Browse Topic: Water reclamation

Items (223)
Inspired by a small and slow snail, scientists have developed a robot prototype that may one day scoop up microplastics from the surfaces of oceans, seas, and lakes.
Recent experiments by a team from the West Virginia University focused on how a weightless microgravity environment affects 3D printing using titania foam, a material with potential applications ranging from UV blocking to water purification. ACS Applied Materials and Interfaces published their findings.
Researchers have integrated water purification technology into a new proof-of-concept design for a sea water electrolyzer that uses an electric current to split apart the hydrogen and oxygen in water molecules. This new method for “sea water splitting” could make it easier to turn wind and solar energy into a storable and portable fuel.
The Pre-Treatment Solution for Water Recovery technology was developed by NASA Johnson Space Center innovators to increase the amount of potable water recovered from the International Space Station’s urine processor assembly system. The solution increased the water recovery rate in the ISS distiller from 75 to 90 percent, doubled the volume of feed processed per cycle, reduced the volume of brine by half, and eliminated the formation of precipitate up to 90% water recovery.
Scientists at NASA's Glenn Research Center have developed a unique water purification method that can be used for water recycling or point-of-use applications. Originally developed as a means to recycle water in space, this technology has applications in industrial water treatment, water recycling, and water purification for military bases, disaster sites, and regions without easy access to clean water. Relying on only electrical energy, this technology uses plasma-generated reactive species to decompose organic contaminants, ranging from submicron particles to water soluble organics like glycol, ethanol, and industrial dyes.
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.
A hot and cold water mixing process with a steam condenser and a chilled water heat exchanger is set up for an engine EGR fouling test. The test rig has water recycled in the loop of a pump, heat exchangers, a three-way mixing valve, and a test EGR unit. The target unit temperature is controlled by a heating, cooling and mixing process with individual valves regulating the flow-rate of saturated steam, chilled water and mixing ratio. The challenges in control design are the dead-time, interaction, nonlinearity and multivariable characteristics of heat exchangers, plus the flow recycle in the system. A systems method is applied to extract a simple linear model for control design. The method avoids the nonlinearity and interaction among different temperatures at inlet, outlet and flow-rate. The test data proves the effectiveness of systems analysis and modeling methodology. As a result, the first-order linear model facilitates the controller design. The simulation studies with internal recycle processes produced promising results. Test rig operating data indicate both the modeling method and Model Predictive Control (MPC) controller are effective.
Wu, Hai, Chen, Wen, Li, Meng-Feng, Wang, Xinlei
Going to the dentist is always a less-than-welcome experience. However, a water purification technology developed for NASA could lead to a more satisfying end result and cleaner teeth.
The paper summarizes the experience gained with the ISS water management system during the missions ISS-1 through ISS-17 (since November 2, 2000, through October 23, 2008). The water supply sources and structure, consumption and supply balance and balance specifics at various phases of space station operation are reviewed. The performance data of the system for water recovery from humidity condensate SRV-K and urine feed and pretreatment system SPK-U in the Russian orbital segment are presented. The key role of water recovery on board the ISS and the need to supplement the station's water supply hardware with a system for water reclamation from urine SRV-U is emphasized. The prospects of regenerative water supply system development are considered.
Bobe, L. S., Kochetkov, A. A., Soloukhin, V. A., Tomashpolskiy, M. Ju., Andreichuk, P. O., Protasov, N. N., Sinyak, Ju. E.
Water Recovery from Wastes in Space Habitats-a Comparative Evaluation of SBIR Prototypes2009-01-23427/12/2009
Water is of critical importance to space missions due to crew needs and the cost of supply. To control mission costs, it is essential to recycle water from all available wastes - both solids and liquids. Water recovery from liquid water wastes has already been accomplished on space missions. For instance, a Water Recycling System (WRS) is currently operational on the International Space Station (ISS). It recovers water from urine and humidity condensate and processes it to potable water specifications. However, there is more recoverable water in solid wastes such as uneaten food, wet trash, feces, paper and packaging material, and brine. Previous studies have established the feasibility of obtaining a considerable amount of water and oxygen from these wastes (Pisharody et al, 2002; Fisher et al, 2008; Wignarajah et al, 2008). This paper summarizes the results of laboratory studies that were conducted to recover water from solid wastes using hardware developed via Small Business Innovative Research (SBIR) grants. The SBIR hardware included a microwave powered freeze drying unit, a microwave powered ambient pressure dryer, and a recirculating hot air dryer. The results are presented and the advantages and disadvantages of each of these technologies are discussed in relation to the potential applications of these units for recovery of water from solid wastes on space missions.
