Tuesday, October 30, 2018

Recommendations for Election 2018

It is time to hold the president accountable for illegal actions.  If Congress will not do this,  they are complicit in the illegalities.  Which means they,  too,  are unfit to hold their offices. 

Border Troubles

The only real chaos on our southern border is that created by the Trump administration.  Claims otherwise trace to conspiracy theories and outright lies coming from far-right websites and outlets.  Anyone with internet access can verify this for themselves.

Refugees have the right under federal law to apply for asylum.  The president wants to deny them that right,  which is therefore an illegal act under federal law.  He does this for purposes that can only be described as racist,  and which are therefore are both illegal,  and abusive,  under the Constitution which he swore to uphold.  Failure to uphold the Constitution is an impeachable offense.   

Due process for illegal aliens is a gray area under federal law,  something Congress has failed to rectify.  But summary deportations and arbitrarily-presumed guilt justifying family separations is definitely a denial of any concept of due process.  Such procedures therefore violate the Constitution,  which the president swore to uphold.  Failure to uphold the Constitution is an impeachable offense.

The president wants to nullify part of the 14th amendment to the Constitution,  by presidential executive order!  Specifically,  he wants to end citizenship-by-birth for the babies of immigrants.  This issue has not before been a problem,  not since the adoption of the amendment right after the Civil War.

Amendments to the Constitution may only be modified or nullified by the Constitution’s amendment process itself:  proposed by 2/3 supermajorities in Congress or by 2/3 of the states,  and ratified by ¾ supermajorities in Congress or by ¾ of the states.  This is subversion of the Constitution by the president,  a very serious impeachable offense indeed!

Incitement to Violence

Despite what the president claims,  the newsreel footage available on-line clearly shows the president using very inflammatory rhetoric at his political rallies,  and in multiple cases encouraging his followers to beat up hecklers and news reporters.  This is clearly incitement to violence,  which is certainly not at all civil behavior,  even if legal.    

“Incitement to riot” laws exist in all the states,  which may make this presidential exhortation to violence an illegal act.  Even if not,  such probably qualifies as a “misdemeanor” under the constitution’s “high crimes and misdemeanors” definition for impeachable offenses,  particularly since the recent mail bomber and the recent synagogue shooter seem to have been far-right wing extremists.  Such are commonly Trump supporters. *** Update 11-1-18:  The mail bomber is known to be both an extremist and a Trump supporter.  The synagogue shooter is most definitely an extremist,  but reportedly not much of a Trump supporter. 

This is all the more serious,  since people died at the synagogue shooting.  The president didn’t do this,  nor did he specifically order this.  But he certainly inspired these criminals to commit their acts.  Inspiring others to commit crimes might well be an impeachable offense.  It is certainly worth considering.

Possible Treason

For two years,  the president has been damaging our alliances by insulting our allies and starting trade wars with them.  These alliances have kept the peace and forestalled our enemies for 7 decades.  While doing this,  our president has treated most of our worst enemies (Russia,  North Korea) better than our allies. 

This very probably qualifies under the “aid and comfort to the enemy” definition of treason in the Constitution,  and it was witnessed by millions,  if not billions,  on television right up to the Helsinki meeting.  The Constitution requires only two witnesses.

Whether actually treasonous or not,  this is serious enough to qualify under the Constitution’s “treason or other high crimes and misdemeanors” definition of grounds for impeachment.  One public figure did call this “treasonous”,  and suffered retaliation at the hands of president for it.  That act alone bespeaks of a very real disregard for the Constitution and federal law. 

Where Is Congress On This?

The Republicans have control of the House,  the Senate,  the White House,  and now, the Supreme Court.  However,  Republicans as we have always known them have mostly left the party,  or been thrown out of it,  by right-wing extremists and Trump supporters.  The party,  as we knew it,  is no more.

Thus there is no chance of a House impeachment or Senate trial under these circumstances,  since this new version of the Republican party has repeatedly demonstrated itself to prioritize party advantage over the good of the country.  

