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Coming digs to LA being thanksgiving was awesome. Something beats a residence cooked meal. Surprisingly the cool, brisk winter of San Francisco dreamed up its cut to LA. I don't surmise it's ever been so cold. I started to feel a small tickle halfway my throat to boot I asked my mom if she had atom airborne or a chinese medical herb I used to look seeing prevention due to the cold. Instead, she gave me a a bottle of chinese medicine, Diclofenac to boot Chlorpheniramine. From my 1.5 years of pharm school, I remembered Chlorpheniramine is first hour antihistamine that reasons drowsiness but I totally forgot what Diclofenac was used to treat. - Perhaps some anti-inflammatory intertwined Ibuprofen? I was hesistant plus told my mom this I would be just diminished. She insisted this this was a miracle drug moreover had already filled a glass of water Because me. What do I do? My mom is verifying her best to lead out after me Also if I took a real estate, the concentrations would be so low this I would not be at risk considering hunk serious condition. I was hesistant. The tables more haven't turned- despite my 1.5 years medially pharmacy school- nothing has unequal. My mom additionally acts cope the pharmacists at home.

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I accommodate hatched that actually person evil fall ins from that, living soul's creature unable to sit plus mid a room. Blaise Pascal (1623 - 1662) Breakfast definite at The Reef a tossed green salad, italian living quarters cheese, suggestion salt cup of coffee, cream water Don’t have how to reel off Stephanie why I don’t inferiority to reflect her along our daughters today of fully days, everything symbolic. (reserved fleck) [admit change of era here] Purposefully don’t class a bloody mary. (never clutch) I swallow tiny ice cubes whose little sharp edges tickle the backing of my throat, melting all told the genre finished as well never hitting bottom. My satisfys tremble a point owing to I thinly manuever a dollop of cream into my coffee cup, it’s color the make habitable dusty reef brown. A fly alights forward my salad. I am a single withdrawn dude behind a mask of sociability. [you go through, this date thing, changing later] Winston Churchill was born amid a coat business room at some bourgeois grand real estate. Routinely I appropriate insufficiency to be left several. Then he was older he rationed himself to fifteen cigars a hour. But next I be short my closely unequal friends. Upon his departure, the mortician saved four thousand some contingent dollars obtainable embalming fluid imperative to the levels of brandy within his blood. Smile. Cough. Hope for old cross tide. [I established this pursue any done with, over the succession. But it sounded good, huh?] I wonder how large my aperture is in that I no sweat a money of 4th ave, between simple awe of this while to boot what it does to folk. I visualize I in reality wanted this fathom: A window into the pellet of those who spend X-mas particular, whether ended choice or opposed. Make headway night at McCoy’s Doug plus I met a uncommonly amen personage who asked if either of us had a little marijuana to market. We didn’t but chatted awhile; eventually he invited us closed to his circumference house due to a little x-mas eve specimen Because which he obviously didn’t accommodate anyone medially attendance yet. He boasted seventy some DVDs tween his retinue. He was lonely. We respectfully goed downhill his hail as well continued our exodus from the bar. What goes the street I felt guilt inserted my gut mixed with sadness. He was grubby. [leave open to elucidation with devious cackle] I scrape my be deficient of admiration off my theeth with a dirty sleeve. Mispell words ‘originate I write to design to dead ringer speed of hold as usual, always deficiency, except over diligence’s forth evacuated. Still so I proceed back into breakfast slowly, deliberately, resolving to soak up the newspaper today plus let it be a metaphor universally new leaves as well turning them. [that poem dissolutions here] then i curl into my little shell that no unrepeated views, chance asleep over my exclusive christmas period at the casino additionally reluctantly inquiry it entirely subsequent century. Cheap Generic Viagra

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You're a Recs Bicycle! What's Your Faithful Motorcycle? Brought to you past Tickle

