Addressing Comments, Questions & Concerns From Prior Proposal Reviews

NSF Proposal Submitted In Year 1998, Ref: AST-9900661

(1) Panel Comment: On the basis of its potential scientific importance, the panel ranked this proposal extremely highly. However, the panel did not feel competent to judge the likelihood that the research could or would be completed successfully. The reason for this is that the proposal is mainly about a laboratory MHD experiment and no one on the panel has any direct experience with such experiments. The panel therefore recommends that the NSF program director seek reviews from several researchers with the relevant experimental expertise. If they conclude that the experiment is feasible and likely to be completed successfully by the PI and Co-Is, then the panel believes this proposal would be among the very best it has reviewed and should be funded by the NSF.

Reply to (1): The PI has spent his earlier career as an experimentalist, initially in nuclear weapons testing followed by a large number of liquid sodium MHD experiments establishing MHD for fusion plasma confinement. The observation of the tearing in a liquid sodium fountain led to elucidation of the "tearing mode". Later, many fusion plasma experiments demonstrated the lack of confinement of tearing unstable pinches. (This plasma physics of "flux conversion" is now central to the question of radio lobe evolution. ) However, at the time there were "pleas" by many theorists to construct and test a liquid sodium dynamo (particularly Johnny Wheeler). The minimum size required appeared to be many 10's of meters requiring many thousands of kW of power. Even for LLNL this was too much. However, in the late 80's with Greg Willette, we recognized the importance of the rotationally coherent nature of axially displaced plumes in a rotating frame. This source of coherent helicity has made this experiment feasible.


(2) Reviewer #1 Concerns: On the "minus" side, I worry about whether there is enough experimental "depth" on this team to pull off the experiment. All in all, I would trust Colgate's considerable expertise and his LANL collaborators to bring other scientists from LANL into this as appropriate.

Reply to (2): The experimental tradition at NMIMT is extensive, especially in observational and experimental atmospheric physics. Please see the NMIMT web site at http://www.nmt.edu/. If it could have been funded at LANL, it would have cost more than 10 times as much and take many times longer.


(3) Reviewer #2 Concerns: There is no evidence that they can get such a high flow speed, up to 100 m/s, thus high magnetic Reynolds number product of 4000 to achieve self-excitation (critical Rm of 1000). The power needed to generate flow speed in a turbulent state should be proportional to cubic of flow speed, instead of speed squared as used in the proposal. The nominal achievable speed is 10 m/s, a factor of 10 smaller than the estimate, therefore, there is no evidence that the goal of self-excitation can be achieved for the given driving power of 50 kW.

Reply to (3): There is an extensive engineering analysis in the year 2000 proposal in response to this question. The Couette flow is only very weakly turbulent, which is why it is chosen. The pressure curves are now part of this proposal relative to the MRI investigations, but were known initially for the original design. The present apparatus is twice the dimension of the size considered in this first proposal and was chosen on the basis of ease of construction, lower technology, lower pressures for a given magnetic Reynolds number.


(4) Reviewer #3 Comments: I am not competent to judge the engineering aspects of the proposed experiment. Achieving the 1-2 x 104 cm/sec with the associated rotating plumes is the key to success. It will not be easy, but the proposers have given considerable thought to the problem, and there is no reason to think that their ingenuity will not be successful.

Reply to (4): The size of the experiment has been doubled for ease of construction, reduced stresses and technology.

NSF Proposal Submitted In Year 1999, Ref: AST-0071070

(1) Panel Comment: The external expert referees raise critical questions about its (the experiment's) safety and engineering feasibility. We wonder whether this experiment can be realized without a greatly increased investment in funds, technology and engineering. Funds might be spent in engineering rather than a Co-I and graduate student who are not hardware experts.

Reply to (1): The experiment has been designed by physicists in conjunction with engineering advice. The physics considerations have been paramount. The original proposal was funded at 100k. Roughly the same has been spent in addition since then. The apparatus to test Phase I, the Ω-flow, is nearing completion as shown in Figs. 1 and 2.


(2) Reviewer #1 Comment: There is little past track record for this type of experiment. Perhaps a scale-down version of this experiment should first be used to demonstrate its feasibility and test the diagnostics.