In a very real sense,  the Trumpist Republicans as they now exist in Congress are complicit in Trump’s offenses,  since they do absolutely nothing to restrain him. 

What to Do About It

The only way around this dilemma is to vote them out as quickly as you can,  starting November 6. 

It really doesn’t matter so much who the opposition actually is,  or what they claim to want to do.  I literally don’t see how any such change at all,  could be any worse than the status quo.

So that’s my recommendation:  vote ‘em out!  Elect anybody but Trumpist Republicans!

Then insist the new ones stop Trump from doing any more damage to this country.  Contact them and tell them so,  in no uncertain terms.

Final Remarks

I do not make these recommendations lightly.  I am a long-time fierce independent voter,  who over the decades voted for more Republicans than Democrats,  all of it split-ticket.  Misbehaviors like these have reversed that trend in recent years. 

Update 10-31-18 for Texas races:

Our governor and lieutenant governor have led the charge to destroy the Texas public schools by underfunding them and promoting tax-funded vouchers at private schools.  This underfunding forces local tax entities to raise their revenues to compensate.  The governor and lieutenant governor then point at "out-of-control local tax offices" for political gain.  

This perfidy outweighs any good either man has done.  So I recommend you vote for the "other guys",  it really doesn't matter who they are or what they advocate.  How could we possibly do worse?  Update 11-7-18:  statewide,  we re-elected them,  not by large majorities.  

Our state attorney general is a 3-time-indicted felon for bribery and corruption,  just not yet tried in a court of law.  This way far outweighs any possible good he could have done.  Vote for the other guy.  Update 11-7-18:  statewide,  we re-elected this one,  for which I am ashamed of my state.

Our commissioner of agriculture has made trips at taxpayer expense to compete in the rodeo in Arkansas,  then Oklahoma to get a pain shot for injuries suffered in that rodeo.  He said he would do state business while on those trips,  justifying traveling at taxpayer expense.  

But the records indicate he did no state business on those trips,  and did not reimburse the state for the expense.  That's actually a crime.  Vote for the other guy. Update 11-7-18:  statewide,  we re-elected this one,  for which I am ashamed of my state.

The rest are not quite so egregious.  You must decide whether they prioritize party advantage over good of the people.  (The correct priority is the other way around.)  If you think they do value party advantage over good of the people,  then I recommend voting for the other guy.  I did,  because that's the conclusion I reached,  for my senator,  my rep,  and a bunch of others.  

Update 11-1-18:  I voted early,  because next week (election day is next week),  my dementia-afflicted mother is being moved to a nursing home,  and I am undergoing (hopefully-minor) cancer surgery (Update 11-7-18:  they got it).  I wanted my vote to count,  no matter what!!!  Split ticket as usual,  biased in favor of the opposition,  in large part. 

Please,  get out and vote yourself !!!  Make your voice heard !!!   If your opinion about any given race is not too strong already,  I recommend you try to determine which candidate might prioritize the good of his constituents above the advantage of his party.  Way too few do. Update 11-7-18:  clearly too few did.

Thursday, October 18, 2018

Taking a Knee Is Way Over-Politicized

I see too much influence of sometimes-vicious political propaganda regarding football players protesting by taking a knee (or locking arms) during the national anthem.  That propaganda says they are disrespecting the flag and the nation by not standing;  I disagree.

I don’t see any of that supposed disrespect.  None of these players are talking or laughing,  unlike many in the stands!  Their attention is quietly focused on the anthem ceremony,  just as it should be.  Only their posture is “wrong”,  and that is the attention-getting item that makes the protest successful. 

Protest is indeed as American as apple pie.  This nation was quite literally born out of protest!  The most famous of these protests was the Boston Tea Party,  but there were many over several years,  before the shooting started that became the American Revolution. 

The protest issue itself aside,  what’s different here is the utter lack of any real collateral damage!  Most protests as we have known them lead to people getting hurt or property damage being done.  Nobody is hurt,  and no damage is done,  when these players kneel! 