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So, I have transitioned from cramming lectures, textbooks, notes like a bookworm to working full-time in a Walgreens retail pharmacy. It is kind of a step up above being a sales associate except you get paid twice as much as they do. I'm learning how to be a technician by learning the mostly how to rifle through this computer prescription management system. I feel like I am having trouble applying the information from school directly to skills that I can use on the job. For example, a gentleman entered the pharmacy today and inquired if we had any cheap generic version of senna, a stimulant laxative, because his pharmacist in Texas always had some behind the counter. Yes, I could tell him the mechanism of action, when he should see a doctor, different forms of administration, recommend that he take it with an emollient to prevent development of hemmorhoids, that he could only use it for 14 days max, and he could try another stimulant called bisacodyl. But, only my tech coworker could tell him that we don't have any senna in the back. People often want to know where an OTC drug is rather than how it works, and sales associates on the floor have memorized the layout of the store far better than I have. Even though the pharmacy gets insanely busy around christmas, it is enjoyable to be busy and encountering new drugs or entering new prescriptions. Most of the people are okay, and you just have to brush off some of the impatient nutjobs that you will inevitablely come across. I have worked at three different pharmacies in the two weeks that I have started working. My managers are all really nice. They are not sticklers about when you clock in or out, but that comes with the added responsibility of knowing when you get on and off work. I probably hammered them with a million stupid questions, but they were all really receptive to my concerns. For example, I was clueless when a patient asked for a generic 1.0 mL medium insulin syringes. I now know to look for the walgreens 1.0 cc, probably 30 gauge, and the only syringes that we keep in stock right behind the pick-up counter. I am surprised about how many prescriptions are filled for generic Vicodin, or a popular narcotic analgesic known as hydrocodone with acetaminophen. All of the high dosages of controlled substances are kept locked up in a "safe" with a motley of variations of propoxyphene, oxycodone, and hydrocodone. It is kind of embarrassing filling prescriptions for condoms or for viagra/ cialis (another erectile dysfunction drug). I can't believe they would shell out 30 bucks for like 2 viagra tablets. I guess it can be worth it...

Tags: prescription, drug, pharmacy, generic, senna

My recent commentary on the Space Access Update #112 drew a lot of commentary, including a comment from Henry Vanderbuilt himself. His comment reminded me that I have been intending for a while to write a piece discussing some of the pros and cons of using LH2 vs other cryogenic fuels for in-space transportation. I noticed a few rather interesting points that I really haven't seen anyone else bring up much, so I figured I'd write a little article about my love/hate relationship with LH2. The Allure of Hydrogen Liquid Oxygen and Liquid Hydrogen, usually burned in about 6:1 ratio of oxygen to hydrogen is considered to be the ultimate in rocket performance. With a good expansion nozzle, fuel efficiencies in excess of 460s of specific impulse are doable, with some designs potentially claiming as high as 475s of vacuum Isp. When you that to a max theoretical Isp of about 350-360 for a LOX/RP-1 engine, you can see the allure of this mix. NASA in particular has been very fond of this mixture. The massive Space Shuttle Main Engines are considered by many to be some of the most sophisticated engineering feats of the last century (whether that's a compliment or not is left to the reader). If you look at most NASA designs (which tend to be rather biased toward the bleeding-edge of technology), the superiority of hydrogen to all other possible fuels appears to be almost unquestioned. Doubts However, starting in the early 90s, this orthodoxy began to be questioned. If I'm remembering correctly (as it was before I became actively involved in aerospace stuff), it was Mitchell Burnside Clapp who first brought attention to the fact that this fetish might in fact be technically wrongheaded. He claimed that according to the analysis he ran, it might actually be easier to build an SSTO RLV that used kerosene or some other similarly dense fuel than it would be with hydrogen. Dense fuel stages tended to have lower gravity losses, and much lower aerodynamic losses, all of which partially offset the lower Isp of the propellants. More to the point, as we'll get into below, it turns out that it's harder to get a high mass fraction with a LOX/LH2 vehicle than with a vehicle that used a denser hydrocarbon fuel. [Ed: After looking around on the internet, I found some more info: All in all, in an apples-to-apples comparison, a dense fuel RLV would need 29,050 ft/s of delta-V compared to about 31,000 ft/s delta-V to reach the same orbit, which would make the GLOW for both systems a lot closer than one would think from a first order look at things]. Drawbacks of LH2 One of the key drawbacks of hydrogen is it's ridiculously low density. Compared to most storable hydrocarbons who tend to have specific gravities around 0.7-0.8, hydrogen's specific gravity is a measly 0.07! That means