Nuclear Science and Engineering / Volume 18 / Number 4 / April 1964 / Pages 508-513
Technical Paper / dx.doi.org/10.13182/NSE64-A18769
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A previous work on the closed-loop dynamics of nuclear rocket engines with bleed turbine drive3 is modified to study the engine dynamics using a topping turbine system. Root locus considerations show that the response characteristics of the two engine systems should be similar, although the topping turbine system has a faster initial response but slower asymptotic response. These conclusions are corroborated by analog simulation of the non-linear dynamic equations.