I applaud that;  it’s the most beneficially innovative form of protest I have ever seen.  Of course,  it’s television showing it,  that makes it as effective as it is. 

As for the protest issue,  the statistics verify that something is indeed wrong with equality-of-justice in this country.  It’s probably a lot more complicated than any one explanation,  things usually are.  

But if there’s a problem,  simple ethics demands we investigate and try to correct it. 

The protest exists because we haven’t been paying attention to this problem.


To support my point,  here are two photos taken during the anthem ceremony at a couple of football games.  The first is fan behavior,  which is largely pretty good.  Most are standing,  some are singing. 

I see some crossed arms (usually symbolic of disapproval of,  or impatience with,  what is going on),  a few talking instead of singing or paying attention,  and at least one individual paying attention to a cell phone instead of the ceremony (dead center,  about 3/4 of the way down the photograph). 

The second is of players,  which are kneeling in protest.  All are quiet,  and all are focused on the ceremony.  Other than the “wrong” posture,  where is the disrespect?  No one is laughing or talking,  no one is focused on anything but the ceremony. 



Friday, October 5, 2018

Space Radiation Risks: GCR vs SFE

Update 11-4-2021:  From AIAA’s email newsletter “The Daily Launch” for Thursday 11-4-2021:

Sun Produced Three Coronal Mass Ejections Since Monday

SPACE (11/3) reports that the sun has produced three coronal mass ejections (CMEs) since Monday. On Monday and Tuesday, “a sunspot designated AR2887 unleashed two of these outbursts. Then, later in the day on Tuesday (Nov. 2), a second sunspot called AR2891 produced a CME as well.” The third ejection is moving more quickly than the two others, “so it swept through all of one previous CME and part of the other.” Scientists predicted that the resulting CME would arrive at Earth Wednesday “and produce geomagnetic storms beginning on Thursday (Nov. 4).”

My take on this:  This is exactly why any manned spacecraft or space station outside the Earth’s magnetic field absolutely must have a radiation shelter or shielding for its crew.   All it takes is a big one of these to kill a crew.  There was one between two Apollo moon landings in 1972.

Update 8-27-2021:

From AIAA’s “Daily Launch” email newsletter for 27 August 2021:

Scientists Suggest Safest Time For Mars Travel

CNET News (8/26) reports that a new study published this month offers suggestions on how to avoid hazardous radiation on a trip to Mars. UCLA said Wednesday that “The scientists’ calculations demonstrate that it would be possible to shield a Mars-bound spacecraft from energetic particles from the sun because, during solar maximum, the most dangerous and energetic particles from distant galaxies are deflected by the enhanced solar activity.”

This news item makes sense only when you realize that there are two space radiation threats,  not one.  They are entirely different in characteristics,  but linked.  The galactic cosmic rays are a very thin drizzle of extremely energetic particles,  which are very difficult to shield,  without making the problem worse with localized floods of secondary radiation created by these particles hitting your shield. 

The solar activity is a threat with large eruptions coming from the sun.  These are far less energetic particles,  but they come in utterly enormous floods,  such that the radiation dose is quite lethal very quickly.  But,  being lower-energy,  they are much easier to shield. 

The linkage between them is that when solar activity and the threat of solar eruptions is higher,  the solar wind itself deflects more of the cosmic rays,  reducing that threat to easily-tolerable values.  To travel during periods of high solar activity,  you must have radiation shielding against solar eruption radiation,  but the radiation overdose threat is actually lower,  because it is an easier type of radiation to shield against.

On the other hand,  if you fail to shield against solar activity eruptions,  you will kill your crew during the mission if such an eruption strikes their vehicle in space.  The slow,  drawn-out exposure to galactic cosmic rays raises the risk of cancer later in life,  long after the mission is over.

