A quasi-unit shield structurally and<br />

functionally similar to one suitable for an aircraft<br />

will probably be used,4 although the structure will<br />

2A. P. Fraas, ANP Qunr. Prog. Rep. Mar. 10, 1953,<br />

<strong>ORNL</strong>-1515, p 61.<br />

3R. W. Bussard and A. P. Fraas, ANP Quur. Prog.<br />

Rep. Dec. 10, 1953, <strong>ORNL</strong>-1649, p 31.<br />

4E. P. Blizord and H. Goldstein (eds), Report u/ the<br />

1953 Sunrmer Thzrldzng Sesrzon, <strong>ORNL</strong>-1575 (June 11,<br />

1954).<br />

17

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