Browse Topic: Water treatment

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A method was developed that allows water recycling, air treatment, thermal control, and solid residuals treatment and recycle to be removed from the usable habitat volume and placed in the walls of a radiation-shielding water wall. This design also provides a mechanism to recover and reuse water treatment (solid) residuals to strengthen the habitat shell.
Manufacturers in the process industries need to adjust to smaller batches and different types of product in the same plant. Plants based on the “Lego principle” are designed and engineered precisely to the respective task, whether for the production of a specific product in units per time unit, or for the throughput of a specific substance in a quantity per time unit. The mechanical design of the plant as a whole is geared towards meeting specifications and guaranteeing the required performance data over the projected lifecycle of the plant. The corresponding automation is carried out using management systems comprising process-specific (control) components, operating and monitoring stations, as well as engineering stations. The entire process is centrally controlled by a single management system.
Improvements in brine water recovery are critical to advancing NASA’s goals for human exploration of space. Water recovery systems must minimize the need for new supplies of clean water by closing the water loop. To accomplish this, water losses must be minimized or eliminated. A major loss of water is the brine produced by the primary water processor. For current technologies, this loss can be up to 15%.
Development and Design of a Low Temperature Solid Waste Oxidation and Water Recovery System2008-01-20526/29/2008
In February 2004 NASA released “The Vision for Space Exploration.” The goals outlined in this document include extending the human presence in the solar system, culminating in the exploration of Mars. A key requirement for this effort is to identify a safe and effective method to process waste. Methods currently under consideration include incineration, microbial oxidation, pyrolysis, drying, and compaction. Although each has advantages, no single method has yet been developed that is safe, recovers valuable resources including oxygen and water, and has low energy and space requirements. Thus, the objective of this work is to develop a low temperature oxidation process to convert waste cleanly and rapidly to carbon dioxide and water. Previously, TDA Research, Inc. demonstrated the potential of a low temperature dry oxidation process using ozone in a small laboratory reactor. Currently, TDA and NASA Ames Research Center are developing a pilot scale low temperature ozone oxidation system to convert organic waste to CO2 and H2O. The system also disinfects the waste and remaining water, and recovers not only the water content of the waste but also generates additional water that can be utilized by the crew. Tests are being conducted with model wastes in a reactor design that maximizes the contact between the reactants by mixing the waste with water, which also makes the oxidation process extremely selective to CO2 and H2O and mitigates the rapid combustion events that were seen in the dry oxidation reactor. An ozone recycle loop was recently added to the system, which significantly increased the waste oxidation rates. The reactor operating conditions were then optimized using the design of experiments technique to maximize the waste oxidation rate. Currently, a pilot scale, fully automated system is being designed that will be capable of handling many different types of waste. The waste oxidation rates achieved to date, along with current waste generation rate models, indicate that all of the waste from a single crew member in one day can be processed in a vessel ranging in size from 8.2 liters (2.2 gallons) for a short term mission to 9.9 liters (2.6 gallons) for a long term mission. In addition, if the system were used solely as a fecal matter oxidizer the reactor size would be only 0.7 liters. At the conclusion of the project the system will be delivered to NASA Ames for evaluation.
Nabity, James A.Andersen, Erik W.Engel, Jeffrey R.Wickham, David T.Fisher, John W.
International Space Station USOS Potable Development Water Dispenser2008-01-20106/29/2008
The International Space Station (ISS) Russian Segment currently provides potable water dispensing capability for crewmember food and beverage rehydration. All ISS crewmembers rehydrate Russian and U.S. style food packages from this location. A new United States On-orbit Segment (USOS) Potable Water Dispenser (PWD) is under development. This unit will provide additional potable water dispensing capability to support an on-orbit crew of six. The PWD is designed to provide incremental quantities of hot and ambient temperature potable water to U.S. style food packages. It will receive iodinated water from the Fuel Cell Water Bus in the U.S. Laboratory element. The unit will provide potable-quality water, including active removal of biocidal iodine prior to dispensing. A heater assembly contained within the unit will be able to supply up to 2.0 liters of hot water (65 to 93°C) every thirty minutes. This quantity will allow three to four crewmembers to rehydrate their food and beverages from this location during a single meal. The unit is designed to remain functional for up to ten years with replacement of limited life items such as filters. It will be the size of two stacked Shuttle Middeck lockers (approximately the size of two small suitcases) and integrated into a science payload rack in the U.S. Laboratory element. Providing potable-quality water at the proper temperature for food and beverage reconstitution is critical to maintaining crew health and well-being. The numerous engineering challenges as well as human factors and safety considerations during the concept, design, and prototyping are outlined in this paper.