The point of this update is that I am not alone in my understanding of this threat.  That understanding is documented here in this article,  and an earlier one posted in 2012.


original article starts here:


I got my data on risks and passive shielding from NASA’s own site and documents.  See

http://srag.jsc.nasa.gov/Publications/TM104782/techmemo.htm, titled Spaceflight Radiation Health Program at JSC (no cited reference newer than 1992).

or go to http://exrocketman.blogspot.com and click on year 2012 then May 2,  for the article titled “Space Travel Radiation Risks”.  That article,  which I wrote and posted,  abstracts the most relevant information from the NASA source for the questions at hand. 

Two Risks:

There is galactic cosmic radiation (GCR) and there are solar flare events (SFE).  GCR is a very sparse trickle of extremely high-energy particles (mostly protons) that are very hard to passively shield,  and which can induce secondary showers of other dangerous particles in some materials.  The risk is modulated by the solar wind which varies with the solar activity level.

SFE radiation is mostly proton and heavier particles emitted from the sun sporadically,  from eruptions on its surface.  These come in very concentrated but brief events,  comprising much lower-energy particles that are far easier to passively shield. 

GCR:  Roentgen equivalent man (REM) per year  = 42 + 18 sin(360o (t, year)/ (11 year)),  max 60 at solar min,  min 24 at solar max.  Solar max is max sunspot activity,  with more frequent eruptions.  Although,  eruptions can occur throughout the cycle.

SFE: from 1968 to 1970,  events every month or so ranging from 2 REM to 50 REM accumulated during each event;  from 1970 to 1972,  events about every 6 months ranging from about 50 REM to about 100 REM accumulated during each event;  and in 1972 right between Apollo 16 and Apollo 17,  one event right at 5000 accumulated REM.  There was one event of about 5 REM during Apollo 16.  Figure 1 is a plot of SFE events during the Apollo program,  direct from the NASA document’s Figure 10.  The quoted numbers are for somebody outside a spacecraft wearing only a spacesuit,  per NASA’s figure.

By way of comparison,  the Earthly natural background in the US is near 300 milli-REM (0.30 REM) per year. Worldwide is not significantly different. 

A rough rule of thumb:  500 REM accumulated in a short time (hours or days) is considered lethal to 100% of those so exposed. 

NASA’s Astronaut Exposure Rules:

These vary with the affected organ (eyes,  skin,  and 5 cm inside the body as representative of blood-forming organs or “BFO”),  but the lowest values are for 5 cm inside.  NASA’s exposure rules limit exposure to 50 REM accumulated in any one year,  25 REM in any single month,  and a career limit that varies with age and gender,  but peaks at 400 REM accumulated over an entire career. 

These are illustrated with Tables 1 and 2 lifted from the NASA document,  and presented here as Figures 2 and 3,  respectively.  Use the equations in Figure 3 to calculate career limits.  These exposure limitations represent approximately twice the exposures nuclear workers are allowed to face,  with a single-digit percentage increase in cancer risk expected. 

 Figure 1 – SFE Events During Apollo,  from the NASA Document’s Figure 10

 Figure 2 – NASA Time Interval Exposure Limits

 Figure 3 – NASA Career Exposure Limits (Use the Equations)

Effectiveness of Shielding Materials:

These divide into the effects of aluminum,  water,  and hydrogen,  which fairly well bounds a lot of possible materials.  The true risk here is the SFE event, of a very large magnitude,  such as the 5000 REM 1972 event.  That’s outside in nothing but a space suit.  Inside the command module,  the effect of the spacecraft structure reduces the exposure to 500 REM.  That’s a 10:1 reduction for the spacecraft hull (remember,  SFE particles are lower-energy and far easier to shield passively).

Based on the NASA document’s Figure 9,  given here as Figure 4,  the plot for the 1972 event reduces 500 REM inside the command module to 20 REM at 20 g/cm2 of aluminum shielding added to the effects of the spacecraft hull.  Use the density of aluminum (2.7 g/cm3) to find the actual physical thickness of this aluminum to be 7.4 cm.  You would want an aluminum shield that thick or thicker to survive a 1972-magnitude SFE event,  and stay barely within the month exposure limit.