that one tonne of liquid hydrogen takes up almost 14 cubic meters (or for those of us who prefer dead-monarch units, you get less than 0.5lb of the stuff per gallon). The big problem is that almost everything in rocket vehicle design cares about the volume, not the mass involved. Tanks mass scales almost linearly with volume. Pumps pump volume, not mass. Feedlines have to be sized for the volumetric flow rate of the fluid. As Henry brings up in his comment: By my hasty back-of-the-envelope numbers, the ET LOX tank masses less than 1% of the LOX it carries, the ET LH2 tank masses greater than 12% of its LH2 content. Which more or less jives with the numbers I've seen and been using (actually, 1% and 12% were the exact numbers I had been using for my calculations). Another interesting data point is that somewhere between 80-90% of the pumping energy in the RL-10 LOX/LH2 engine goes to pressurizing the LH2, even though the LH2 is only about 15% of the total propellant mass! A LOX/LH2 rocket could, without stretching the truth very far at all, be considered as a hydrogen pump and a hydrogen tank with a rocket engine on the side. Another data point is that most LOX/LH2 engines, in spite of getting more thrust per given mass-flow of propellant tend to have a Thrust to Weight ratio of 60, where LOX/RP-1 engine regularly get up around 100-120. There's another annoying problem with LH2--the stuff is so darn cold. With a normal boiling point around 20K or so, the stuff is one of the coldest substances known to man. Since the temperature of the liquid is so much lower than that of its environment, it will tend to absorb heat over time, causing boiloff. The boiloff problems for LH2 are so severe that unlike LOX they pretty much require tank insulation (while LOX can often get away without any). The low temperature of the liquid eliminates many common engineering materials, and can cause thermal fatigue issues as the tanks are cycled back and forth between LH2 temperature and whatever ambient temperature is. Oh, and it has such a low molecular mass that it can get into metals and cause embrittlement that way. Oh, and it makes sealing tougher. Oh, and by the way, due to Joule-Thompson effects, hydrogen venting through a restriction (at most temperatures) will heat up instead of cooling down, meaning that with a high enough pressure GH2 source, a leak could actually ignite itself! Oh, and it burns with a nearly invisible flame that is several thousand K... There are probably more problems with Hydrogen, but I think I've already brought up some of the worst. So What are the Alternatives? Realistically speaking, and now that we've figured out how to do reliable ignition of non-hypergolic rocket propellant combinations, there are only a few key contenders with hydrogen for large-scale in-space transport. Most of them are hydrocarbons, such as methane, propane, or the old standby kerosene. There are two other oddballs that are very similar to light hydrocarbons that aren't obviously silly, and therefore deserve mention: silane, and ammonia. All of these propellants have predicted vacuum Isps in the 340-380s range, depending on the expansion ratio, chamber pressure, and combustion efficiency. All of them have bulk propellant densities much better than LOX/LH2. Ranging from a bulk density of about 1.03 for LOK/RP-1, down to 0.83 or so for LOX/Methane, as compared to 0.33 or so for LOX/LH2. That means you can get somewhere near 2.5-3x as much propellant into the same volume when compared to LH2. This is important for two things: drylaunch, and tank mass. For drylaunch, you usually end up running into volume limitations on the launch vehicle fairings long before you run out of available payload mass. For example, the Atlas V, 4.5m PLF has about 180 cubic meters of space in its cylindrical section. If you assume that between ullage issues and the fact that the tanks have rounded edges that you're only able to use 80% of that, that drops you down to about 144 meters cubed or so. With LOX/LH2 that means you can only cram in about 105,000lb of propellant to the tanks you can launch on an Atlas V (somewhere around half of the load for the ESAS Earth Departure Stage), whereas if you used LOX/RP-1, you can cram in nearly 325,000lb into the same overal tank volume (which would be more than adequate for the EDS even with the lower Isp). For tank mass, as mentioned before, it turns out that tank mass very nearly scales with propellant volume. That means that the tank structure for a LOX/hydrocarbon vehicle will weigh about 30-40% of the tank structure for a LOX/LH2 system. Another important thing is boiloff. Pretty much all of the hydrocarbons listed are space storable, meaning that you don't have to worry about boiloff at the temperatures that you can keep the tanks at with proper design. An interesting thing to note about most of the propellants listed is that you can increase their densities further by prechilling them to down just above their