Shaw, Laura A.Barreda, Jose L.
Solid Phase Extraction Mechanistic Studies of the Ag(I)-DMABR Complex: Improving Efficiency of the C-SPE Standard Method of Analysis2008-01-22006/29/2008
Aqueous silver(I) is added at trace levels (0.1 – 1.0 mg/L) to spacecraft potable water as a biocide. Development of a method that can be deployed on orbit and in future Lunar and Mars missions is therefore central to maintenance of safe drinking water and crew health. To address this need, our laboratory has created an analytical technique that couples a selective sorption process based on solid phase extraction (SPE) with the quantitative measurement of the extract by a hand-held diffuse reflection spectrophotometer. This technique, referred to as colorimetric-solid phase extraction (C-SPE), enables the low level detection (limit of detection ∼5 ppb) of silver(I) by metering 1.0 mL of a water sample through a reagent-impregnated (i.e., 5-(p-dimethyl-aminobenzylidene)rhodanine, DMABR) SPE membrane. The total workup time for the analysis is only 60-90 s. Moreover, the effectiveness of this method has been demonstrated by microgravity simulations through comparisons to concurrent ground-based analyses of companion samples. In keeping with the mission of our research, we are constantly refining the efficiency and effectiveness of our methodology. One pressing problem when using C-SPE in a microgravity environment is the presence of dispersed air bubbles that can lead to errors in exact measurement of sampling volumes. Our current protocol requires the withdrawal of more than the specified volume of analyte into a syringe and swinging the syringe in an arc to force the entrapped air to the tip. The air and excess sample are expelled into a waste container before ejecting the analyte through the extraction cartridge. The ideal situation would involve filling a syringe without concern for the exact sample volume, and this can be accomplished by applying the principles of negligible depletion (ND) in conjunction with C-SPE measurements. To determine if current C-SPE protocols could be manipulated to our advantage, a series of experiments were performed to gain a fuller understanding of the role of DMABR in complexing silver(I). Currently used SPE membranes were found to be highly efficient for retaining DMABR, suggesting that reagent loadings may be reduced without compromising extraction performance, posing the potential to adjust the amount of reagent in a membrane to manipulate ND volumes.
Siperko, Lorraine M.Porter, Marc D.Lipert, Robert J.
Lightweight Contingency Water Recovery System Concept Development2008-01-21436/29/2008
The Lightweight Contingency Water Recovery System (LWC-WRS) harvests water from various sources in or around the Orion spacecraft in order to provide contingency water at a substantial mass savings when compared to stored emergency water supplies. The system uses activated carbon treatment (for urine) followed by forward osmosis (FO). The LWC-WRS recovers water from a variety of contaminated sources by directly processing it into a fortified (electrolyte and caloric) drink. Primary target water sources are urine, seawater, and other on board vehicle waters (often referred to as technical waters). The product drink provides hydration, electrolytes, and caloric requirements for crew consumption. The system hardware consists of a urine collection device containing an activated carbon matrix (Stage 1) and an FO membrane treatment element (or bag) which contains an internally mounted cellulose triacetate membrane (Stage 2). All components are light weight disposable plastic, the system is potentially wearable, and it uses no electrical power. When treating urine and other wastewaters containing high levels of organic contaminates this two stage treatment process is required. Seawater and wastewaters containing low levels of organics can be treated for removal of inorganic contaminants (like the salt in seawater) and microorganisms using only the second stage FO membrane element. First year performance testing indicated acceptable flux rates and water recovery percentages over 6 to 12 hours of optimal urine treatment, when using the full system. Some challenges remained in achieving and evaluating acceptable contaminates flux/rejection rates for TOC and nitrogen species in the product; see ICES paper 2007-01-3037 (Gormly and Flynn, 2007). Year 2 work has focused on four basic areas: Characterizing performance of the Stage 2 FO membrane treatment to harvest seawater for use in post landing survival at sea. Researching alternative food product and components for use as the osmotic agent (OA). Pursuing better TOC confirmation in terms of total expected flux/rejection and characterization. In particular, research to confirm (TOC) flux measured in NaCl/ultra-pure water brine product solutions using high chloride compatible analysis methods. Increased nitrogen species control and characterization in the process and product, particularly investigating product side options for urea and/or ammonia nitrogen control. Of these tasks the first is complete, the second and third are in work with substantial data currently available and reported, and the last is in the initial stages of concept development and data collection. Concluding comments and discussion will include a synopsis of seawater, urine and technical water recovery concept development as well as some future options for developing this technology. Initially, the system's urine recycle function is intended for contingency/emergency use only, but will do so at a significant mass savings when compared to contingency water supplies and/or conventional water treatments. LWC-WRS Stage 2 can be exploited to provide emergency utilization of seawater and technical waters. Ultimately, further development of the technology may also provide options for better integration of water recycling into larger habitat component design by including FO membrane elements within the structures.
