Monday, January 29, 2007

Repurpose NEOs

Purpose of the Asteroidal Volume is to suggest ways of exploiting this incredible resource to benefit of all humankind. Purpose of this chapter is to present some background material about Near Earth Objects (NEOs), the most available asteroids and comets. 

Ultimately, humanity should welcome Near Earth Objects (NEOs) as an excellent resource for constructing habitats in space. Towards this end, there will be a series of projects increasing in difficulty until we eventually gain enough experience to actually mine the asteroids and accomplish the construction.  Thus, it makes sense to do the easiest task first and progress from there.
TE arbitrarily assumes least difficulty for the task of transporting a radio beacon to a Near Earth Asteroid (NEA), and mounting it in such a way to enhance reception by Earth bound sensors.  At first glance, this task seems sufficiently straightforward enough to be an excellent science fair project for enthusiastic students. 
Perhaps this science project could have following objectives:
  1. Monitoring signal could teach a number of things about doppler effect, ranging.
  2. All projects require the collection of lessons learned for future missions. Subsequent projects require the review of these lessons as part of the project planning process.
  3. Thus, subsequent NEA missions could add beacons with enhanced capabilities.
It's not surprising to find out that the professionals have been considering this "science project" for a long time.
Beacon for an Asteroid
Perhaps ion or plasma propulsion can actually change an asteroid's orbit; there would a compelling reason to demonstrate how this concept if an asteroid was going to impact the Earth.  Thus, NASA had a meeting of relevant experts (including: Dr. Edward Lu; Piet Hut, Institute for Advanced Studies; Rusty Schweickart, former astronaut) which led to the B612 Foundation.
REASON: Asteroid approaches Earth in a couple of decades.
In 2029, the asteroid, 2004 MN4, will pass within 4 Earth radii away (this is closer then many of our satellites; for example, geosynchronous satellites are almost 5 radii above Earth's surface).  While close enough for a great show, there shouldn't be an impact; however, 2004 MN4 will pass close enough for the Earth's gravity to change its orbit. 
In 2029, Apothis will pass near Earth,
well inside Moon's orbit
Thus, B612 Foundation is really interested in the asteroid's subsequent orbital path.  Current calculations indicate that about 2035, 2004 MN4 will again fly near the Earth with a remote chance of an actual impact.  It would be nice to know for sure.  
Put Transmitter on Asteroid  Thus, there is a compelling reason to mount a beacon on 2004 MN4.  It is only 300 meters in diameter; so, a radio beacon would be an invaluable tracking aid. Much like FAA's ubiquitous system of transponders on all large aircraft, NASA needs a radio transmitter on 2004 MN4 to monitor its exact location. 
Rusty Schweiker: "In the very unlikely case, this thing is going to hit us, this’ll tell you whether or not it will (most likely not); but, if in fact it is not going to hit us, you still have a very scientifically interesting mission out there. You can see what this thing is made of, what its surface structure is like, what it might be like to land on one of these things later, if you have to move another one. It tells you a lot about the properties of asteroids; so, this mission won’t go to waste ....."
Apothis approaches Earth in 2029 and returns in 2036.
Tentative Schedule. The mission should launch around 2012/2013.  If the probe takes a year or so to get there, then, you'll likely know within a year if the impact is imminent. If it is going to hit us; that puts us at 2015 with 14 years to do something about it (recall flyby Earth in 2029). Then, we get the compelling reason to put the plasma propulsion concept to work, a much more ambitious mission: "push" an asteroid into an orbit which won't impact Earth. It’ll take some years to prepare the spacecraft; get it ready to launch, test it; then, actually fly the mission.
Apophis is an approximately 400-metre 'near-Earth object' (NEO), which will come closer than 36,000 km to Earth in 2029 - inside the the orbit of many satellites. On that pass, the asteroid will be gravitationally perturbed to an unknown orbit, one that could cause it to hit Earth in 2036.
 "While the odds are very slim that this particular asteroid will hit Earth in 30 years, they are not zero.  Apophis and other NEOs represent threats that need to be addressed," said Rusty Schweickart, Apollo astronaut who now heads the NEO committee of the Association for Space Explorers.  
If Apophis passes through a several hund red-metre wide "keyhole" in 2029, it will impact Earth in 2036. With such a severe impact, it makes sense to augment Earth-based observations of Apophis with much closer sensor measurements to determine if a deflection mission is required. The tagging mission must complete before 2017 space agencies can determine if they must deflect the asteroid from the keyhole.
Another Approach.  Much like amateur astronomy has made enormous contributions to astronomy, there is plenty of room for rookie researchers to work this problem. The Planetary Society, non-profit organization dedicated to space research, conducted their Apophis Mission Design Competition, an open contest for best design of a tagging mission to mark and track Apothis. The Society paid $50,000 in prize money for the winning proposal.
http://www.phenomenica.com/2010/07/massive-asteroid-may-hit-earth-in-2182.html
Bruce Betts, The Planetary Society's Director of Projects: "This competition generated creative thinking about tagging Apophis and stimulated greater awareness of the broader near-Earth object threat."

