FIELD: nuclear engineering; spacecraft nuclear reactors. SUBSTANCE: reactor core is divided into two subcores which are mounted in tandem on reactor longitudinal axis; one of subcores is subcritical and spaced from other subcore at distance ranging within values of which maximum is chosen from inequality , where Dcore is diameter of cores, sq.m; π is pi number equal to 3.14; Fact. is multiplication factor of neutrons in critical subcore; Pn is return probability of neutrons formed in critical subcore and those returned to subcritical subcore; minimum value is chosen from set of inequalities , where S is neutron density at end of critical subcore in power condition (m-3s-1); K∞ is subcritical subcore multiplication factor; P is leakage probability of neutrons produced in critical subcore through gap between subcores; Q.h.r. is permissible power of heat-removal system in subcritical subcore in power condition, W; Fact. is effective multiplication factor of critical subcore in shutdown state; Σk is material neutron absorption macrosection between ends of subcores, (m-1); Σfuel is fissionable material absorption macrosection in subcritical subcore, (m-1); ΔKs.s. is safety system efficiency in reactor subcritical subcore; Σa is subcritical subcore absorption macrosection, (m-1); γfuel is nuclear concentration of fissionable material in subcritical subcore, (m-3). EFFECT: reduced cost of reactor and facilitated manufacture along with reduced size and mass of reactor and vehicle as a whole; facilitated transfer from one operating condition of vehicle to other and provision for operation in two modes; reduced effect of high temperatures and vacuum on reactor components. 7 cl, 1 dwg
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Authors
Dates
1996-10-20—Published
1994-02-10—Filed