The effect of the various materials as passive shielding for GCR is given in Figure 5,  which is lifted from the NASA document’s Figure 6.  In terms of shield mass per unit area of hull,  hydrogen is the most effective,  and aluminum the least,  with water in between.  Note how the curves flatten at larger masses per unit area,  leading to stronger differences in the amount of shield material required.

Here we ignore the shielding effect of the spacecraft hull structure as negligible against the more energetic radiation.  For 20 g/cm2 (7.4 cm thick) aluminum,  60 REM/year reduces to 40 REM/year,  which is well within the annual limit.  You get the same exposure at only 10 g/cm2 water at 1 g/cm3,  which is 10 cm thick,  and 3 g/cm2 hydrogen,  which at .07 g/cm3 is some 43 cm thick. 

The problem with “over-killing” the shielding is the secondary shower of dangerous particles created by the high-energy GCR particles.  This gets to be a problem if you make the shield too thick,  and it simply doesn’t happen with the lower-energy SFE particles.  That makes passive shielding a real trade-off for design purposes.  This is less a problem with spacecraft design,  and more of a problem with surface habitation design and construction.  The temptation would be to pile too much regolith atop the roof,  causing the secondary scatter problem.  

 Figure 4 – Effectiveness of Aluminum Against SFE Events,  from NASA Document Figure 9

Figure 5 – Effectiveness of 3 Materials Against GCR,  From NASA Document Figure 6

My own recommendation would be to use 15-20 g/cm2 water,  some 15-20 cm thick,  which would reduce 60 REM/year GCR to about 30 REM/year.  Against the GCR,  the same protection obtains at some 50 g/cm2 aluminum,  which is about 18.5 cm thick.  These are similar thicknesses (15-20 cm water vs 18-19 cm aluminum),  but very different masses per unit area:  15-20 g/cm2 water vs 50 g/cm2 aluminum.  Water is simply the lighter shield for the same effect, by about a factor of 2.5 to 3.   

We don’t have anything but aluminum to look at in Figure 4 the for the SFE event.  At the same 50 g/cm2 aluminum that looks good against GCR,  the 500 REM SFE event,  as measured inside the command module,  gets reduced to a 2 REM/event exposure.  Assuming the same attenuation ratio and mass per unit area ratio between aluminum and water that we saw with GCR in Figure 5,  then we should see the same 500 REM to 2 REM reduction of SFE radiation that 50 g/cm2 of aluminum provides,  with only 15-20 g/cm2 water,  which is 15-20 cm thick.  That’s an assumption requiring verification

Lessons for Spacecraft Design:

Water is the best shielding material,  because it is the lightest,  while providing practical thicknesses,  unlike hydrogen.  My best guess is that storable propellants should resemble water in their shielding properties.  They are light molecules made of light atoms,  like water,  and have densities far more comparable to water than to liquid hydrogen.

The recommended water shield is 15-20 g/cm2 (15-20 cm thickness),  which could be water,  wastewater,  or even frozen food.  It could also be storable propellants like the hydrazines and NTO oxidizer.  Increase the thicknesses for wastewater,  ice,  or frozen food:  a good guess is a factor of 1.5 to 2 increase in thickness over straight water.

Against GCR and ignoring any effects of the spacecraft hull,  15-20 cm of water should reduce 60 REM/year of GCR to something near 30 REM/year.  This might,  or might not,  be practical for the entire spacecraft,  but putting water in one form or another around the sleeping quarters might be,  in addition to a designated radiation shelter space.  

There is some benefit of the spacecraft hull reducing SFE from a 5000 REM/event outside the hull to a 500 REM/event inside the hull.  Since that is still a lethal dose,  further shielding is absolutely required!  That same 15-20 cm of water should reduce an inside-the-hull 500 REM/event to something nearer 2 REM/event,  which is well within the monthly limit,  even if multiple such events occur spaced rapidly together.  This gives us a lot of margin in the case of an event far larger than the 1972 SFE event.

