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A CARBON TAX FUELED SOCIAL SECURITY SOVEREIGN WEALTH FUND; And TVA ,a study of bond limits and earnings ratios

we want to explore the macroeconomics of the Tennessee valley authority(TVA) bond limit, bond limit to cash flow formulas and the TVA boards electrical rate setting authority.The TVA has almost reached its maximum debt limit need to build nuclear reactors;

TVA 2013 annual report

http://www.snl.com/Cache/20876667.pdf?IID=4063363&FID=20876667&O=3&OSID=9

TVA 2012 annual report

http://www.snl.com/Cache/15350412.pdf?IID=4063363&FID=15350412&O=3&OSID=9

 

secondary we want to study the relationship of the TVA to the carbon tax social security sovereign wealth fund, how can we build 6 to 15 heavy water reactors in the TVA service region without doing harm to the TVA bond debt limit of $30 Billion?could we avoid the prohibition of selling this power outside the TVA service area as now required by law?

 

possible solution might be that the social security sovereign wealth fund pays TVA to build and operate the plants but  the carbon tax sovereign wealth fund retains ownership and TVA purchases the power for 60 years from each plant for resale.

the sovereign wealth fund will take possession of spent nuclear fuel and build heavy water nuclear power plants on the site of existing nuclear reactors to ease the NRC regulatory burden and to burn the spent fuel using the minimal processing of the DUPIC idea.

Progress-on-approaches-to-the-management-of-separated-plutonium-position-paper-January-2014

http://www.wincanada.org/event_uploads/192/1385574939459Rosaura_Ham-Su.pdf

http://library.lanl.gov/cgi-bin/getfile?00796025.pdf

http://www.nuclearsafety.gc.ca/eng/pdfs/vendor-licensing/EC6-Phase-3-Executive-Summary-eng.pdf

 

 

 

the other ideas discussed here are very expensive;

just say no to Yucca mountain,reprocessing, interim storage!

http://www.world-nuclear.org/info/Nuclear-Fuel-Cycle/Fuel-Recycling/Processing-of-Used-Nuclear-Fuel/

as are transfer to a geological burial and/or interim storage,we would build a fleet of heavy water reactors to burn spent fuel at the existing sites at TVA, it would take another 60 years to burn the spent fuel to produce yet more fuel

The grand bargain

we need the 16 mostly republican senators of the states in the TVA service region to vote for a carbon tax to build 6 to 7 heavy water reactors in the TVA service area as well as 7 reactors more in South carolina savannah river DOE facility.The grand bargain includes cession of all laws in regards to yucca mountain and the implantation of policy to burn all spent fuel in heavy water reactors followed by a fleet of molten salt reactors to burn heavy water spent fuel in a nation wide program to build heavy water reactors at all existing nuclear plant sites

 

 

Carbon Tax sovereign social security wealth fund 3.0 The macroeconomics of open economies

UM Flint Summer principle of economics  201   

net exports equals value of country’s exports minus value of country’s imports

The $250 Billion annual carbon tax would for the most part be invested in the capital markets of the world.As such it would become a part of the macroeconomic concept of net capital outflow.We have proposed a $50 Billion per year nuclear power plant and other renewable energy build program that would produce cash flows from electrical sales for future generations of unborn future social recipients.

https://yellowdragonblog.com/2014/07/06/a-carbon-tax-fueled-social-security-sovereign-wealth-fund-2-0-macroeconomic-effects-on-nuclear-power-plant-build-program/

The other $200 Billion per year invested in the world economy would according to the text book by N. Gregory Mankiw represent a net capital outflow that must be balanced by the principles of equality of net exports and net capital outflow,

NCO = NX

net capital flow equals  net exports

S = I + NCO 

saving  equals domestic investment plus net capital outflow

The carbon tax social security sovereign wealth fund has acquired some foreign asset such as a stock or bond or some physical capital asset.The carbon tax sovereign wealth fund is also a very large national savings fund.according to Mankiw savings = investment + net exports or S= I + NX 

