RU2000104682A - METHOD FOR STARTING NUCLEAR MISSILE ENGINES BASED ON RESONANCE - DYNAMIC DIVISION AND SYNTHESIS REACTIONS - Google Patents
METHOD FOR STARTING NUCLEAR MISSILE ENGINES BASED ON RESONANCE - DYNAMIC DIVISION AND SYNTHESIS REACTIONSInfo
- Publication number
- RU2000104682A RU2000104682A RU2000104682/06A RU2000104682A RU2000104682A RU 2000104682 A RU2000104682 A RU 2000104682A RU 2000104682/06 A RU2000104682/06 A RU 2000104682/06A RU 2000104682 A RU2000104682 A RU 2000104682A RU 2000104682 A RU2000104682 A RU 2000104682A
- Authority
- RU
- Russia
- Prior art keywords
- fission
- nuclei
- synthesis
- energy
- speed
- Prior art date
Links
- 238000003786 synthesis reaction Methods 0.000 title claims 16
- 210000004940 Nucleus Anatomy 0.000 claims 15
- 230000004992 fission Effects 0.000 claims 14
- 230000015572 biosynthetic process Effects 0.000 claims 12
- 230000002194 synthesizing Effects 0.000 claims 12
- 238000006243 chemical reaction Methods 0.000 claims 7
- 230000004927 fusion Effects 0.000 claims 6
- 238000010584 magnetic trap Methods 0.000 claims 5
- 230000000977 initiatory Effects 0.000 claims 2
- 210000002381 Plasma Anatomy 0.000 claims 1
- 230000001133 acceleration Effects 0.000 claims 1
- 230000003247 decreasing Effects 0.000 claims 1
- 229910052805 deuterium Inorganic materials 0.000 claims 1
- YZCKVEUIGOORGS-OUBTZVSYSA-N deuterium Chemical compound [2H] YZCKVEUIGOORGS-OUBTZVSYSA-N 0.000 claims 1
- 238000001704 evaporation Methods 0.000 claims 1
- 238000000034 method Methods 0.000 claims 1
- 229910052722 tritium Inorganic materials 0.000 claims 1
- YZCKVEUIGOORGS-NJFSPNSNSA-N tritium Chemical compound [3H] YZCKVEUIGOORGS-NJFSPNSNSA-N 0.000 claims 1
Claims (1)
Соотношение радиусов: RAЗ > Rp = Mp · Vp/(Zp · Вp)
Определение релятивистской массы ВП: Мp = Zp · Вp · Мi/(Zi · Bi);
где RAЗ - радиус A3 магнитной ловушки;
Rp - ларморовский радиус ВП (ларморовский радиус уменьшается при снижении энергии);
Мp, Мi - релятивистская масса ВП и выбранного типа исходных ядер синтеза; Vp - скорость ВП;
Zp, Zi - заряд ВП и выбранного типа исходных ядер синтеза;
Вp, Вi - напряженность магнитного поля в месте вращения ВП и выбранного типа исходных ядер синтеза;
νp, νi - ларморовская частота вращения ВП и выбранного типа исходных ядер синтеза;
С - скорость света;
m - масса протона;
mp - релятивистское приращение массы;
Δm - релятивистское приращение массы;
Δm/mp+1 - масса, которая должна соответствовать исходному ядру синтеза (например, дейтерию его масса равна 2 протонам, следовательно Δm = mp и тогда Δm/mp+1 = 2).A method for initiating a nuclear resonance-fission nuclear reaction with additional thermonuclear fusion neutrons is that the fissile material is ionized and moved by rotation inside the magnetic trap at the speed of its resonant fission when it collides with thermal neutrons emerging from the moderator surrounding the reactor core, while under the action of high-energy fission products initiate thermonuclear fusion reactions, and the resulting high-energy fission products and synthesis and they direct it to the engine output nozzle to create reactive thrust, characterized in that at the initial time when there are no fission nuclei in the reactor core and the initial synthesis nuclei, the initial products of fission and synthesis reactions are introduced into the reactor core, then, after reaching the specified concentration and the required ratio between fission and fusion nuclei, high-energy protons are introduced into the magnetic trap during the initiation of fission and fusion reactions and rotate them inside it under the influence of a magnetic field, forcing I, during the entire time that they are trapped, pass through the vapor or gas contained in it from fissile material and the original fusion nuclei and thereby initiate the occurrence of nuclear reactions in them with the emission of neutrons, such as fission, evaporation of neutrons from excited fission nuclei and tritium, etc., the fast neutrons emitted in this way are sent to the moderator and slow them down to thermal energies, after which the obtained thermal neutrons are directed inside the magnetic trap, in addition to