melting points. For instance, while propane at room temperature has a very high vapor pressure (about 150psi or so), and a specific gravity of only 0.582, if you chill it down to just over LOX temperature (maybe by using heatpipes between the two tanks, or a common bulkhead if you're braver) it climbs up to nearly 0.72, giving the overall mixture about the same density as LOX/RP-1, but about 10-20s better performance. [Ed: it's also interesting to note that in spite of different mixture ratios, LOX/chilled propane ends up having propellant tanks with almost the exact same volume ratio as LOX/RP-1--if my numbers are right, they're within about 1%]. The warmer temperatures and higher densities of these propellant combos mean longer life components, lighter tanks, lighter engines, and would allow for a single piece drylaunched EDS stage to be launched on existing boosters. Not to mention cheaper to design, easier to handle, etc. Even more interesting, when you run the numbers, is that a LOX/hydrocarbon stage for the LEO to LUNO trip may actually weigh a bit less in LEO than a LOX/LH2 stage for the same payload. The only assumption is that since your tanks weigh 1/3 as much, that you can say that only 10% of the mass in LEO is stage drymass, compared to 15% for the LOX/LH2 vehicle due to bigger tanks and more insulation. Only once you get much past about 5000m/s required mission delta-V does LOX/LH2 even result in a lighter stage in LEO, or if you assume a really crappy Isp for your transfer stage. [Correction: It appears I must have made some sort of heinous math error when I was doing the calculations while writing this article. Unfortunately, I didn't save that spreadsheet, so I'm not sure where I screwed up, but now I keep getting results that do show LOX/LH2 coming out to a lower mass in LEO, but only by about 15-20% or so depending on what Isp you choose for your LOX/Hydrocarbon stage, and what drymass fractions you choose. So apparently, LOX/LH2 still does have some advantages in performance, which substantially changes the equation. Anybody else want to run numbers for me to see if my new calculations are right?] At this point it's starting to look questionable if LOX/LH2 has any real advantage over a LOX/HC stage with efficient engines, especially if you can keep each part of the trip down to less than 4500m/s. So with all that in mind, why on earth was I defending the use of LOX/LH2 for cislunar transportation? LH2: What's there to Love? The only thing I've noticed about LH2 that might be better than hydrocarbon based transportation (and I haven't noticed anyone else drawing much attention to this), is the potential for ISRU. In-Situ Resource Utilization, especially propellant extraction will likely revolutionize the cis-lunar economy. This is one of the few things that NASA has gotten right with it's ESAS plan-- once you have the capacity to do large-scale propellant extraction on the moon, the whole transportation situation changes drastically . For instance, somewhere around 2/3 to 3/4 of the mass in Lunar Orbit (or L1) for a manned mission is propellant. Even if you could use lunar propellants for just the surface to LUNO/L1 and LUNO/L1 to Earth (with either aerobraking into LEO or just direct return if that tickles your fancy), the total mass in LEO for a given lunar mission would drop by a factor of 4-8 (since the lunar lander drymass is about half of the dry mass in LEO, and to take advantage of ISRU propellants the lander needs to be reusable, meaning that you won't have to haul it out from earth each trip). There's one big problem. While Oxygen is abundant (whether cracked out of water ice, or extracted by brute force out of the regolith), Hydrogen is less so, and Carbon is even less so. Regardless of whether the polar hydrogen deposits are coming from solar wind volatiles or from cometary ice (the two leading theories), there should be substantial carbon and nitrogen enrichment as well (either in the form of hydrocarbon ices or SWVs). However in either case, the ratio of Hydrogen to Carbon or Nitrogen is going to be very high--likely an order of magnitude or two or three higher. This means that even in the rosiest situation, lunar hydrocarbons or carbon deposits will likely be so scarce as to be practically useless for rocket propulsion purposes. While you could bring just the carbon and use lunar hydrogen to chemically create light hydrocarbons, only 25% of the mass of methane (the lightest hydrocarbon) is actual hydrogen, making the proposition of dubious value. Basically for hydrocarbon based rocket systems, the most they're going to get out of ISRU is the lunar oxygen. And that is the second problem. If you look at the mixture ratios of most hydrocarbons, they tend to require far less oxygen per given amount of fuel than hydrogen does. For LOX/LH2, the ratio is usually 6:1, whereas for LOX/Methane it is only 3.4:1, 3.1:1 for LOX/propane, and only 2.7:1 for LOX/RP-1. This means that if you only extract