S=I+NE

However the $200 Billion capital outflow is not NET and it also must balance as in Gregory Mankiw’s table 1 above.Does the formula in table 1 work in reverse? our $200 Billion might be offset by domestic investments in stocks and bonds and the net capital outflow implies that this would be offset by a reduction in the american balance of trade or reduce the american trade deficit!

figure2

Figure 2 from  Mankiw’s chapter 18 The macroeconomics highlights the relationship between national savings and domestic investments and the percent of national capital outflow to GDP, they match. So if $100 Billion per year were “saved’ in the domestic capital markets and $ 100 billion per year in the foreign domestic markets and $ 50 billion per year in power plant construction projects than $100 Billion minus the $50 Billion power plant build yields $50 Billion in additional capital outflow from invested carbon taxes in addition to the $100 Billion already invested in foreign markets

$ 150 Billion total capital outflow per year

this would be a little less than 10% of the trade deficit  or would reduce the trade in balance by this amount.

  http://www.bea.gov/newsreleases/international/trade/tradnewsrelease.htm

The $150 billion per year carbon tax net  capital outflow would change the percent of capital outflow as a percent of GDP by less than 1% upwords.

https://econ411w14.lsa.umich.edu/tag/international-finance/

net-export-and-private-saving

The above chart from UM econ 411 class seems to show a $150 Billion Carbon tax invested as net capital outflow would be a increase of almost 3 % or more of GDP increase.

GDP+Fed spending 1900-1950

the $50 Billion in annual power plant build would represent a small percentage of the federal budget, what would this $50 Billion per year investment do to the Phillips curve? would this cause inflation? Nuclear power plants and solar voltaic panels are high tech high wage trades jobs so this could have a multiplier effect but this is chapter 22 of the Gregory mankiw text.

The nuclear and renewable investment might put pressure on the consumers price index that would make the exchange rate for the USD higher, (e x P ) / P* exchange rate x price index / by foreign price index.Nominal exchange rate is currency trading real exchange rate  products and goods sold at that rate.

The carbon tax sovereign wealth fund and its governance by the federal reserve and the social security trust fund board

The business cycle and the stabilization of the economy would be greatly benefited by the management of the sovereign wealth fund by a partnership of the federal reserve board and the presidentially appointed social security trust fund board.At times the sovereign wealth fund might want to slow its use of carbon tax cash to build power plants domestically and to borrow funds on foreign markets to build power plants,Euro bonds would have the effect of transferring or decreasing net capital outflow if in fact the eurobonds to fund nuclear power plants where bought by foreigners.another idea would to slow down or speed up capital expenditures in the american market to slow or speed up the business cycle and/or inflation.  

http://www.nei.org/Master-Document-Folder/Backgrounders/Fact-Sheets/Nuclear-Power-Plants-Contribute-Significantly-to-S

Nuclear build

CTC_Carbon_Tax_Model

Recessions could be dealt with by always having shovel ready investments held in reserve for a surge of building by the sovereign wealth fund as a new mechanism to be used by the federal reserve as long as the capital is deployed for positive cash flow activities.In a true national emergency the sovereign wealth fund could buy bonds from the federal government in order to move aggregate demand and aggregate supply to the right.The sovereign wealth fund could have lent money to the government for the 2009 stimulus and that loaned  money could have gone to non positive cash flow projects to boost employment.Injecting cash through buying a $ trillion of bonds makes more sense then attempting to have shovel ready power plants ready to construct.

The aggregate supply curve for electricity is most likely  in a recession to be affected by a leftward shift of  Aggregate demand another reason not to increase or decrease power plant production/construction but instead to loan sovereign wealth fund cash to the federal government. ideally the amount of the federal debt owed to the sovereign wealth fund should never exceed 5%

So the job of the sovereign wealth fund is to invest in positive cash flow capital, loaning money in a downturn for the government to spend on public works and relief is the job of both.

ramping up construction of such large projects as power plants would produce a effect that lags results over time as to be noticed only after the recession is over, this is a known problem in fiscal policy recognition lag,implementation lag and effectiveness lag.deploying rapidly deployable solar arrays would make more sense. 

