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DEVELOPMENT OF THE SRE MARK 1 SAFETY ROD

Technical Report ·
OSTI ID:4250006
Designs development, and testing of the SRE Mark I safety rod are reported. In this device all of the operating mechanisms, with the exception of a removable drive botor, are located in a sealed thimble beneath the reactor loading face. The safety rod incorporates a solenoid operated mechanical latch to drop the neutron absorbing elements a ball screw for retrieving the element and a gas compression tyne shock absorber. The neutron absorbing element falls at ~ 92 per cent the acceleration of gravity and is fully inserted in ~0.96 second. At full reactor power the moving mechanisms of the safety rod operate at 1100 F in a helium atmosphere. The materials problems encountered in operating mechanisms at high temperatures and their solutions are discussed. The difficulties encountered in high temperature testing of the prototype safety rod have led to limited use of the Mark I safety rod in the SRE. (auth)
Research Organization:
Atomics International Div., North American Aviation, Inc., Canoga Park, Calif.
DOE Contract Number:
AT(11-1)-GEN-8
NSA Number:
NSA-13-014063
OSTI ID:
4250006
Report Number(s):
NAA-SR-2008
Country of Publication:
United States
Language:
English

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