 
A much bigger Near Each Asteroid (NEA)  is hurtling towards the Earth, and NASA is considering sending a probe. This asteroid , 1999 RQ36, has a slight chance (1-in-1,000) of hitting Earth before the year 2200, but the consequences of the collision could be severe, destruction equivalent to detonating hundreds of nuclear bombs. NASA has officially classified RQ36 as a "potentially hazardous asteroid" as it passes within about 280,000 miles of Earth. However, on the plus side, this proximity makes it easier to reach than other asteroids.
NASA analysts predict the most likely impact date as September 24, 2182, but scientists want to forecast its trajectory more accurately. If NASA decides to proceed, the spacecraft could launch in 2106 to collect data from the 1,800 feet-wide asteroid.
Ideas for further content:
1. Plasma propulsion to move asteroids. Chicken or egg analogy. Which task will will plasma propulsion do first? 
---move asteroids for safety or for harvest
---shuttle passengers/cargo between asteroids.
2. Network of radio transceivers to monitor potential impactors even if too small to see or hidden behind Sol.
3. Metaphorically, putting a beacon on an asteroid is like putting a bell on a cat.
Risk vs. Opportunity.  Near Earth Objects (NEOs)present much more opportunity then risk.  Most NEOs present absolutely no risk at all because their trajectories do not impact the Earth ever.  These NEOs are pure opportunity to harvest at will; the only risk is that we'll refuse to harvest them at all.  For the very few NEOs which will impact the Earth; they present an imperative for ASAP harvesting before they present any danger.
Asteroids have impacted Terra in the past (many times) and the chances are pretty good that more impacts are likely (or near impacts if our technology advances enough to avoid this Doomsday scenario). However, the probability of an impact during any particular year (in absence of observed data) is very slight, while the probability of NEOs passing near us will remain very great. These NEOs provide much more opportunity then risk. Simple logic will eventually compel relevant decision makers to realize that the source of materials for habitats in space must come from NEOs. At least, the initial habitats will need the mass from these NEOs. As humans build initial habitats from NEOs, then later phase of habitats will be able to use materials from further away asteroids.
There are numerous sources of NEO information available on the web, following is a very small sample of perhaps the better ones.
1. Study to Determine the Feasibility of Extending the Search for NEOs.

NASA Releases Near-Earth Object Search Report 
In 1998, NASA joined the "Spaceguard" effort to discover and track over 90% of the near-Earth objects larger than one kilometer by the end of 2008. There has been good progress toward eliminating the risk of any large, undetected impactor which could cause global damage; however, there are many more objects with diameter less then 1 km.
In 2003, NASA released a technical report on potential future search efforts for smaller near-Earth objects. Assuming that larger NEOs (greater then 1 kilometer in diameter) have mostly been detected, NASA tasked this report's Science Definition Team to determine ways to find smaller near-Earth objects (less than 1 km). Smaller objects could cause significant regional damage and constitute a long-term hazard. Thus, smaller objects are much less hazardous then larger objects; however, smaller objects are much more numerous and the likelihood is therefore much greater of an impact from a smaller NEO. Thus, the importance of detecting them is just as great as for the larger objects.
Content for this report was produced by the Science Definition Team. chaired by Dr. Grant Stokes of the MIT Lincoln Laboratory. These 12 eminent scientists studied and stated the feasibility of extending the search effort to the far more numerous, perhaps hundreds of thousands, of near-Earth objects with diameter less than one thousand meters.