 

OSIRIS-REx ice cream asteroid meteorite naming contest

is this idea marketing or educational? (or both)

Ben and Jerry’s and the OSIRIS-REx team would partner, you have to know your classes of asteroids well and design an ice cream around that asteroid or meteorite and name it!

 

the winners have a ice cream manufactured by ben and jerrys and the proceeds go to a trust fund in the small body science community

 

Ben and jerry’s asteroid ice cream naming contest

Ben and jerry’s asteroid ice cream naming contest

 

EDIT    29 Dec 2014

And with 7 Billion people on our planet its impossible o come up with an original idea! some folks in the UK have thought of this idea first,Imagine what a productive world we will have if all 7 Billion people have laptops

 

 

http://www.youtube.com/watch?v=4-CyMv8h47w

 

http://www.exploreyouruniverse.org/wp-content/uploads/2013/07/asteroid-icecream-instructions.pdf

 

http://www.nuffieldfoundation.org/asteroids-ice-cream

 

 

 

 

 

 

 

 

 

 

 

 

LH2, LO2 boil off fuel cell cubesat flight experiment 2015 SBIR proposal

(A)(1) fly  SLS EM-1 on a lunar free return back to a earth flyby

(A)(2) Fly a LH2,LO2 fuel cell power by boil off from the SLS EM-1 upper stage

(A)(3) before earth flyby the cubesat deploys and power beams some of the  power through the Earths atmosphere with ground based monitoring of microwave beam characteristics

so can we deploy on a 6U a fuel cell?

can we deploy a microwave power beamer on this 6U cubesat?

can we max out on insulation on the SLS EM-1 mission upper stage?

would there be enough or any fuel remaining in the upper stage for an earth oberth burn?

would we need an oberth burn with an earth flyby to assist the NEO scout deployment?

can the other ULA long term cryogenic proposed experiments be brought to a cubesat level of deployment such as cryogenic fluid transfer?

EDIT

17 August 2014

A mini microwave transmitter also validates the microwave power system on our proposed small fission reactor hybrid with the Lunar polar centaur lander

The Centaur upper stage with a small fission reactor radiator and its Xenon/Argon ullage gas in the propellent tank is generating power three ways, the last one being the radiator heating the Noble gasses and powering stirling or ranking engines.

the lander and a rover are in total darkness in a Lunar or Mercurian polar crater so the rover must be powered by a cable or a microwave beamer and it should be pointed out both the lunar and mercurian nights are long and would benefit from my unique chemical.small fission reactor power plant idea

https://yellowdragonblog.com/2014/03/27/ula-coaxial-lander-small-fission-reactor-hybrid-powerplant/  

SLS EM-1 upper stage as experimental flight test bed (Lunar free return flight)

greetings!