generating fast neutrons, High-energy protons rotating inside the reactor core ionize fission and fusion nuclei and, due to this, provide the beginning of their drift rotation under the influence of crossed electric and magnetic fields, with a speed providing resonant-dynamic fission of fissile material, while the energy - speed - relativistic mass of high-energy protons introduced into the reactor core, set so that their cyclotron speed in the magnetic field of the trap coincides with the cyclotron at the rotational speed of the selected type of the initial synthesis nuclei located in the axial region of the magnetic trap, which will provide collisionless energy transfer of high-energy protons by generating electromagnetic and magnetoacoustic waves directly to the original synthesis nuclei, and in addition, the energy of high-energy protons will be transferred to the synthesis nuclei due to collective collisionless, plasma processes - instabilities such as: two-stream, turbulent, etc., after acceleration of fission and synthesis reactions, the supply of high-energy protons to the reactor core is stopped or can be continued if it is necessary to further reduce the critical density of the fissile material, if the fission or synthesis reactions are insufficient, if additional energy is needed, as well as when the reaction is completely excluded from the joint reaction, synthesis or fission reactions, so that the high-energy protons introduced into the active zone do not fall on the walls of the reactor, their Larmor rad the jus should not exceed the radius of the active zone, while the energy - speed - relativistic mass of high-energy protons, as well as the Larmor frequency of their rotation and rotation of the synthesis nuclei located in the axial region of the active zone, are determined by the following relations
The ratio of the radii: R AZ > R p = M p · V p / (Z p · V p )
Determination of the relativistic mass of VP: M p = Z p · V p · M i / (Z i · B i );
where R AZ - radius A3 of the magnetic trap;
R p - Larmor radius of the airspace (Larmor radius decreases with decreasing energy);
M p , M i - relativistic mass of VP and the selected type of initial synthesis nuclei; V p - speed VP;
Z p , Z i is the charge of the VP and the selected type of the initial synthesis nuclei;
In p , In i - the magnetic field strength at the place of rotation of the VP and the selected type of the original synthesis nuclei;
ν p , ν i - Larmor frequency of rotation of the VP and the selected type of the initial synthesis nuclei;
C is the speed of light;
m is the mass of the proton;
m p - relativistic mass increment;
Δm is the relativistic mass increment;
Δm / m p +1 is the mass that should correspond to the original nucleus of the synthesis (for example, its deuterium mass is 2 protons, therefore Δm = m p and then Δm / m p +1 = 2).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000104682/06A RU2182260C2 (en) | 2000-02-29 | 2000-02-29 | Method for starting nuclear rocket engines based on resonant-dynamic fission and fusion reactions |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000104682/06A RU2182260C2 (en) | 2000-02-29 | 2000-02-29 | Method for starting nuclear rocket engines based on resonant-dynamic fission and fusion reactions |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2000104682A true RU2000104682A (en) | 2000-09-10 |
RU2182260C2 RU2182260C2 (en) | 2002-05-10 |
Family
ID=20231110
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2000104682/06A RU2182260C2 (en) | 2000-02-29 | 2000-02-29 | Method for starting nuclear rocket engines based on resonant-dynamic fission and fusion reactions |
Country Status (1)
Country | Link |
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RU (1) | RU2182260C2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2566620C2 (en) * | 2013-12-24 | 2015-10-27 | Сергей Николаевич Зубов | Method and fuel for compound-synthesis, air jet engine running on compound-synthesis and turbomachine unit to this end (versions) |
-
2000
- 2000-02-29 RU RU2000104682/06A patent/RU2182260C2/en not_active IP Right Cessation
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