Reply to (2): As discussed in the proposal there are three sodium dynamo experiments in this country, and two successful ones in Riga, Latvia and in Karlsruhe, Germany. The later experiments are up to 10 times the proposed experiment size.


(3) Reviewer #1 Comment: Safety issue is only lightly addressed.

Reply to (3): An extensive safety report is posted on our project web site; please see http://physics.nmt.edu/~dynamo/. A panel member of the 2001 proposal reviewed this with a positive comment; see first reviewer's summary statement, AST-0098474.


The experiment will be performed by remote operation, at ~100 m distance, in the open without building confinement. The experiment will be performed at the NMIMT high-explosive testing grounds, the Energetic Materials Research and Testing Center (EMRTC). More than 20,000 high explosive tests have been safely performed at EMRTC in the last 55 years. This is a major national high explosive testing facility. The safety practices and procedures are reviewed and overseen by both the EMRTC engineers and the NMIMT Research Division's Hazardous Materials and Safety Officer.


(4) Reviewer #2 Comment: The proposal makes little mention of sodium handling and safety. I appreciate that one of the proposers have worked with liquid sodium before (but at a time before much of the present liquid metal technology had developed), and that the liquid sodium volume is small. Nonetheless, the proposal leaves me curious as to how they intend to proceed.

Reply to (4): This is discussed in the safety section of our project's web site: Safety Practices, Procedures and Compliance. Please see http://physics.nmt.edu/~dynamo/.


(5) Reviewer #2 Question: How the vessel is charged and emptied of sodium in order to service the magnetic probe arrays?

Reply to (5): Neither of the two magnetic probe arrays require emptying and recharging the vessel for service. There are two magnetic probe arrays associated with the experiment: a 2-D matrix array and a radially-aligned linear array. The matrix array is mounted on the external surface of the driven end-wall of the apparatus, and thus it is directly serviceable. The radially-aligned linear array is inserted into, and removed from, a radial probe housing that is itself sealed into the outer cylinder. The radial probe housing is a hollow aerodynamic "vane", and remains in place whether the sodium is liquefied or solid. Thus the linear array is serviceable as required, independent of the sodium.


(6) Reviewer #2 Question: How cold spots are eliminated during the charging given only the inner cylinder is heated?

Reply to (6): The thermal time constant of the sodium when solid is about 5 minutes. When liquid, the convection time is much shorter. In addition the external shield can be electrically heated if necessary.


(7) Reviewer #2 Question: How catastrophic would a vessel rupture be, even with the safety shields?

Reply to (7): 140 kg of liquid sodium sprayed into the atmosphere at operating pressure and velocity will make a fine particle cloud that may or may not be able to be ignited at a temperature of ~110 C. If it burns, it will be about the same as the equivalent mass of gasoline or jet fuel. This is why the experiment is performed unconfined outside, not in a building. The experiment is to be remotely operated.


(8) Reviewer #2 Question: What strategy is proposed for the sliding seal through which the titanium piston is pushed. If this is simple packing material, are the pressures there small enough to eliminate a significant sodium leak?

Reply to (8): The titanium piston itself is guided on its outer surface via the bore of the inner reservoir plenum cylinder and internally by a linear bearing and high-temperature hydraulic seal sliding on the volume-compensating shaft. There is no seal on the piston's outer surface, but the by-pass flow should be negligibly small (clearance area / piston area). The volume-compensating shaft allows for the internal volume of the apparatus to remain constant while the piston extends and retracts in the source and sink reservoirs. The piston rod (hydraulic shaft), titanium also, is guided through linear bearings and high-temperature hydraulic seals. The hydraulic seals are capable of restraining pressures in excess of 3000 psi (~3x actuation and operating pressures) and withstanding temperatures of 150 C.