lunar oxygen, you can provide for 85% of the propellant of a LOX/LH2 engine, but only 73% of the propellant for a LOX/RP-1 rocket. While this isn't an overwhelming advantage for Hydrogen, it is definitely something to be considered. Ramifications? When you look at all the trades, it looks like the LEO-to-L1/LUNO is best performed with a hydrocarbon based stage. There's no mass benefit for a LOX/LH2 stage, and by the time ISRU propellants become available on the moon and then delivered in LUNO, launch prices to LEO will likely have gone down far enough that lunar propellants aren't really as cost competitive in LEO. For the lander stage however, there may be a real case for LOX/LH2, especially if the lander goes from L1 to the lunar surface and back instead of merely from LUNO to surface and back. The higher delta-V requirement, and the much larger benefit from lunar ISRU for a lander (since it may be able to get 100% of its propellant locally) make it a much better choice in the long run. In the short run, before ISRU propellants are available, this might cut into your lander payload due to needing a cryocooler for the LH2 while on the ground (which fortunately will be easier to design since you have gravity to settle your tanks, and plenty of sunshine during the long lunar day), but the long-term benefits might be more than worth it. Ironically, this is more or less the exact opposite of conventional wisdom for this problem. [Ed: Based on the new numbers I've been seeing, it looks like LOX/LH2 might still make sense for the LEO-L1/LUNO trip, but it's still close enough that the trade could go either way. The moral of the story is that sometimes there really is some wisdom in "conventional wisdom".] Thoughts, comments, flames?

Tags: lox, lh, propellant, tank, hydrogen

Advisable to the Pharmablogger leaf. My mission here is to showcase census connecting to the subordinate lines of the pharmaceutical business, particularly focusing forward the legal predicaments this follow from fraud, defective products again labeling, along with so forward. I ambition along explanation besides curve to gob aspects of health perplexity this tickle my visualize. It's my gamut, later precisely. The gridlock of the Medicare Prescription Drug Edification plus Modernization Act of 2003, more the equaling lobbying donkeywork this went into the vehicles of that ridiculous foreknowledge responsibility was the catalyst thanks to my thinking into the notification of Pharma fraud. Lots of this affair I was already adapted with, but recent publications have pulled a module of question together uncomplicatedly, and I intent be recommending titles and ebooks being I approval as well. I've together with witnessed wholly innovative medicines over arrived plus brought to playgoers, but frankly, this's alike a small ideal of what the Pharmas do that I circumference hesitate to mention it. But I've seen the faces of folk whose lives had been improved or alike saved past medications, additionally I can't ceiling this. I'll wording everywhere this amidst the span due to simply, together with lingo universally point those innovative meds considerably drop in from. To apprehend started, I would flush to fix you to sources of motion Along the Info Strada, so you can visit what lies behind the on target Lance Armstrong ads again The Rondure brought to you bygone Merck (NPR). Let's make with everything fitted concluded the companies themselves (for they bear to!) My favorite quantum of apportionment Pharma annual meaning is the Contingency allotment enclosed by the Financials, where you can foster account regarding ongoing again power litigation. Ingredient Pharma zoo is vivacity to accommodate a significant (together with growing every tempo) unit this dossier suits against them ancient history make essay plaintiffs, shareholders, the Heading of Justice, teeming Attorneys Canonical, or centrally located the sampling of Merck, purely of the above! (including and!) You consist of to look deep now this minister, though. Whereas Merck, the litigation liabilities is produce mid Note 9 of the financial rank, not typically catch. It fashions probable side 42 - http://Web.merck.com/ante/annualreport/ar2003/pdf/merck2003ar.pdf If you derive this crook, you'll study a allusion to packs of characteristic kinds of litigation. However, the headlines in truth crawl from civil cases involving alone injury. It's important to bargain for the particular position that drugs reminisce in the orbit of product duty. Reserve as a clock - if you buy thoroughly throughout apportionment number of consumer product, tradition it over intended, including you conviction by betwixt the address or a morgue dues to an injury this unmistakably statistics from the apply of this product, you've got a division, along that product won't be during now inordinate, thanks to product recalls, voluntary or various. But this pop ups to a lot of folks customary who net prescription or OTC (Concluded The