I think that just like catalysator was added to the car engines, by requlatory dictat jet engines could be required to have injection nozzle that automatically activates when the plane reaches a certain altitude. It took over a decade to get catalysators fully deployed in cars. It might not be practiceable in jet engine retrofit, but for all future planes it would be fine.
I am not convinced that a specialist stratospheric planes should be as the starting point. Remember both supersonic Concorde (English/French) and Tupolev Tu-144 civilian aircraft have been mothballed and taken out of active service due to cost consideration. It remains my view that even if subsonic commercial jetliners had 90% shorter athmospheric half-life in spreading sulphur or carbon silicates, this would be a break-even point as supersonic jets are 10 times more costly. Remind my practical allegory from Farnborough Air Show when the manager felt it was still more sensible to leave brochure cases back and send someone to pick them up with several hours drive by a packet van, rather than dumping them to the back seats of the helicopter and go home at once after the event. Similarly, NASA uses nose diving subsonic jets for some short duration microgravity experiments, rather than loaded them on space shuttle or boarded on the ISS. What is ideal is not always cost effective. If I can hire a commercial jet, so it should be easiest to assume that universities would find it also easier to fund such a flights. In my experience, commercial flight at 11,000 metres (33,000 feet) is at least 10 times cheaper than planes that go above this (as these are not standard civilian aircrafts). So my question remains, is the half-life at 11,000 metres over 10 times shorter, or not, to justify ultra-expensive stratospheric specialist flights. It may also boil down as VHS versus BETA. The latter was far more sophisticated, but due to former's established presence it won the old video recorded market, whereas the more compact beta lost it. A plain stupid commercial jetliner is a far easier to sell as practical idea. For political reasons, I would suggest any nozzle would not be switched on below toposphere. The open skies really begin above that. 8,000m 13,000m 18,000m 23,000m 28,000m 9,000m 14,000m 19,000m 24,000m 29,000m 10,000m 15,000m 20,000m 25,000m 30,000m 11,000m 16,000m 21,000m 26,000m 31,000m 12,000m 17,000m 22,000m 27,000m 32,000m Can someone give me the following figures: (a) athmospheric half-life of the substance at this altitude, (b) quantity you want to load for the plane? I will be able to to give to cost of such operation. I will look into balloon costs separaterly from jets. Please lets not build hose of straws relying on some magical plane to be developed for us to do the trick. Otherwise it is just another concept car we try to do research which will never see daylight in use. So far, all electric concept cars have proven my point. There is no climate solutions from concept oriented reasearch, but solutions oriented which have a clear costing and cost comparison. Kind regards, Albert From: [email protected] To: [email protected] CC: [email protected] Subject: Re: [clim] RE: [geo] The problem with stratospheric SRM Date: Sat, 23 Oct 2010 07:21:48 +0100 Thanks for the support, but I now think any thought of commercial fight use is just wildly premature at the moment. For now we need to concentrate on the practical, one off, development of the ways of distributing particles at the heights required. Trivial amounts of research money are required for this but so far I cant get any. Grant proposal attached again. johngorman ----- Original Message ----- From: Veli Albert Kallio To: David Keith ; [email protected] ; [email protected] Cc: [email protected] ; [email protected] ; Geoengineering FIPC ; [email protected] ; Climateintervention FIPC Sent: Thursday, October 21, 2010 3:24 PM Subject: RE: [clim] RE: [geo] The problem with stratospheric SRM Note that Gorman has proposed direct formation of silicates in commercial aircraft exhaust, following earlier suggestions of sulfur in jet fuel. Commercial aircraft don’t flight at the right height or location to efficiently deliver materials to the stratosphere. You need to be in the tropical stratosphere get reasonably long lifetimes, this requires altitudes beyond about 18 km. I think it is a very important fact to bear in mind that the stratospheric flights are specialist flights, whereas the commerical flights to certain extent will have a free-ride. One could argue equipment added on same basis as catalysators on cars through regulatory directive. This would effectively ensure a free ride, even though the flotation half-life would be very much shorter. This recalls my experience at Farnborough Air Show where we were looking Locheed Martin F-130 Hercules aircraft and Sikorsky Helicopters. At the end of the meeting, some of the staff suggested a Sikorsky ride home to take down the stuff at the air show by chopper. But then the manager said no, we pack all stuff to packet vans and drive back and forth several hours to-and-fro (even though immensely multiplying the task of taking stuff home.) As per the above experience, I have doubts about the practicality any specialist stratospheric flight programme by specialist aircraft: (even if it delivers ten or twenty times longer flotation half-times in stratosphere to the commercial flights). If spraying carbon tetrasilicate, sulphur dioxide, or H2S, or H2SO2 the cost of speciality flights may count against the ideal delivery such a way in quantities. Have anyone look at cost / half-life ratios if the startospheric flights would still end up as more expensive? A commercial air craft flies at 11,000 metres: Wouldn't it make more sense to say that planes flying above, say, troposphere would be required by law to have an injector installed in them, which should be switched on when above say 8,000, 9,000, 10,000 or 11,000 metres? Any feedback from this pragmatist viewpoint? Kind regards, Albert From: [email protected] To: [email protected]; [email protected] CC: [email protected]; [email protected]; [email protected]; [email protected]; [email protected] Date: Thu, 21 Oct 2010 07:04:06 -0600 Subject: [clim] RE: [geo] The problem with stratospheric SRM A few comments on microphysics of stratospheric aerosols. We have examine