we know that there are papers that talks of interplanetary hosted payloads so I would like to see any future ULA upper stage that is intended for stage disposal in solar orbit instead be sent on a lunar free return followed by an earth oberth burn.My understanding is that two centaurs on classified missions did a disposal burn into solar orbit
could those Centaurs have made a lunar free return orbit?(Earth reentry)?
6 days in space would inform us as to boil off behavior in an upper stage?
would there be any propellant left after 6 days?
enough to perform an oberth earth burn back out into solar orbit?
I propose such an in space stage mission be monitored by cubesat type payloads meant to monitor in space stage cryogenic behavior and possibly deployed cubesats
consideration should be given to look for DCCS and the  SLS EM-1 possibilities for lunar free return and earth escape trajectories to enhance the trajectories of the proposed NEO scout and other future interplanetary cubesats
Enabling the SLS upper stage to last for 6 days would perhaps inform us further as to future in space stages as long-term missions.
NASA Ames could ask the human space flight directorate to model the requirements to allow the SLS EM-1 upper stage to do this mission
another exciting possibility would be to have NEO scout deploy from the in space stage after sending the stage to L-1 or L-2 perhaps shortening the trajectory of NEO scout?
this version also should have cubesats dedicated to in space stage cryogenic monitoring for several days after lunar flyby and to have NEO scout image the stage before moving off.These spent stage ideas seem to me to be very low risk, even the high-speed reentry from lunar free return could perhaps provide some data? fly that monitoring device that rode the ET tank back down to earth! I know that the stage will need a solar array like LCROSS or perhaps fly an experimental fuel cell that can use the boil off?such a fuel cell itself perhaps could be an attached cubesat payload? and this fuel cell could enable many in space stage applications and in space stages as spacecraft in the outer solar system
What’s needed?
(A)(1) Human space flight directorate “release” the upper stage for transport to a Lunar flyby orbit to L2 to the NEO scout project
(A)(2) characterization of ULA  multi day flights of cryogenic upper stages to this upper stage and residual fuels load and survival for two days to  lunar flyby
(A)(3)NEO scout is seen as a 2.5 year mission travel time to a candidate NEO, releasing this mission  and others after a lunar flyby could shorten this travel time.
(B)(1) modest funding for long duration SLA upper stages informs us as to other other proposed uses for long term cryogenic storage of propellants such as fuel depots/tankers/deep space missions.
(B)(2) in the introduction to this article we posit a upper stage whose secondary mission would be a Lunar free return to earth orbit followed by an earth fly by with an Oberth burn.This is 6 days!  cryogenic stored this long would be an important intermediate flight experiment and the cargo would be interplanetary cubesats
EDIT  5 October 2014
here is a paper that follows closely what I am thinking, I can’t read it as its behind a paywall.I am thinking they are not proposing to use the upper stage at  the moon to perform a burn…………………….
Geoffrey A. Landis, Steven R. Oleson, Melissa L. McGuire, Laura M. Burke, Michael C. Martini, James E. Fittje, andThomas W. Packard

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. July

Mini-Me Cubesat hypersonic decelerator flight experiment

We propose a Cubesat mission to Mars with the NEO scout architecture and deployment from SLS on a cislunar trajectory,intriguingly we think that even with boil off of propellants a SLS third stage could do a free return lunar flyby with a Oberth burn at earth.

One 6U cubesat would prove out ideas concerning very small inflatable hypersonic decelerators in the martian atmosphere, the other concept is a 6U cubesat Phobos and Deimos explorer, all of them could benefit from hypersonic deceleration.

 

(A)(1) At what range could a 6U cubesat communicate with a mars orbiting Electra communications payload?

(A)(2) could we operate a 6U cubesat beyond .5 AU while on a trajectory to mars without communications for 6 months?

(B)(1) can we miniaturize hypersonic decelerators for use with cubesats?

(C)(1) can the SLS TLI stage survive long enough (5 days) to do a free lunar return and Earth Oberth burn?(to mars)

20140000962

20140004799

 

7045

03-2150

A3_Banazadeh_Presentation

 

Descanso9_Full_rev

why launch from Puerto Rico; 2.0

why launch from Puerto Rico

visualized!

Puerto Rico SpaceX ballistic stage recovery

We would want the ideal launch azimuth to LEO from Puerto Rico  and the secondary goal is where to ballisticly soft land the first stage on land? and in the case of the Falcon heavy where to land the CBC and core stage?

Puerto Rico launch at a heading of 202 degrees without a first stage dogleg 432 miles to Bonaire (sun synchronous orbit).

Puerto Rico launch at a heading of 202 degrees without a first stage dogleg 432 miles to Bonaire (sunsynchronos orbit).

Vandenberg AFB is more of a problem I think? San Nicolas or any of the other channel islands looks like to me to be a much more  of a propulsive maneuver from the point of MECO then  a purely ballistic first stage recovery wich is what we where seeking, still better than a return to Vandenberg if it where not for costs  of transport from the island landing zone back to Vandenberg or Hawthorne.

is there fuel for weight to be gained for a classified payload or a government payload  by landing a stage at San Nicolas? some I would think but I am less than happy.

And the ISS destination from Puerto Rico?

ISS launch from Puerto Rico stage recovery at US Virgin Island with a ballistic trajectory

This would depend on a cost benefit analysis of whether ISS cargoes is enhanced by an increased payload to ISS VS the cost of a virgin islands landing infrastructure to 2024?