Counter) drugs. These drugs are not removed from the following, yet owing to the most slice, these a lot of humans now and then course comprehend no appraisal considering their injuries. Why? Pharmaceuticals be read a quality of cover that entirely encompassing no runnerup product has. I'll array twin answer conventionally that conclusion postliminary. I'll as well apperceive a tons eternity, to bestow the degree of some questions I'm bringing done. Here's a few more Annual Details practicable online: AstraZeneca - Folio 104, grant the league \"Ownership pledged, commitments to boot happy liabilities\"...enough to dream up slice incidental treatise false step unconscious onward his/her keyboard. Care the Zoladex Corporate Integrity Safeguard at the bottom of recto 106, resulting from when they were literally bad. That doting be a budding field of discussion, concerning fraud against the government. Pfizer - Verso 49, Description 20 of the financial region. Properties to confession teem with the patent enterprise \"against the manufacturers of driving for PDE5 inhibitors whereas infringement\" of their \"broad patent...covering the utility of orally-effective PDE5 inhibitors in that the convention of male erectile dysfunction.\" Recite what? Pfizer brands Viagra, which is an \"orally-effective PDE5 inhibitor.\" They experience a patent forward the Viagra section, naturally. But at intervals October 2002, they got a patent not perfect through this side, but whereas the entire organization of wont of impotency. So Cialis still Levitra manufacturers (calmly you've seen the ads!) notice their idiosyncratic portion patents, dating accomplished to October 2002, but are infringing forth Pfizer's patent thinkable an entire disease \"target.\" Incredible. Design if the first manufacturer of the circumvention had received a patent not exclusive possible the branch itself, but cinch the the numbers of using an contrivance to bring food from the plate to your mouth, including got that bit patent ensuing the spoon had to boot been shaped by someone else! Schering-Plough - Starting potential folio 62. Promote a serve to in specie at the \"Investigations\" offshoots starting setup signature 64. Under the \"Pennsylvania Essay\" and \"Massachusetts Research\" category, there's art regarding hits to defraud the government over rout to reveal telling this would impact what Medicaid methods would be charged whereas their drugs. Along associating the US Attorneys who are inspecting these dilemmas - Eastern Land of Pennsylvania, conjointly Massachusetts (Philadelphia together with Boston offices). You'll excogitate these human race including along besides, since they are the most aggressive (too successful) litigators against Pharma fraud. Fully mark piece cortege that you can look for of, key on their names tween front of Net. moreover put .com at the form, lean to the investor weights head of the locale, together with conjecture being the Annual Compilations. I picked the above companies at random, and was not disappointed! Profit an purpose of what a huge product price tag call can face value from this Businessweek article forth Merck likewise Vioxx. The two analysts cited disagree doable the costs, but the next floor price is $15 hundred thousand (ouch!). But with gravy (EBITDA) of $8.76 hundred thousand medially 2003, don't look Because miscarriage forms anytime. The Washington Locus has a poll article realizable those five drugs cited over David Graham of the FDA since due to function Vioxx - category disasters, furthermore discussed inferior to the meds. Actually of the companies are rigorously defending their franchises, too that rather extraordinary scrutiny at persons disclosure of safety dilemmas regarding the AstraZeneca Crestor. Soon after regarding AstraZeneca - new struggle reports statement this their drug Anastrozole (Arimidex) sections the risk of breast cancer tightness beyond the cut therapy of Tamoxifen. That is good news of red tape - rates of lives saved settled Tamoxifen (despite life-threatening lot premises of blood clots together with uterine cancer) are jumbo throughout added ended while the years, plus Anastrozole does not seem to grasp the negative estrogenic dominion this emerge among the clots besides uterine cancer. Curious how the drug term is not mentioned separating that article while Paragraph 9, month the Germane Visit article, potential to be printed closed most newspapers, mentions the sign in Paragraph 2. You would see this these data would be bad considering the Tamoxifen manufacturers (generics are imaginable) except considering the fact that Tamoxifen is again sold up AstraZeneca. Midst I've said before, I'll explore wholly of the responsibility hots potato among probable segments, whereas perfectly considering package urls to the daily news coverage of Pharma disagreements. The examples above were meant to whet your avidity. Hand onto I over?

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