the microphysics in a recent GRL paper. We confirmed earlier findings that the standard SO2 injection can be surprisingly ineffective because most of the sulfur is deposited on existing particles making them too large. We proposed a solution, injecting H2SO4 directly and showed that in the same modeling framework it worked far better than SO2. (Better=less sulfur mass to get same forcing, plus weak ozone surface-area benefits). This can be generalized to other condensable vapors. The paper is enclosed along with slides that may be helpful. N.B., we have reexamine assumptions and discovered an minor error in the original calculation, as it happens the new results make the direct H2SO4 scheme look a bit better, the figure on the slide is the new version. We also reexamined ozone loss, this effort was directed by Thomas Peter, one of the collaborators on the paper who runs a major stratospheric chemistry group. We have examine the engineering with an aircraft engineering group and found no first-order problems (that report will be released soon). I don’t think H2S would help. It has the same disadvantage as SO2. Note that Gorman has proposed direct formation of silicates in commercial aircraft exhaust, following earlier suggestions of sulfur in jet fuel. Commercial aircraft don’t flight at the right height or location to efficiently deliver materials to the stratosphere. You need to be in the tropical stratosphere get reasonably long lifetimes, this requires altitudes beyond about 18 km. Yours, David From: [email protected] [mailto:[email protected]] On Behalf Of Oliver Wingenter Sent: Sunday, October 17, 2010 7:39 PM To: [email protected] Cc: Ken Caldeira; [email protected]; geoengineering; Wingenter Subject: [geo] The problem with stratospheric SRM Dear Ken, The problem is after the initial injections, i.e. the second yea of GE, can we even create new particles with a background now 15 to 25 times higher with or with out nucleation sites? Under the present sulfate schemes it appears not. in order to "tune in" particle size and number ternary nucleation of sulfate, water and perhaps ammonia (NH3) will probably need top be invoked. Let us remember that water vapor is not finite in the stratosphere and as more particles are produced additional sulfate will be needed to reduce the vapor pressure of the aerosols. An additional species such as NH3 could help over come this limitation. Injection of H2S would lead to greater dispersion of sulfur, allowing more particle growth but is not considered in stratospheric SRM paper to date because the microphysics involved in most modeling studies has not yet been considered. The actual formation of particles in models of the stratosphere as a result of geoengineering has yet to be established. This is it greatest priority of SSRM at this time. Sincerely, Oliver Wingenter On 10/17/2010 3:41 PM, Ken Caldeira wrote: Yes, you could produce even more new particles yourself which would inhibit new particle production from someone else's emissions, but presumably the total particle count would be higher at the end of all of this than if you did not intervene. Would it be possible to act on someone else's particle production in a way that would lower overall particles counts? On Sun, Oct 17, 2010 at 1:50 PM, Oliver Wingenter <[email protected]> wrote: Dear Josh, If the concentration of background particle were large enough, a few hundred particle per cm3, then this would inhibit new particle production. At least this is case in the marine boundary layer. I understand that stratospheric microphysical models are having trouble making new particles. However, adding NH3 would allow ternary nucleation tens of thousands of times faster than sulfuric acid and water alone as is seen in the free troposphere. In terms of a volcanic eruptions like Pinatubo, I wonder how much ash made it to the stratosphere and provided nucleation sites? Sincerely, Oliver Wingenter On 10/17/2010 12:29 PM, Ken Caldeira wrote: Multiple, independent injections would decrease the likelihood of coagulation relative to injecting it all in one place. Of course, there is potential for coordinated injections to decrease coagulation (aggregation) relative to uncoordinated injections. There is no evidence that I know of that one injection could "cancel out" the effects of another injection. It seems that the main case is that the climate effect of A+B would be less than the climate effects of A plus the climate effects of B. It is an interesting research question to understand whether there are countermeasures that would decrease the effectiveness of injection by injecting something upwind from an injection site that would promote aggregation of the injected material. ___________________________________________________ Ken Caldeira Carnegie Institution Dept of Global Ecology 260 Panama Street, Stanford, CA 94305 USA +1 650 704 7212 [email protected] http://dge.stanford.edu/labs/caldeiralab @kencaldeira On Sun, Oct 17, 2010 at 10:43 AM, Josh Horton <[email protected]> wrote: Hi everyone, I am finalizing a chapter on geoengineering policy for publication and would greatly appreciate informed feedback on the following paragraph: "The aerosol most commonly suggested for stratospheric injection is sulfuric acid. Plans call for delivering sulfate aerosols by dispersing gas-phase precursor materials. Precursor oxidation and aerosol formation involve complex processes with the potential to reduce the effectiveness of stratospheric insertion. For instance, coagulation could lead to excessively large sulfuric acid particles that sediment out of the stratosphere, neutralizing the effect of the initial dispersion. Multiple, independent injections would increase the likelihood of such unintended consequences. Unsynchronized staging, scheduling, and delivery of sulfate aerosol injections would magnify the potential for perverse particulate interactions, and might jeopardize the success of geoengineering deployment. Lack of policy coordination may result in separate injection schemes that effectively cancel each other out." For those with scientific/technical backgrounds, is this a sound argument? Is the basic science correct? I am outside my comfort zone with this and want to be sure I don't miss the mark. Thanks to anyone who can offer insight. 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