2. The Watch provides, as a public service, NASA's March 2007 NEO Report to Congress.
NASA Administrator complied with Congressional direction and transmitted an initial report to Congress which:
(1) analyzes possible alternatives to survey near-Earth Objects (NEO), including groundbased and space-based alternatives with technical descriptions.
(2) recommends prefered options and proposed budget to accomplish the survey program. .
(3) analyzes possible alternatives to divert an object on a likely collision course with Earth.



3. NEAR-EARTH OBJECTS AS FUTURE RESOURCES 
While Near Earth Objects (NEOs), comets and asteroids, might possibly hazard the Earth someday in the distant future, they offer immediate, enormous benefits, their raw materials. It is not cost effective to mine these minerals and then bring them back to Earth. However, these raw materials could prove essential in developing spaceborne structures needed to explore and colonize our solar system in the twenty-first century. Mineral wealth in the belt of asteroids between the orbits of Mars and Jupiter could equal about 100 billion dollars for every person on Earth today. Whereas asteroids are rich in the mineral raw materials required to build structures in space, the comets are rich resources for the water and carbon-based molecules necessary to sustain life. In addition, an abundant supply of cometary water ice could provide copious quantities of liquid hydrogen and oxygen. It seems likely that when we begin to colonize the inner solar system, the metals and minerals found on asteroids will provide the raw materials for space structures, and comets will become the watering holes and gas stations for interplanetary spacecraft.
Reference: Lewis, John S. Mining the Sky: Untold Riches from the Asteroid, Comets, and Planets. Addison-Wesley, 1996.

4. Near-Earth Resources
Today's technologies can detect, track, categorize, and intercept objects which cross Earth's orbit; they can also access their rich storehouses of materials. Thus, mining a threatening NEO may complement a deflection scenario of a NEO which hazards the Earth. This converts the distant NEO threat to a near-Earth resource. NEOs can supply materials for a wide range of operations both in space and on Earth, as they likely contain large amounts of water, carbon, structural metals, industrial feedstocks of many types, and precious metals. This resource has low overhead for use in space; some known NEOs would require lower transportation energy expenditure than lunar resources. Mining a NEO inherently requires, among other things, altering the mass distribution of the body during exposure, removal, and processing of the ore. These processes can deflect the body from Earth impact by altering its orbital characteristics.
NEO mining contributes toward two important goals
1. Mitigation of a possible threat of NEO collision.
2. Ample resources for space exploration without expensive transport from Earth's intense gravity field.
This allows sequential mitigation of the NEO in a controlled manner while providing the resources contained within the NEO for use either in space or on Earth.
Both goals require optimizing many sources of knowledge. Two important ones are an extensive reconnaissance of the target NEO and the long history of terrestrial mining practice. Linked document discusses how current mining technology can adapt to mine NEOs, threatening or not. It summarizes our knowledge of NEO composition, physical properties, and mining and processing methods, and points out areas where further research, especially physical testing in space, is vital.

NASA NEO News: Open Letter to Congress on Near Earth Objects ...
Studies indicate that, with the commitment of modest resources, NEO impacts ..... ability to understand and use the vast and beneficial resources of space. ...www.spaceref.com/news/viewsr.html?pid=9866 - 46k - Cached - Similar pages
[PDF]
NEAR EARTH OBJECTS AS RESOURCES FOR SPACE INDUSTRIALIZATION
File Format: PDF/Adobe Acrobat - View as HTMLWingo D et al: “NEO Metals Resources and their value to the World Economy”, Space Front (Journal of the Space. Frontier Foundation) 

