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Proving DRACO will deliver
The United States is now closer than it has been in over five decades to launching the first nuclear thermal rocket into space, thanks to DRACO—the Demonstration Rocket for Agile Cislunar Orbit.
Osamu Mitarai, Akira Hirose, Harvey M. Skarsgard
Fusion Science and Technology | Volume 16 | Number 2 | September 1989 | Pages 197-210
Technical Paper | Plasma Engineering | doi.org/10.13182/FST89-A29148
Articles are hosted by Taylor and Francis Online.
The concept of a generalized ignition contour map, showing , nτE, and T, is extended to the realistic case of a plasma with temperature and density profiles in order to study access to ignition in a tokamak reactor ( is the average total auxiliary heating power density). The “generalized” saddle point, which corresponds to the minimum height of , is found to lie between the Lawson and ignition conditions. If the height of the operation path with Goldston L-mode scaling is higher than the generalized saddle point, a reactor can reach ignition with this scaling for the case with no confinement degradation effect due to alpha-particle heating. In this sense, the saddle point given in a general form is a new criterion for reaching ignition. Peaking the profiles for the plasma temperature and density can lower the height of the generalized saddle point and help a reactor to reach ignition. With this in mind, we can judge whether next-generation tokamaks, such as Compact Ignition Tokamak, Tokamak Ignition/Burn Experimental Reactor, Next European Torus, Fusion Experimental Reactor, International Tokamak Reactor, and AC Tokamak Reactor, can reach ignition with realistic profile parameters and an L-mode scaling law. We can also obtain the required confinement enhancement factor with respect to L-mode scaling for reaching ignition. The confinement degradation effects on the operation path due to alpha heating are also considered.