LT RBR:

34
LT RBR: Long Term Radiation Belt Remediation Joshua Davis ASTE 527 Space Concepts Studio

description

LT RBR:. Long Term Radiation Belt Remediation. Joshua Davis ASTE 527 Space Concepts Studio. LT RBR:. RBR means removing the trapped electrons and ions from the near Earth environment for the benefit of manned and unmanned spacecraft. Radiation Environment’s Impact on Manned Spaceflight. - PowerPoint PPT Presentation

Transcript of LT RBR:

Page 1: LT RBR:

LT RBR:Long Term Radiation Belt Remediation

Joshua DavisASTE 527

Space Concepts Studio

Page 2: LT RBR:

LT RBR:RBR means removing the trapped electrons and ions from the near Earth environment for the benefit of manned and unmanned spacecraft.

Page 3: LT RBR:

Radiation Environment’s Impact on Manned Spaceflight

A majority of the radiation Astronauts receive on orbit is attributed to the trapped radiation particles in the inner Van Allen belt.

Time on orbit is limited by an Astronaut’s total radiation exposure, limiting the ability to study long term micro-gravity effects on Humans.

Temporary and permanent eye damage.

Increased risk of cancers as well as heart, digestive, and respiratory diseases.

The daily dosage of radiation on the ISS is equal to 8 chest X-rays per day.

Career exposure cannot exceed 3 percent risk of exposure-induced death (REID) at a 95% confidence level.

NASA Career Exposure Limits Male Female

25 Years Old 52 rem 37 rem

55 Years Old 147 rem 112 rem

Average annual exposure on the Earth’s surface is .125 rem/year, on board ISS during solar maximum is .1 rem/day

Page 4: LT RBR:

Solar array power decrease due to radiation damage

Single event effects in microelectronics: bit flips, fatal latch-ups

Spacecraft components become radioactive

False stars in star tracker CCDs before after

Surface degradation from radiation

Electronics degrade due to total radiation dose

Solar array arc discharge

Cryogenic systems experience notable charged particle heating

Electromagnetic pulse from vehicle discharge

Induced Voltage

Time

Energetic Particle & Plasma Hazards

Page 5: LT RBR:

Energetic Particle & Plasma Hazards

Arc Discharging

Page 6: LT RBR:

Energetic Particle & Plasma Hazards

Solar Panel Power Decrease

Page 7: LT RBR:

Energetic Particle & Plasma Hazards

Bit Flips/Single Event Upsets

Page 8: LT RBR:
Page 9: LT RBR:

Particle Motion in Earth’s Magnetic Field

Page 10: LT RBR:

Radiation Belts are Highly Dynamic

Page 11: LT RBR:

Radiation Belts are Highly DynamicVideo reconstructing belts with SAMPEX data from Oct 18, 2003 to Jan 1, 2004

http://www.youtube.com/watch?v=QwNNh4c9bR0

Oct 25 Oct 27

Oct 30 Nov 3

Page 12: LT RBR:

Natural Remediation

1 10 100 1000 10000

Total Trapped Particles

Time (Days)

Parti

cle C

ount

1 10 100 1000 10000

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

Solar or Nuclear Events

Page 13: LT RBR:

How RBR Works:Change the particle’s pitch cone angle such that its velocity vector is pointed roughly parallel to the magnetic field lines.

Page 14: LT RBR:

VLF:Very Low Frequency Radio Waves

Ground Based

Space Based

Page 15: LT RBR:

Experimental Data for Ground Based VLF RBR

Increase in loss-cone electron flux during VLF operation

Ambient flux conditions

Page 16: LT RBR:

AFRL DSX to test Space Based VLF RBR

“The overall primary objective of DSX is to resolve critical feasibility issues of injecting VLF waves into the magnetosphere to determine how efficiently, how effectively, and to what degree of efficacy this can be accomplished. The goal is to assess the particle distribution, perturbations, and scattering effects on the particles as a result of the VLF waves produced by nature and by man-made systems on the ground and in space.”

Page 17: LT RBR:

Starfish Prime – High Altitude Nuclear Explosion

Crippled 1/3 of operational satellites and disabled 7 satellites in the months that followed due to the particles injected into the radiation belts, some of which persisted for 5 years.

“It has been suggested that even a “small” HANE (~10–20 kilotons) occurring at altitudes of 125–300 km would raise peak radiation fluxes in the inner radiation belt by 3–4 orders of magnitude, and lead to the loss of 90% of all low-Earth-orbit satellites within a month [Dupont, 2004].”