San Nicholis island as a SpaceX first stage landing site

San Nicholis island as a SpaceX first stage landing site

I have argued in a post from three months ago that the best use of a SpaceX first stage reusability would be to return to earth the first stage after a ballistic reentry and not return the stage to its landing site propulsively. This results in an unwanted ocean landing unless I argued some months ago that there might be a launch site with some convenient islands near by?

For Vandenberg AFB this would be the channel islands, however during parts of the year the channel islands are to the east of the sun synchronous orbit insertion so a first stage would have propulsively dog leg east to get to one of them. Which one is closest? I think this would be San  Nicholas island. It has a new heavy-duty pier installed as of 2002/3,

http://www.globalsecurity.org/military/facility/san-nicolas-island.htm

also it is a secured facility out of the way from any population centers and should as a munitions test site pass any EPA regulatory requirements. A barge could ship the first stage back to Vandenberg AFB. Could the first stage be shipped back to Hawthorne from San Nicolas? In addition San Nicolas is home to tracking and range assets.

the idea is based on my post from a 7  June 2014 dealing with First stage landing sites in the leeward islands from a Puerto Rico launch site the leeward islands may be close to LEO launch’s trajectory’s, Dominica for example is  350 miles south/south-east of Puerto Rico and a Falcon heavy core could come down in Barbados or St Lucia  are 500 + miles.

why launch from Puerto Rico?

Puerto Rico being closer to the equator makes possible bring a falcon heavy core stage all the way to orbit but without a payload, I would do this with extra RP-1 onboard as a storable propellant as the only payload.

Georgia-Institute-of-Technology-Final-Paper-2013

Polyethylene foamed with Argon and Xenon as spacecraft radiation barriers

Polyethylene foamed with Argon and Xenon as spacecraft radiation barriers

Could be used to fill in inter tank voids in my proposed decadel survey small fission reactor hybrid with a cryogenic upper stage.upper stage tank walls and upper stage hull combined with noble gas foamed polyethylene might be the combination we need to stop radiation from damaging  payload and avionics.These noble gasses are light weight neutron poisons.

could be a useful way to shield astronauts

Night Time Polar Synchronous Hybrid Chemical/NEP Stage for Classified Missions

night-time polar synchronous hybrid chemical/NEP stage for classified missions, “The B Train”

The decadal surveys proposed small fission reactor make possible to place in orbit a classified payload into orbit on the nighttime side of polar synchronous orbits with out need for solar arrays. The lack of incident radiation and visible light should render the spacecraft invisible in the visible spectrum.Possibly a night only Molniya orbit can be designed?

The small fission reactors radiator is located in one of the fuel tanks of the upper stage so as to recover heat from the radiator to power a secondary power generator.The upper stage remains with the payload  for power.The upper stage uses Xenon ullage to pressurize the tanks and after the chemical fuel burn the Xenon moderates radiation levels and transfers radiator heat to a second set of Stirling motors.

I have an entire class of missions that would be enabled by this idea here on this site ,

https://yellowdragonblog.com/category/small-fission-reactorchemical-stage-hybrids/

To include capsule pressure vessels as fission reactor cogenerators

https://yellowdragonblog.com/2014/03/26/hybrid-small-fission-reactor-pressurized-argonhelium-capsule-as-ion-powered-sep-stage/ from 26 March 2014

and a new post from 27 September,

https://yellowdragonblog.com/2014/09/27/nuclear-powered-spy-sats-in-night-time-orbits-for-permanent-eclipse-1-5/

Lunar polar and deep space systems of exploration could benefit from this unusual idea of mine and I would like to interest the DARPA inter agency program offices for dual use technology.Our goal for NRO would be to be invisible to the sees sat community as well as adversary’s. Is it possible to plan a Molniya orbits in total darkness?A polar orbit in darkness is not optimal for intelligence gathering so some elliptical orbit that drifts inside the nighttime side.

this spacecraft should ride into orbit into a sun synchronous trajectory and once in darkness dog leg it over to a night-time synchronous polar orbit to further confuse the potential observer(The B Train).