I believe that you will find that rail guns are rather more developed than you 
believe but all of it is classified and basically you will hit a brick wall if 
you want to delve into this further. But I don’t think you are going to need 
rail guns. Make a solution of calcium chloride. This will give you freezing 
protection down to -52 C.  Suspend in the solution precipitated calcium 
carbonate (less than 2 microns) and then pump this up to the desired height 
using a balloon tether. I am assuming the antifreeze properties should be 
enough but I don’t know the height. 2 microns or less particles in a high 
density fluid like calcium chloride solution won’t settle out at any speed that 
is likely to give you problems.  If you need greater freeze protection, there 
are other salts that can be used to reduce the freeze point further. The 
engineering challenges on this don’t seem all that bad and a lot easier and 
cheaper than liquid nitrogen. 

 

A number of carbon capture processes can also produce precipitated calcium 
carbonate, so this could be a useful double kick.

 

 

David Sevier

Carbon Cycle Limited

248 Sutton Common Road

Sutton, Surrey SM3 9PW

England

Tel 44 (0)208 288 0128

Fax 44 (0)208-288 0129

 

This email is private and confidential 

 



 



 

 

 

From: Andrew Lockley [mailto:andrew.lock...@gmail.com] 
Sent: 16 October 2017 21:18
To: Doug MacMynowski
Cc: geoengineering; David Sevier; Hugh Hunt
Subject: RE: [geo] Engineering drama, post CEC

 

To reply specifically with likely issues :

 

AFAIK the liquid/gas column behaviour in the balloon pipe is problematic. Hugh 
Hunt (cc) has, I believe, worked on this aspect of the viability. The adiabatic 
cooling causes a temperature reduction, as the hydrostatic pressure drops. This 
requires heating to a problematic temperature. 

 

Rail guns are problematic for a range of reasons, not least their lack of 
development. They are highly prone to wear, and aren't particularly suited to 
launching large payloads. I've worked on gas guns, which have more suitable 
performance characteristics.

 

Generally, I don't take the view that engineering is trivial. I think we should 
engineer early, and with the same enthusiasm as we apply to other aspects. 
Engineering is trivial when it's done, not when it isn't. 

 

A

 

On 16 Oct 2017 18:53, "Douglas MacMartin" <macma...@cds.caltech.edu> wrote:

The start was Andrew’s email, which was based on a presentation given at CEC17 
(sorry, there weren’t any viewgraphs, but you’ve already got the summary).

 

There’s nothing inherently “wrong” with any approach.  Eventually we’ll need a 
more serious engineering analysis of different options (i.e., beyond 
speculation).  IMHO that day isn’t now, I’m satisfied with knowing that it is a 
solvable problem.

 

Re material, yes, various other materials have definite advantages with respect 
to either stratospheric heating or ozone loss.  But there’s also a big 
advantage with using something that exists naturally in the stratosphere, as 
that at least gives an argument for bounding uncertainty.  I think it is rather 
premature to say one makes “more sense” than another right now, as there are 
different (and somewhat non-commensurate) concerns.

 

From: geoengineering@googlegroups.com [mailto:geoengineering@googlegroups.com] 
On Behalf Of David Sevier
Sent: Monday, October 16, 2017 1:46 PM
To: andrew.lock...@gmail.com
Cc: 'geoengineering' <geoengineering@googlegroups.com>
Subject: RE: [geo] Engineering drama, post CEC

 

I am struggling to find the beginning of this thread. What are you guys talking 
about exactly. What is wrong with pumping up a tube as so many have suggested 
or using rail guns to launch packages into the higher atmosphere. In the latter 
case, fine particles of chalk (such a PCC) make more sense than sulphuric acid.

 

From: geoengineering@googlegroups.com [mailto:geoengineering@googlegroups.com] 
On Behalf Of Greg Rau
Sent: 16 October 2017 17:23
To: andrew.lock...@gmail.com
Cc: geoengineering
Subject: Re: [geo] Engineering drama, post CEC

 

But as to the pile of papers, just think of the carbon storage!

G

Sent from my iPhone


On Oct 15, 2017, at 4:19 PM, Andrew Lockley <andrew.lock...@gmail.com> wrote:

>From what I gather, it seems we have a bit of engineering drama. Apparently, 
>you can't just swap aircraft engines and do SRM, because the wings aren't 
>right on any aircraft with even a vaguely adequate payload.

 

This is A Problem. 

 

We've either got to 

A) engineer a new aircraft, like the Delft team did (with a $100m expected 
development cost)

B) work out a way to make new wings for an existing jet (not simple) 

C) come up with something else 

 

If we assume it's C, then there's quite a lot decent new hardware around. One 
choice is Blue Origin/Space X kit. Does anyone know how that would fare in an 
up-and-down flight path? I know Blue Origin did that before. Payload should be 
manageable, but I'm not sure how costs are coming down. 

 

Another alternative is one of the hybrid concepts. I got a flea in my ear for 
mentioning BAE systems hybrid engines before. However, their power in thin air 
may make them suitable for geoengineering use - either as zoom climbers or 
cruise. 

 

I know that current thinking is to condense H2SO4 directly, but I guess with 
any kind of zoom climb, you're pretty much stuck dumping bulk SO2 and crossing 
your fingers it doesn't all coagulate to baseball-size and drop out!

 

Would be great to hear from people on the list. 

 

(Personally, my concern is that our best option for accessing the stratosphere 
at the current rate of engineering might be to make a large pile of climate 
engineering governance papers, and walk up that carrying gas tanks! There will 
soon be enough of them  ;)  ) 

 

Andrew 

 

 

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