Gormly, SherwinRichardson, Tra-My JustineFlynn, MichaelKliss, Mark
Biological Degradation of Spent De-Icing Fluids in a Municipal Wastewater Treatment Plant – Experiences and Challenges2007-01-33499/24/2007
Oslo Airport Gardermoen (OSL) is situated over a ground water reservoir, and collection and handling of spent de-icing fluids is therefore of major importance. OSL have chosen to handle low- and medium strength spent fluids in cooperation with a nearby municipal wastewater treatment plant (WWTP). Medium strength fluid is used as a carbon source for nitrogen removal, and thus used as a resource. Low strength fluid is pre-treated in an aerobic biofilm reactor before it is routed to the plant inlet. Prior to the choice of solution for disposal of the fluids, investigations were performed in laboratory and pilot scale. The efficiency of the fluid as a carbon source for denitrification was studied in parallel with ethanol and methanol as well documented carbon sources. The achieved denitrification rates were comparable with those achieved with methanol, while the necessary addition of carbon source was slightly higher for spent de-icing fluid than for methanol. The treatment plant has been operating for almost 9 years, with operational results confirming the spent de-icing fluid to be appropriate as a carbon source. The possible toxicity and low degradability of some of the additives were particular concerns, and was studied for both aerobic and anaerobic biological processes. While the rather toxic fatty alcohol ethoxylate was easily biodegradable when sufficiently diluted, the additives benzotriazole and sodium petroleum sulphonate were hardly or not biodegradable. The latter two additives were therefore substituted. The laboratory scale results were confirmed in full scale prior to this substitution. The pre-treatment of the low strength spent deicing fluid in an aerobic biofilm reactor followed by coagulation and dissolved air flotation was tested in laboratory and pilot scale. The pre-treatment produces water suitable for discharge to the biological stage at the municipal WWTP. This technical solution is implemented, with operational results confirming that this integrated treatment of spent de-icing fluids in a WWTP is a good solution.
Hem, Lars J.Rusten, BjørnSkjefstad, Jostein
The ISS Water Processor Catalytic Reactor as a Post Processor for Advanced Water Reclamation Systems2007-01-30387/9/2007
Advanced water processors being developed for NASA's Exploration Initiative rely on phase change technologies and/or biological processes as the primary means of water reclamation. As a result of the phase change, volatile compounds will also be transported into the distillate product stream. The catalytic reactor assembly used in the International Space Station (ISS) water processor assembly, referred to as Volatile Removal Assembly (VRA), has demonstrated high efficiency oxidation of many of these volatile contaminants, such as low molecular weight alcohols and acetic acid, and is considered a viable post treatment system for all advanced water processors. To support this investigation, two ersatz solutions were defined to be used for further evaluation of the VRA. The first solution was developed as part of an internal research and development project at Hamilton Sundstrand (HS), and is based primarily on ISS experience related to the development of the VRA. The second ersatz solution was defined by NASA in support of a study contract to Hamilton Sundstrand to evaluate the VRA as a potential post processor for the Cascade Distillation system being developed by Honeywell. This second ersatz solution contains several low molecular weight alcohols, organic acids, and several inorganic species. A range of residence times, oxygen concentrations and operating temperatures have been studied with both ersatz solutions to provide additional performance capability of the VRA catalyst.
Nalette, TimSnowdon, DougPickering, KarenCallahan, Michael
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