The axial bearings and seals will be in an oil environment. A finite amount, ~1 liter, of mineral oil will intentionally be left in the apparatus when filled with sodium metal. Due to the different specific gravity of mineral oil vs sodium metal, ~0.81 vs ~0.93 at 100 C, when the apparatus in spun up to the very low rotation rate of 42 rpm, the mineral oil will centrifugally float to the region of the rotational axis relative to the sodium. Thus the seals and bearings internal to the apparatus will operate in a hot mineral oil environment, not a liquid sodium environment. After an experimental run, the apparatus will be cooled while rotating so that the sodium will solidify with the mineral oil retained at the axis. Thus the only time that the seals could come in contact with the sodium is under the static configuration during the filling or draining process. In these circumstances the pressure will be small and would only be due to gravity acting on the liquid sodium. This means that all seals are oil seals, NOT sodium seals. These components are therefore standard high-temperature industrial components.


The piston that drives the flow for the pulsed plumes will be used in Phase II. Phase I of the experiment, the first year of this proposal, will not use the jets and hence will not use the piston.


(9) Reviewer #3 Concerns: Sodium safety; a) caustic smoke ventilation in case of fire, b) fire suppression of metal fires, c) sodium handling, d) safety training of personnel/students.

Reply to (9): These facets are all discussed in the safety section of our project's web site: Safety Practices, Procedures and Compliance. Please see physics.nmt.edu/~dynamo/


(10) Reviewer #3 Concerns: Stress analysis; The proposed experiment would be pushed to an internal stress in the stainless steel of 30 ksi. Although such a design is possible, one should not undertake this without a more detailed (numerical) stress analysis of the design. The presented back-of-the-envelope calculations are not suitable design criterion.

Reply to (10): The size of the apparatus has been doubled and the vessel material has become aluminum alloy. The maximum stress currently expected is 10 ksi compared to a limiting strength of 40 ksi. The vessel will be tested hydrostatically and the apparatus will have integrity verification measurements performed with mineral oil under rotational operating conditions.


(11) Reviewer #3 Concerns: Seals; The seals which hold the sodium into apparatus between differentially rotating parts are a concern.

Reply to (11): See above for discussion of oil immersion of all seals and bearings; Sec. 1.2, Reply to (8), paragraph 2.


(12) Reviewer #3 Concerns: Cooling; The proposed maximum mechanical power needed is 40 kW. This mechanical energy is converted to heat by the actions of viscosity and possibly Joule heating.

Reply to (12): Experimental runs or tests at or near high speed will be of the order of a few minutes duration. The total time at the near maximum speed will be no more than a few minutes also. The change of temperature during a test will be small, a few degrees at maximum speed (~1 degree per minute at 40kW). The oil circulation can be used as cooling if necessary, but we expect windage heat loss to be larger than internal friction heat gain and therefore have provided the opportunity for heating in the surrounding safety shield. We may require greater power and the current motor can be used to double capacity for the short periods of the experiment.


(13) Reviewer #3 Concerns: Rotating electronics; Substantial rotating analog and digital electronics appear to be proposed. These electronics are needed to survive 100 Hz rotation leading to a 2000g acceleration and a temperature of 100 deg. C. Standard laboratory electronic techniques are unsuitable. Discussion is needed about what Mil. spec. techniques are available.

Reply to (13): Due to the doubling of the apparatus size, the the outer cylinder assembly, low-speed drive and printed circuit board (PCB) mount rotate at 30 Hz. The acceleration at the periphery of the ~30 cm radius apparatus is ~1000 g. The electronics undergoing this acceleration are the analog devices consisting of Hall effect detectors, pressure transducers and temperature sensors. The specific examples of each that have been chosen and purchased can readily withstand 1000 g in a sustained thermal environment of 150 C. They are in essence ``off-the-shelf'' items, thus Mil. spec. techniques were not required. Power and signal communication with these analog electronics takes place via twisted pairs from the PCB. The PCB houses the balance of the analog electronics and all the digital electronics. These consist of amplifiers, multiplexers, A-to-D converters, and a programmable logic device (PLD). The PCB is ~15 cm in radius, thus the acceleration at its periphery is ~500 g. All components, or component sockets are wave soldered to the PCB. Being individually low mass, they can readily withstand 500 g. Wiring traces on the PCB are configured such that induced currents from the magnetic field coils are minimized or nullified. Power for the electronics are brought on board via conventional carbon brush slip rings. Bidirectional digital communication with the electronics takes place via capacitative (air gap) slip rings. The PCB mounting flange thermally isolates it from the bulk of the convective and radiative heat such that it should have a saturation temperature of less than 55 C. The standoff vanes to which the PCB is physically mounted are configured to pump air behind it when the apparatus is rotating, and thus force cool it also. When static heating is taking place, such when charging/emptying of sodium, a fan and duct will be used to cool the electronics. (The pressure and temperature electronics will be used to monitor the apparatus during charging and emptying.)