Any spacecraft design should incorporate its flight control station within the designated-shelter radiation shielding so that critical maneuvers may be flown regardless of the solar weather.  Shielding about the sleeping quarters is also recommended for purposes of reducing GCR exposure. 

By using the shadow-shield effect,  this kind of shielding might be obtained with a combination of water/wastewater/frozen food items located about the sleeping quarters and flight control station,  combined with propellant tanks for the next burn,  that are docked about the periphery of these regions,  outside the spacecraft hull.  These are all items you already must have,  anyway,  so that extra shielding mass is not added to the design.  See Figure 6 for a concept sketch.

 Figure 6 – Concept for Incorporating Propellants and Water-Based Materials as a Shadow-Shield

Exposures Calculated for a Mars Mission at 60 REM/Year GCR with Three 1972-Class SFE Events:

The mission is 9-month transit/13-month near (or on) Mars/9-month transit.  One SFE event occurs during each transit,  and the other occurs while the crew is on or near Mars.  Calculations are made with and without the sleeping quarters shielded,  for 1/3 of clock time during each day.  Shielding about the sleeping quarters and the designated shelter is spacecraft hull plus 15-20 cm water-equivalent for SFE,  just 15-20 cm water-equivalent for GCR.  How this might actually be done was shown conceptually in Figure 6 above.

The first radiation exposure year is 3 months pre-mission on Earth,  then 9 months in transit to Mars.  The second radiation-exposure year is 12 months on Mars.  The third radiation-exposure year is one month on Mars,  9 months in transit to Earth,  and 2 months post-mission on Earth.  Earthly exposure is at the 0.3 REM/year rate.

The 9 month transit is 0.75 year.  Without any shielding effects at all,  45 REM are accumulated during transit for the year in which transit occurs. 

If there is sleeping quarters shielding,  its presence cuts the GCR to a rate of 30 REM/year while sleeping. Then based on clock times,  a 2/3-1/3 split occurs between the 60 and 30 REM rates:  that is a rate of 50 REM/year applied to a 9 month transit.  Thus the crew accumulates 37.5 REM during the transit,  which goes toward the total accumulated exposure during the year in which the transit takes place.

While on or near Mars,  the planet blocks half the spherical “sky”,  for a net in-space unshielded GCR rate,  assumed unattenuated by the planet’s atmosphere,  of 30 REM/year,  accumulated during each year spent on Mars.  The stay is 13 months,  so without sleeping quarters shielding,  30 REM counts toward the first full year on Mars,  and one month’s worth (2.5 REM) counts toward the second year on Mars and in-transit home.   

If there is shielding about the sleeping quarters on Mars,  the same 2/3-1/3 split applies to rates of 30 and 15 REM/year,  reducing the effective exposure rate to 25 REM/year.  In that case,  the year on Mars accumulates 25 REM,  and the 13th month accumulates 2.1 REM. 

Add 2 REM to the accumulation in any one month for SFE events during the transits and during the stay on Mars.  There must be a designated radiation shelter for SFE events,  even while on Mars,  or the exposures could easily be lethal.  That assumes no attenuation of the radiation by Mars’s thin atmosphere. 

The result is depicted graphically in Figure 7.  Again,  shielding is 15-20 cm of water-equivalent.  

Figure 7 – Radiation Profiles for 15-20 cm Water Shield,  with or without Sleeping Quarters Shield

These results show a marginal yearly exposure during year 3,  at just barely under the 50 REM annual limit,  for the case of no sleeping quarters shielding.  With sleeping quarters shielding,  this reduces well under the limit.  Worst case monthly exposures are well under the limit for both cases.  Two such missions will approach career limits,  in either case. 

Note that if there is no shielded place for SFE events,  then during any event in the same class as the 1972 event,  the exposure will be fatal at 500 REM received over a matter of hours.    There simply must be a solar flare shelter somewhere.  This is true during the transits and on Mars.

