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Aerospace Nuclear Science & Technology
Organized to promote the advancement of knowledge in the use of nuclear science and technologies in the aerospace application. Specialized nuclear-based technologies and applications are needed to advance the state-of-the-art in aerospace design, engineering and operations to explore planetary bodies in our solar system and beyond, plus enhance the safety of air travel, especially high speed air travel. Areas of interest will include but are not limited to the creation of nuclear-based power and propulsion systems, multifunctional materials to protect humans and electronic components from atmospheric, space, and nuclear power system radiation, human factor strategies for the safety and reliable operation of nuclear power and propulsion plants by non-specialized personnel and more.
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Conference on Nuclear Training and Education: A Biennial International Forum (CONTE 2025)
February 3–6, 2025
Amelia Island, FL|Omni Amelia Island Resort
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Christmas Night
Twas the night before Christmas when all through the houseNo electrons were flowing through even my mouse.
All devices were plugged in by the chimney with careWith the hope that St. Nikola Tesla would share.
J. Ongena, A. M. Messiaen
Fusion Science and Technology | Volume 49 | Number 2 | February 2006 | Pages 425-440
Technical Paper | Plasma and Fusion Energy Physics - Fusion Reactor Issues | doi.org/10.13182/FST06-A1142
Articles are hosted by Taylor and Francis Online.
The total amount of heating power coupled to the plasma Ptot and the energy confinement time are determining parameters for realizing the plasma conditions suitable for the reactor. We recall that the ignition condition can be expressed by the following condition on the triple fusion product :NT = Ptot2/3 Vol = 3N2T2Vol/Ptot > (NT)ignition (1)with T ~= 15keVwhere = E/Ptot is the energy confinement time, E = 3NT Vol for an isothermal plasma with Ti = Te = T and a plasma volume Vol; N is the plasma density. The value T ~= 15 keV corresponds to the minimum value of (NT)ignition as a function T (see Fig. 1). In the present discussion for the sake of simplicity, we neglect density and temperature profile factors. The heating power in most of the present experiments is given by Ptot = POH + Padd where POH is the ohmic power and Padd is the additional heating due to neutral beam injection or R.F. heating. At ignition, the additional heating power must come completely from the energetic particles produced by the fusion reactions and we must have Ptot = P if we neglect the residual POH and the plasma losses by Bremsstrahlung (PBr [is proportional to] N2T1/2).