INTERSTELLAR COMMUNICATION: Maintain Contact




VOLUME I: ASTEROIDAL
VOLUME II: INTERPLANETARY
VOLUME III: INTERSTELLAR



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Can interstellar radio signals go directly from sender to receiver?? Even on Earth with transmission distances far less than one Light Year (LY), this basic method needs considerable augmentation. 
CURRENT EXAMPLES include "store and forward" technologies as well as numerous nodes which regenerate data packets and reroute data streams.Some such nodes orbit Earth as communications satellites (COMSATs).  
However, vast distances to other stellar systems introduce prohibitive delays, given light speed limitations. An immediate radio reply to nearest stars would take years; however, most stars would require generations to just converse. Some scholars have made an excellent point: "If it takes generations to just talk with entities on other stars, why not send manned probes???"

·        1974, B.S. from Harvey Mudd College (dual major, physics and psychology)
·        1978, J.D. from University of Santa Clara School of Law.  
Work history includes:
·       Late 1970s and early 1980s, published several editions of Lobbying for Space, the first space program political advocacyhandbook.
·        Co-edited the 1980 NASA feasibility analysis of self-replicating space factories
·        1996, authored the first detailed technical design study of a medical nanorobot ever published in a peer-reviewed mainstream biomedical journal.  
· Three separate observational SETA/SETI programs.
·  Research Fellow and Study Editor, NASA/ASEE Summer Study Programs, including Advanced Automation for Space Missions
· 
Co-founded the Nanofactory Collaboration (2000-now)
·        Senior Research Fellow, Institute for Molecular Manufacturing(IMM)
·        Member American Association for the Advancement of Science
·       Member, National Space Society
·      Research Scientist,  Zyvex Corporation
Thought Experiment's (TE's) Typical Interstellar Profile
ACCELERATION: G force propulsion for 1 year brings vessel to .6443 Lightspeed (c) and .38 Light Year (LY).
CRUISE:Ship turns off propulsion and spins for several years (as observed from Earth) until it reaches deceleration point.
DECELERATION: Once again, do G force propulsion for 1 year and .38LY to reduce vessel velocity to orbital speeds at destination stellar system.
Consistent Two Way Communications. Home base at Earth will want constant flow of scientific data gleaned from new vantage points far from our home star, Sol. Vessel occupants will want latest home news, latest developments in relevant fields of knowledge not to mention lessons learned from other interstellar missions. Also, they'll want as much entertainment as bandwidth will allow. 
Sadly, such huge data flows over such great distances (LYs) will likely prove problematic. 
How does an interstellar vessel consistently communicate with home base as well as established bases throughout other stellar systems?
We might insert beacons, interstellar communications capsules, in static positions between Sol and other stars. Deployed comm. capsules could regenerate signals much like repeaters in current Wide Area Networks (WANs).
Primary vessel (i.e., "mothership") could start deploying these comm capsules at selected points during cruise portion of flight. 
To maintain a constant position with respect to neighboring stellar systems, they must decelerate from cruise speed per the typical interstellar profile. 
EXAMPLE: In above diagram, planners arbitrarily decide to place comm. capsule at one LY from Sol.