Note also that during times when the GCR is under 60 REM/year out in space,  exposures inside the ship (either case) will be much lower.  It is only the worst-case 60 REM/year space environment that is analyzed here.

Note also that it is the shorter-than-a-year transit time that reduces in-transit unshielded exposure to 45 accumulated REM!  Extending the transit time by using repeated aerobraking passes to capture at Mars,  instead of a one-time rocket burn,  will quickly violate the annual exposure limit!  The same thing applies to electric propulsion using spiral-out/spiral-in flight plans.  (Not to mention exposure times passing through the Van Allen Belts at Earth.)

Once the unshielded one-way flight time exceeds 10 months,  the annual exposure limit gets exceeded in a max GCR year.  Once that long-transit situation obtains,  you must shield the entire habitable volume of the ship,  not just a designated shelter and perhaps the sleeping quarters. 

Finally,  if the entire habitable volume of the spacecraft could be shielded at the 15-20 cm water-equivalent level,  exposures would be cut essentially in half,  to only around 30-something REM per radiation-exposure year in the transits,  and 15 REM/year on Mars,  even in a 60 REM/year part of the solar cycle.  Year 1 would be 32.08 REM,  year 2 would be 17 REM,  and year 3 would be 33.3 REM,  for a mission total of 83.4 REM.  Three,  or possibly even 4,  such missions in 60 REM GCR years might be feasible,  before hitting career exposure limits.  

Final Comments:

First,  this kind of radiation shielding will inevitably prove to be absolutely necessary,  but it will look nothing at all like what we have ever before done with our spacecraft designs.  When “they” show you spacecraft design concepts that look like what we have done before,  you already know that ”they” have not thought this problem through!

Second,  the shield design concept shown in Figure 6 above is entirely compatible with a “long” ship design that is spun end-over-end like a rigid baton for artificial gravity.  A design like that is also entirely unlike anything we have ever before done,  but it is rather well-understood from an engineering viewpoint,  and would require far less technology development and demonstration than any sort of cable-connected spin gravity design.

Third,  it is quite evident that worst-case GCR risks are slight over-exposure for late-in-life cancer,  while the SFE risks really are lethal doses leading to an ugly death within hours.  Thus,  when “they” point to GCR as the radiation risk that precludes humans going into deep space,  you already know that (1) they are lying for nothing but fear-mongering purposes,  and (2) “they” are truly ignorant of the real radiation risk.  Such claims are simply not credible.

Wednesday, October 3, 2018

On the Senate Kavanaugh Accuser Hearings

Cases like this are supposed to be settled in a proper court of law,  not the "court" of public opinion.  Before the 24/7 news "cycle",  the media were not so insistent on trying these cases in the "court" of public opinion. 

The "court" of public opinion is not a cousin,  but a sibling,  of lynch mob justice!  That has a very poor track record at determining true outcomes,  which is why we supposedly outlawed it (except that the media and our political figures have brought it back). 

And don't kid yourself,  an open Senate hearing is nothing but another “court” of public opinion.

The proper way of dealing with this would have been to do the police investigation,  and present the results to a grand jury.  If worthy of an indictment,  then go to trial with it.  If not,  safely discard the issue.

Meanwhile,  if the accused is a public figure being considered as a nominee for a judicial post,  then (1) he is innocent until proven guilty,  but (2) you don't want to have to unseat him for a conviction,  afterwards,  if he does go to trial.  It is difficult to unseat judges,  even with proven misbehavior.

What that really means is that you put the nomination on hold,  until you find out from the real courts of law whether he really is innocent or guilty.  I'm sorry,  that is the wisest choice,  and it is best for the good of the country.  Simple common sense says so.  Very inconvenient for party advantage,  though.

We seem to have so very few who prioritize the good of the country above party (or personal) advantage anymore.  My advice is vote only for those who would prioritize highest the public good,  regardless of their party membership.  All else pales in comparison.