NSF Proposal Submitted In Year 2000, Ref: AST-0098474

(1) Panel Comment: The experimental details and the specific way in which the experiment works were not made optimally clear in the proposal. For example the schematic diagram was not accompanied by a step by step outline of how the experiments are performed.

Reply to (1): Additional information is on our web site and added to this proposal. Please see physics.nmt.edu/~dynamo/


(2) Panel Question: Under what circumstances would Beckley continue on the project given that his participation seems essential?

Reply to (2): Howard Beckley is desiring to stay on the project through its completion. It is intended that he will receive his Ph.D. at the completion of Phase I, the Ω-Phase of the experiment. He hopes to continue working on the project as a postdoc and guide the efforts of other graduate students pursuing their advanced degrees. He has been responsible for the day-to-day research guidance of the physics and electrical engineering undergraduate student's efforts on the dynamo project's instrumentation development and looks forward to continuing this aspect. All of the requested funding for this proposal is for Beckley's postdoc salary.


(3) Panel Recommendation: It seems that the experiment is well on its way, however the panel recommends having an experienced outside experimentalist review the current status and the likelihood of success and safety of the experiment.

Reply to (3): We will continue to present the experiment at meetings. A paper has been accepted. We are posting more details on our web site. We welcome visitors. The PI obtained his degree in experimental physics with Bob Wilson of Cornell. As an experimentalist he was responsible for the fast diagnostics (neutrons and gammas) for the major thermonuclear weapons tests of LANL and LLNL during the Castle series of 1954, including the 12 megaton equivalent Bravo test. He published more than 50 SRD and open literature reports of plasma physics experiments of the "fusion pinch" program at LLNL. He published more than 40 reports and publications of atmospheric, geophysics, and automated astronomy experiments, 1964 through 1975, while at NMIMT. He continued with a major experimental program at LANL in high explosives and plasma physics.


Howard Beckley has had comparable experience as a machinist for 23 years, including foreman of a machine shop for 3 years. He has done considerable experimental work in astronomy, astrophysics, fluid dynamics, and thermodynamics at NMIMT for 7 years and at Sacramento Peak and Cerro Tololo for one summer each. We feel we have the credentials and experience to make this experiment work.


We continue to have reviews within the institution on safety. For instance, we question the safety of any high speed liquid sodium experiments within a confined building without the exclusion of oxygen. The safety experience and tradition of 55 years of more than 20,000 high explosive tests makes the NMIMT's EMRTC high explosive proving grounds one of the major HE test facilities of the country.


(4) Panel Recommendation: We recommend that it be clarified what a smaller level of funding would still be viable to ensure the experiment's success.

Reply to (4): We are asking for a more modest 80k per year for this proposal, primarily to support Howard Beckley as a postdoc. This level of funding would allow us to complete both phases, I & II, of the experiment in three years, or just Phase I of the experiment if funding is for only one year. We expect to have roughly equal funding available from other funding sources, including DOE Fusion, LANL and a Frontier Center proposal, and in addition, separate support of the graduate and undergraduate students.


(5) Reviewer #1 Question: I do think the proposer could have mentioned the magneto-shearing instability. Why are Rossby waves the mode of angular momentum transport rather than magneto-shearing instability?