“the manned space program would need to be placed on hold for a year or more”

Page 18: LT RBR:

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

1 2 3 4 5 6 7

Total Trapped Particles

Time

Parti

cle C

ount

Rapid Response Remediation

Solar or Nuclear Event

Occurs

Particles Remain

Event Ends

Rapid Remediation Occurs

Ionospheric Distortion Begins Ionospheric Distortion Subsides

Page 19: LT RBR:

Issues with RBR

Page 20: LT RBR:

2 4 6 8 10 12 14 16 18 20

Ionogram (with Turbulence)

Frequency (MHz)

Heig

ht

Page 21: LT RBR:

Radio Communication Fade vs. Solar Cycle – Thule

Page 22: LT RBR:

1 10 100 1000 100000.3

0.7

1.1

1.5

1.9

2.3

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 10 100 1000 100001.5

2

2.5

3

3.5

4

4.5

Total Trapped Particles

Time (Days)

Parti

cle C

ount

1 10 100 1000 100000.3

0.7

1.1

1.5

1.9

2.3

Particle Flux In/Out

Time (Days)

Parti

cle C

ount

1 10 100 1000 100001.5

2

2.5

3

3.5

4

4.5

Total Trapped Particles

Time (Days)

Parti

cle C

ount

Enhanced Remediation vs. Natural Remediation

Long Term Radiation Belt Remediation

Page 23: LT RBR:

Conclusion and Future Work for LT RBR

VLF ground based architecture study for geographic locations of interest

Feasibility study of Long Term operation of VLF stations (power, cost, effectiveness)

Page 24: LT RBR:

References

• Odenwald, Sten. "What Are Space Radiation Effects?" NASA. <http://radbelts.gsfc.nasa.gov/outreach/effects.html>.

• Hess, Wilmot N. "Energetic Particles in the Inner Van Allen Belt." Space Science Reviews 1.2 (1962). <http://rd.springer.com/article/10.1007%2FBF00240580>

• Hoyt, Robert P., and Forward, Robert L. "Radiation Remediation." Tethers Unlimited. <http://www.tethers.com/HiVOLT.html>.

Page 25: LT RBR:

References Cont.

• Gamble, Rory. Et al. "Radiation Belt Electron Precipitation by Man-made VLF Transmissions." Journal of Geophysical Research 113 (2008): American Geophysical Union, 21 Oct. 2008. <http://www.agu.org/pubs/crossref/2008/2008JA013369.shtml>.

• Rodger, Craig J. "The Atmospheric Implications of Radiation Belt Remediation." Annales Geophysicae 24 (2006). European Geosciences Union. <http://www.ann-geophys.net/24/2025/2006/angeo-24-2025-2006.pdf>.

Page 26: LT RBR:

References Cont.• Basu, Santimay, and MacKenzie, E. “Ionospheric constraints

on VHF/UHF communications links during solar maximum and minimum periods” Radio Science 23 (1988): American Geophysical Union, 17 Jan. 1988. <http://www.agu.org/journals/rs/v023/i003/RS023i003p00363/RS023i003p00363.pdf>.

• Scherbath, Mark. Et al. "AFRL's Demonstration and Science Experiments (DSX) mission", Proc. SPIE 7438, Solar Physics and Space Weather Instrumentation III, 74380B (September 23, 2009); doi:10.1117/12.824898; <http://dx.doi.org/10.1117/12.824898>

Page 27: LT RBR:

Backup Slides

Page 28: LT RBR:
Page 29: LT RBR:

Why does the Earth have a Radiation Belt?

A Radiation Belt ismore stylish thanRadiation Suspenders!

Page 30: LT RBR:

Tethers Unlimited : HiVOLT

Page 31: LT RBR:

Neutral Particle InjectionIon-Cyclotron Turbulence Generation

Page 32: LT RBR:

Natural Remediation - AnalogyWater is poured into the top of the bucket and exits through a porous plug at the bottom of the bucket.

If the rate of water being poured into the system increases, the water level rises until the pressure causes an equilibrium condition

If there is no water, there is still a bucket.

The radiation belts work in a similar fashion, the more particles coming into the system, the more particles come out of the system.

However, particles in the belts can become stuck for months or years, so equilibrium takes a very long time to reach after an event.

Just as with the bucket, if there are no particles in the radiation belt, the protective magnetosphere is unaffected

Page 33: LT RBR:

2 4 6 8 10 12 14 16 18 20

Ionogram

Frequency (MHz)

Heig

ht

Increasing Density

Page 34: LT RBR:

Radio Communication %Fade vs. Solar Cycle – Ascension Island