Freitas authored Nanomedicine, a seminal, multi-volume, technical discussion of the potential medical applications of molecular nano-technology, published by Landes Bioscience.  
Home page has publication list of 617 items.
He has published 49 refereed journal publications and contributed book chapters, co-authored Kinematic Self-Replicating Machines(Landes Bioscience, 2004), 
Professional Awards include:
·        2006 Guardian Award from Lifeboat Foundation.  
Extensive research interests include:  
·        nano-medicine
·        medical nano-robotics design
·        molecular machine systems
·        diamondoid mechano-synthesis (theory and experimental pathways)
·        molecular assemblers and nano-factories
·        atomically precise manufacturing
·        self-replicating machine and factory systems.  
Patents include first ever filed on diamondoid mechano-synthesis (awarded on 30 March 2010)
Serves on the Editorial Boards of 9 technical journals.
HABITATS will likely start small with larger versions to follow Perhaps first Earth orbiting habitat might be Dr. O'Neill's Island 1, a cylindrical structure with radius of 225 m and spin rate of 12°/sec to simulate Earth gravity for about 10,000 occupants  inside of outer hull. Humanity will eventually build much larger habitats such as Island 3, which might house a million humans.
Islands in Space
In his book, The High Frontier, Colonies in Space, Dr. Gerald O'Neill states that Earth orbiting "habitats" will someday host many humans (perhaps millions). Others extrapolate this habitat concept to orbits around other planets and throughout the Solar System. Most materials to construct and support these habitats can come from asteroids and comets throughout the Solar System especially in the Kuiper Belt and the further out Oort Cloud.
For Earth Orbiting Habitats: Dr. O'Neill further assumes 
1) energy via sunlight reflected from large co-located mirrors
For interstellar habitatsTE assumes energy needs will be augmented from other sources, perhaps Helium -3 mined from Solar System's gas giant planets.  
2) artificial gravity via carefully controlled spin about vessel's longitudinal axis. NOTEWould still work for interplanetary and interstellar habitats.
3) extensive agriculture for food, breathable air, and pleasant environments.NOTEWould still work for interplanetary and interstellar habitats.
For Interstellar Cruises, An Island 3 habitat could fill the Mothership role. It's reasonable to assume that many Island 1 habitats could be carried and/or constructed to fill the comm capsule role.
Earth Based RF or Physical Probes...
...to nearby stars; which is better?
Bob Freitas expertly examines relevant issues 
(1) Do deployed probes cost more than an Earth bound radio frequency (RF) beacon? 
No! Cost for observable RF signals roughly equals probe cost over the duration of an entire exploration program.  Even better, if probe self-replicates, only one initial device need deploy for much less cost.
(2)Does interstellar probe flight take too much fuel? No! EXAMPLE: Probe might accelerate to 10%c; then, eventually decelerate back to zero. Such performance requires a mass-ratio (initial/final mass) of 5.0 for a fusion rocket, much less than ratio of 21 for the recent Space Shuttle.
(3) Is the Interstellar Probe way too expensive? No! Routine interstellar probes implies a highly advanced, well resourced society, e.g.,  Kardashev Type II society cost for interstellar, g-force vehicle compares to a current Saturn V orbital launch by us.(4) Should we divert probe launch resources for other societal uses?
No!
If active cosmic exploration is a priority; then, we must spend accordingly.
(5) Are interstellar flights slower than radio signals? Of course they are; however, probes don't waste time for radio messages to cycle between the stars. (6) Is probe technology too difficult? No! While RF tech is simpler, interstellar probes, are more capable. NOTE: Probes will likely include RF tech.
Recall that Snowball from Oort can quickly deploy with following advantages over the Mothership Method.
1) 7G acceleration to about .87c takes only 100 days; 7G deceleration is same duration.
2) Quicker cruise speed.
3) Artificial Intelligence (AI) Controlled by autonomous robots; i.e. much less human error.
4) With no humans, no need for associated life support, certainly no need for in-flight entertainment.
5) Such a vessel can quickly establish comm. capsule ; it can also quickly resupply an established capsule.
                          To establish beacons at 1 LY intervals, ABOVE EXAMPLE shows:
  1. A group of "snowballs" (ice encased beacons) accelerate in tandem.
  2. After 291 days of joint cruise, one snowball decelerates.
  3. Remaining beacons cruise jointly for another 456 (100+356) days; 1 more beacon decelerates.
  4. This goes on until we run out of snowballs or Light Years.
More Snowballs  A series of beacons between Sol and any destination star would definitely help two way communications Given inevitable signal attenuation due to great interstellar distances, a repeater beacon could receive RF signals, regenerate them, amplify them; then, re-transmit them to the next beacon or perhaps the intended receiver. 
Operational considerations include:
a. Onboard Power. After deployment, these capsules will need continuous power supply.  Thus, subsequent snowballs could reprovision these waystations.
b. Positional Stability. Track both Sol and destination star to maintain constant position.
c. Minimize Hazards. To avoid inflight collisions, they must track subsequent vessels, likely traveling at .65c (or even faster).
d. Emergency Waystations. If these relay stations were big enough they could even be used as "way stations" for vessels that needed such things. (perhaps emergencies or scientific observatories). 
(7) Does each probe require a dedicated RF listening antenna? No! Only one radio antenna system can simultaneously collect signals from all the probes. NOTE:Redundancy is good; so; use back up systems.(8) Does Inevitable Obsolescence Obviate Interstellar Probes? No! Of course, interstellar flight's lengthy duration means probes must use very mature tech. However, old tech probes can remain very useful.
(9) Are probes reliable for long-term missions? Yes!!!
EXAMPLE: NASA's reliability of 99.99% for the Apollo Project. works out to a survival probability of 99.9% after 1000 years and 81.9% after 100,000 years.
(10) Is searching for probes a passive task?  No.  It would be passive to  just wait for visiting extraterrestrial probes to initiate contact; however, SETI now actively seeks both probes and RFs.
(11) Can we search all possible, physical artifact sites?  Of course not, but recall possible RF bin quantity is infinite. However, it makes most sense to focus our search on the more likely "magic frequencies"; likewise, the "magic orbits" are where probes are more likely (e.g., Icarus, 1980 [Ref]).(12) Are RF signals superior to probes with physical artifacts?
Clearly not!!! RF beacons are limited to only repeat same information for perhaps eons to gain nothing new. On the other hand, manned (and/or AI) probes can autonomously seek out evidence of life such as communications.
SUMMARY:  For interstellar communication,
physical AI probes are more capable than RF waves.
SOURCE DOCUMENT:  Freitas, Robert A. Jr. (July–August 1983).
"
Debunking the Myths of Interstellar Probes"AstroSearch 1: 8–9.
Sending physical vessels between stars may prove much more useful than just RF signals. While vessels are limited to speeds far below light-speed, information in a few tons of physical matter could easily exceed utility of data via practical RF bandwidth for the foreseeable futureRobert Freitas proposed physical space-probes for better interstellar communications than RF signals.