Reply to (5): The magneto rotational instability (MRI) was mentioned in a foot note as an obvious first experiment during the Phase I experiment in the year 1999 and year 2000 proposals. This was not emphasized because we had not performed the stability analysis in the presence of the Eckman layer induced turbulence. This analysis is now a part of this proposal. There were just too few of us spread too thin. The Rossby vortex mechanism of torque transmission in a Keplerian disk has the possibility of torque transmission in an insulating disk and therefore before magnetic fields are generated. This is not a problem in stellar size disks around compact objects because the companion star can always supply the flux to the Roche lobe overflow. The scientific question is whether the MRI can act as a dynamo and create its own flux. We hope to address this question in the Phase I & II experiments.


(6) Reviewer #1 Question: Why are the disks not turbulent in AGN?

Reply to (6): So far there is no known accepted way to produce turbulence in a Keplerian disk except the MRI. There are very many papers that assume it, but none that prove it without the MRI. This is why the MRI is considered so important. This requires flux and conductivity. The Rossby vortex mechanism circumvents this difficulty. (astro-ph/0012479)


(7) Reviewer #1 Question: Also, the Rossby waves should be studied in the presence of magnetic fields. Are they present in the dynamo region?

Reply to (7): The "turbulence " induced by the Eckman layer flow stress will indeed be an ensemble of "Taylor columns" . However the magnetic Reynolds number of these eddies, Rmag / (Rey1/2), presumably following the law of the walls, or logarithmic profile distribution, is too low to be significantly affected by the turbulence.


(8) Reviewer #1 Comments: (Referring to 5,6,7) These should be addressed in the associated theoretical work, but this is not the main use of funding requested. We do not have experimental evidence for magneto-shearing instabilities, only numerical evidence - perhaps the experiment itself could test for it.

Reply to (8): Now a major thrust of this proposal.


(9) Reviewer #2 Concerns: The proposal also suggests that the experiment is directly relevant to dynamos in astrophysical settings, particularly accretion disks onto compact objects. I have several misgivings about this conclusion, which bear on the astrophysical relevance of the experiment (at least for compact object accretion; for stellar or galactic dynamos the analogy may be more appropriate).

Reply to (9): We apologize for implying that the α-Ω dynamo might occur in the accretion disk around compact objects. This may or may not occur depending upon the effectiveness of the MRI or Rossby vortex mechanism. To apply the α-Ω dynamo to stars requires a deeper understanding of convective plumes at the base of the convective zone than is presently available. One might expect that the diffusive heat flow, radiation transport transition to convection would truncate the smaller scales leaving only the large scale convective elements, of order H to carry the heat. At this scale such plumes would make effective helicity-generating plumes for the α-Ω dynamo in nearly all rotating stars.


(10) Reviewer #2 Comments: In addition, the Couette flow proposed in the present experiment has an Ω~R-2 rotation profile. This is a rather special rotation law for which the radial epicyclic frequency of the system vanishes. It appears from numerical simulations that dynamo action in an Ω~R-2 system can be rather different from that in a Keplerian disk with Ω~R-1.5. The feasibility of varying Ω(R) should be considered and would be an interesting addition to the proposed experiment.

Reply to (10): We agree that other profiles are of interest. The profile with maximum stable shear has the best possibility of making a dynamo with positive gain as demonstrated by the calculations. Lower shear will create a lower toroidal field (lower magnetic Reynolds number) and hence less gain for a given helicity. We will find out in Phase I of the experiment. One simply disconnects the high-speed drive clutch and monitors the magnetic effects as the Couette flow profile decays to the solid body profile.


(11) Reviewer #2 Statement: The proposed experiment would be an interesting and scientifically important proof-of-principle for dynamo amplification of magnetic fields; its astrophysical relevance for the compact object accretion problem motivating the proposal is, however, probably limited.

Reply to (11): Separately we have been demonstrating theoretically and by observations (astro-ph/0106281) that the giant radio lobes are an indication that the major free energy of BH formation must be accessed to satisfy the minimum energy requirements, 1061 erg. In addition this must be a coherent, large-scale production mechanism of magnetic flux. This magnetic energy is 107 greater than the galactic magnetic energy, and 103 greater than the galactic binding energy. The flux is 104 greater than the galactic magnetic flux. Only an α-Ω dynamo in the BH accretion disk has the possibility of accessing this amount of energy and creating this flux. The helicity generation must then be non-axisymmetric and episodic by Cowling's theorem.




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