high energy propulsion
DESCRIPTION
High Energy Propulsion. Brice Cassenti University of Connecticut. High Energy Propulsion. Fusion Annihilation Photon. Fusion Energy. Binding energy Reactions Propulsion. Binding Energy. Some Fusion Reactions. Nuclear Reactions. DT Fusion Reaction Uranium Fission Lithium Fission. - PowerPoint PPT PresentationTRANSCRIPT
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High Energy Propulsion
Brice CassentiUniversity of Connecticut
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High Energy Propulsion
• Fusion• Annihilation• Photon
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Fusion Energy
• Binding energy• Reactions• Propulsion
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Binding Energy
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Some Fusion Reactions(1)
2 1D +
3 1T →
4 2He ( 3.5 MeV ) + n0 ( 14.1 MeV )
(2i) 2 1D +
2 1D →
3 1T ( 1.01 MeV ) + p+ ( 3.02 MeV )
50%
(2ii)
→ 3 2He ( 0.82 MeV ) + n0 ( 2.45 MeV )
50%
(3) 2 1D +
3 2He →
4 2He ( 3.6 MeV ) + p+ ( 14.7 MeV )
(4) 3 1T +
3 1T →
4 2He
+ 2 n0
+ 11.3 MeV
(5) 3 2He +
3 2He →
4 2He
+ 2 p+
+ 12.9 MeV
(6i) 3 2He +
3 1T →
4 2He
+ p+ + n0
+ 12.1 MeV
51%
(6ii)
→ 4 2He ( 4.8 MeV ) +
2 1D ( 9.5 MeV )
43%
(6iii)
→ 4 2He ( 0.5 MeV ) + n0 ( 1.9 MeV ) + p+ ( 11.9 MeV ) 6%
(7i) 2 1D +
6 3Li →
2 4 2He
+ 22.4 MeV
(7ii)
→ 3 2He +
4 2He
+ n0
+ 2.56 MeV
(7iii)
→ 7 3Li + p+
+ 5.0 MeV
(7iv)
→ 7 4Be + n0
+ 3.4 MeV
(8) p+ + 6 3Li →
4 2He ( 1.7 MeV ) +
3 2He ( 2.3 MeV )
(9) 3 2He +
6 3Li →
2 4 2He
+ p+
+ 16.9 MeV
(10) p+ + 11 5B →
3 4 2He
+ 8.7 MeV
http://en.wikipedia.org/wiki/Nuclear_fusion
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Nuclear Reactions
• DT Fusion Reaction
• Uranium Fission
• Lithium Fission
10
42
31
21 nHeHH
10
23892
10 2
21
1nXXUn N
kN
k
31
42
63
10 HHeLin
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Fusion Reactions
• The DT reaction
• And Lithium fission reaction
• Are equivalent to
10
42
31
21 nHeHH
31
42
63
10 HHeLin
42
42
63
2 HeHeLiH1
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Reaction Cross-Section
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Reaction Kinetics
• Rate -
• Parameter -
• Velocity depends on temperature
–
– k is Boltzmann’s constant
nv
v
kTmv2
3
2
1 2
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Thermonuclear Weapon
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Magnetic Confinement Fusion PowerTokamak
http://upload.wikimedia.org/wikipedia/commons/4/4b/Tokamak_fields_lg.png
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Magnetic Confinement Fusion PowerMirror
http://www.google.com “magnetic mirror nuclear fusion reactor pictures”
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Inertial Confinement Fusion Power
The stages of inertial confinement fusion:
1. Laser beams or laser-produced X-rays rapidly heat the surface of the fusion target, forming a surrounding plasma envelope.
2. Fuel is compressed by the rocket-like blowoff of the hot surface material. 3. During the final part of the capsule implosion, the fuel core reaches 20 times the density
of lead and ignites at 100,000,000 ˚C. 4. Thermonuclear burn spreads rapidly through the compressed fuel, yielding many times
the input energy.
The blue arrows represent radiation; orange is blowoff; purple is inwardly transported thermal energy.
http://en.wikipedia.org/wiki/File:Inertial_confinement_fusion.svg
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Fusion Rockets
• Magnetic Mirror– End fields unequal: preferential exhaust
• Tokamak– Power to expel high speed plasma
• Inertial Confinement– Magnetic nozzles align pellet products
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Orion
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Daedalus StudyBritish Interplanetary Society
From Nicolson “The Road to the Stars”
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Daedalus
http://www.grc.nasa.gov/WWW/PAO/images/warp/warp44.gif
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Medusa
http://en.wikipedia.org/wiki/File:MedusaNuclearPropulsionOperatingSequenceDrawing.png
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Medusa
Specific Impulse:100,000-500,000
http://en.wikipedia.org/wiki/File:MedusaNuclearPropulsionOperatingSequenceDrawing.png
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Matter-Antimatter Annihilation
ee
Positron-Electron Annihilation
nnmpp 0
nnmpn )1(0
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Antiproton-Uranium Nucleus Annihilation
+
p
p
n
knXUp 223892
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Courtesy of G. Smith
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Pellet Ignition
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Tritium Fuel Considerations
• Tritium is naturally radioactive– Beta decay– Half-life ~12 years
• Tritium requires cryogenic storage• Lithium-6 is not radioactive• Lithium-6 does not require cryogenic storage
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Pellet Construction
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Hybrid Fusion-Fission Nuclear Pulse Propulsion
• Use of Li6 – Reduces tritium handling problems– Decreases specific impulse
• System can be developed in a two step process– Use fusion to boost the specific impulse of a pulse
fission rocket– Evolve to a full hybrid system
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Typical PelletGeometry
• Core radius 0.05 mm• Fuel Radius 1.00 cm• Tungsten Shell Thickness 0.10 mm• Antiproton Beam Radius 0.10 m• Uranium Hemisphere Radius 0.30 mm
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Typical Pellet Performance
• Antiproton Pulse 2x1013 for 30 ns• Maximum Field 24 MG• Pellet Mass 3.5 g• Specific Impulse
– 600,000 s for 100% fusion– 200,000 s for 10% fusion– 3,000 s for contained fusion
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Exotic Propulsion Alternatives
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Sanger Electron-PositronAnnihilation Rocket
By G. Matloff
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Proton-Antiproton Reaction
nnmpp 0
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Proton-Antiproton Reaction
nnmpp 0
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Proton-Antiproton Reaction
nnmpp 0
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Proton-Antiproton Reaction
nnmpp 0
ee
ee
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Proton-Antiproton Reaction
nnmpp 0
ee
ee
+
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Proton-Antiproton Reaction
nnmpp 0
ee
ee
+
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Pion Rocket
By R. ForwardIsp: 10,000,000 sec
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References• Kammash, T., (editor), Fusion Energy in Space Propulsion, Volume 167 Progress in
Astronautice and Aeronautics, American Institute of Aeronautics and Astronautics, Washington, DC,, 1995.
• Kammash, T, Fusion Reactor Physics, Ann Arbor Physics, Inc. Ann Arbor, MI, 1976.• Manheimer, W.M., An Introduction to Trapped-Particle Instability in Tokamaks,
Energy Research and Development Administration, Washington, DC, 1972.• Miley, G.K., Fusion Energy Conversion, American Nuclear Society and U.S. Energy
research and Development Administration, Chicago, 1976.• Miyamoto, K., Plasma Physics for Nuclear Fusion, The MIT Press, Cambridge, MA,
1987.• Vedenov, A.A., Theory of Turbulent Plasma, National Aeronautics and Space
Administration, National Science Foundation, and Isreal Program for Scientific Translations, Jerusalem, 1966.