REFERENCES

  1. Freitas, Robert A. Jr. (1980). "Interstellar Probes: A New Approach To SETI". Journal of the British Interplanetary Society 33: 95–100. Bibcode:1980JBIS...33...95F.
  2. Freitas, Robert A. Jr. (July–August 1983). "Debunking the Myths of Interstellar Probes". AstroSearch 1: 8–9.
  3. Freitas, Robert A. Jr. (November 1983). "The Case for Interstellar Probes". Journal of the British Interplanetary Society 36: 490–495. Bibcode:1983JBIS...36..490F.
  4. Freitas, Robert A. Jr.; Francisco Valdes (1980). "A Search for Natural or Artificial Objects Located at the Earth-Moon Libration Points". Icarus 42 (3): 442–447. Bibcode:1980Icar...42..442F. doi:10.1016/0019-1035(80)90106-2.
  5. Valdes, Francisco; Robert A. Freitas Jr. (1983). "A Search for Objects near the Earth-Moon Lagrangian Points". Icarus 53 (3): 453–457. Bibcode:1983Icar...53..453V. doi:10.1016/0019-1035(83)90209-9.
VOLUME I: ASTEROIDAL
VOLUME II: INTERPLANETARY
VOLUME III: INTERSTELLAR
CONCLUSION:  For several decades, the Search for Extra-Terrestrial Intelligence (SETI) project has  searched for signals from other stellar systems.  So far, no success; 
HOWEVER,  Earth will eventually receive interstellar signals from our descendants traveling to neighboring stars. Two way interstellar communications will undergo considerable attenuation due to intervening LYs; thus, it might be necessary to deploy RF repeater beacons at static interstellar positions.
1G Acceleration for 1 year.
7G Acceleration for 100 days.
7G Deceleration for 48¼ days.
1G Deceleration for 1 year.
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For certain stellar routes, comm capsules might deploy to facilitate communications for vessels between the two stars.
These comm capsules could also function as way-stations at fairly static locations; perhaps at 1 Light Year  (LY) distance intervals.
Such way-stations could provide good distance indications to vessels cruising at constant velocity.

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