Fisher, John W., Hogan, John A., Delzeit, Lance, Wignarajah, Kanapathipillai, Alba, Ric, Pace, Gregory, Fox, Thomas G
Starship Life Support2009-01-24667/12/2009
The design and mass cost of a starship and its life support system are investigated. The mission plan for a multigenerationai interstellar voyage to colonize a new planet is used to describe the starship design, including the crew habitat, accommodations, and life support. Cost is reduced if a small crew travels slowly and lands with minimal equipment. The first human interstellar colonization voyage will probably travel about 10 light years and last hundreds of years. The required travel velocity is achievable by nuclear propulsion using near future technology. To minimize mission mass, the entire starship would not decelerate at the destination. Only small descent vehicles would land on the destination planet. The most mass efficient colonization program would use colonizing crews of only a few dozen. Highly reliable life support can be achieved by providing selected spares and full replacement systems. Two alternate candidate life support approaches are oxygen and water recycling systems with stored dehydrated food or plants grown to provide food, oxygen, and water recycling. The mass costs of such systems using current technology are estimated and compared. Growing food for starship life support requires more mass than providing dehydrated food, even for multigeneration voyages of hundreds of years. The benefits of growing some food may justify the added mass cost. A system growing half the food is competitive with all dehydrated food. Plant growth technology has much more potential for mass reduction than dehydrated food, and currently projected improvements in plant growing technology could make it competitive. The lowest total mission mass is achieved a relatively low interstellar travel velocities. The life support mass saving on shorter voyages is less than the propulsion mass required to increase velocity. Life support is half the total spacecraft mass without propulsion, but propulsion is one and a half times more massive than the spacecraft, so life support is only twenty percent of the spacecraft plus propulsion mass. A single multigenerationai interstellar voyage to colonize a new planet would have cost similar to that of the Apollo program. We can go to the stars!
Jones, Harry
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, Sherwin, Richardson, Tra-My Justine, Flynn, Michael, Kliss, Mark
The New Italian Bioregenerative Life Support Program CAB2007-01-30907/9/2007
The Bioregenerative Life Support program CAB (Controllo Ambientale Biorigenerativo) is a key element of the Italian Space Agency (ASI) Medicine & Biotechnology scientific program, set forth in the ASI Activity Plan 2006-2008. The CAB program started in October 2006, under the prime partnership of Thales Alenia Space Italia, with a feasibility study of a controlled biological system, allowing the regeneration of resources and the production of food for life support in long duration missions. Main constituents of the CAB program are (a) higher plants as basic elements for food and oxygen production, CO2 regeneration and water purification via the photosynthetic and leaf transpiration processes, and (b) biological & physico-chemical systems for environmental control, monitoring, power & data distribution, etc. The sectors of technological and scientific concern are practically all the ones typical for life support systems in the frame of long duration human missions, i.e.: Food production, in particular via the cultivation of higher plants, and food management Air regeneration (Production of O2, Removal of CO2, Trace Gas Control) Water regeneration (Urine processing, Gray water processing, Potable water management) Solid waste processing Resources allocation and storage Control of environmental conditions (Thermal-hygrometric, light, pressure, radiation, etc).
Lobascio, C., Lamantea, M., Rampini (*), R., Cotronei, V., Negri, B., De Pascale, S., Maggio, A., Maffei, M., Palumberi, S.
Microfluidic Ion Chromatograph for In-Flight Water Quality Analysis2007-01-31537/9/2007
Although water quality may currently be analyzed on the ground after a flight, long-duration missions will require the capability to perform analyses on-board. If a water purifier fails, contaminants must be detected rapidly and corrective action taken in a timely manner to prevent serious harm to the crew. Many of the possible contaminants which could negatively affect astronaut health are inorganic ions. These ions can be quantified by ion chromatography (IC), although current commercially-available IC's are too large, heavy, and power-intensive to be used on a space mission. These units also require large quantities of caustic chemicals for analysis, which would pose a significant hazard in a microgravity environment. To meet the need for an inorganic water quality analysis device for long-duration missions, Lynntech developed an ion chromatograph tailored for future planned long-duration missions. The entire unit is the size of a shoebox, requires little power, produces anionic and cationic chromatograms simultaneously, and generates the acid and base needed for analysis from benign salt water. Several components were developed specifically for this application over the course of work. A developed microfluidic liquid/gas phase separator performed successfully in microgravity conditions; a syringe pump was developed to provide uniform and repeatable high-pressure flow from a low-power, compact device; and a conductivity detector was designed and implemented with six orders of magnitude in dynamic range, an internal volume of only 0.7 microliters, and an autoranging capability which allows the analysis of both high and low ionic species concentrations in the same sample. The complete system and its measurement capabilities are described in detail.
Ragucci, Tony, Maldonado, Francisco, Raducanu, Marius, Cisar, Alan
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, Tim, Snowdon, Doug, Pickering, Karen, Callahan, Michael
Regenerative Total Organic Carbon Analyzer for Long-Duration Missions2007-01-31547/9/2007
Potable and hygiene water availability is a critical requirement for long-duration manned space missions. Frequent water quality testing helps to ensure astronaut health by providing needed feedback on the effectiveness of on-board water purification units. One of the most basic and broad-spectrum indicators of contamination is organic carbon concentration. To meet the need for water quality feedback on the International Space Station (ISS), as well as on planned missions to Luna and Mars, Lynntech is developing a mesofluidic total organic carbon analyzer (TOCA) through the NASA SBIR program. The unit has been designed to operate in the demanding environment of a long-duration manned space mission and addresses the issues of microgravity operation, an operating lifetime of 5 years, low power consumption, simple user interface, robust architecture, and inherent safety. The TOCA design eliminates the need for launching and maintaining large quantities of hazardous chemicals while minimizing equivalent system mass (ESM). Considerable advancements have been made in TOCA development over the past year and are ongoing, including: zero-g flight testing of the liquid-gas phase separators developed for this application, redesign of critical components to increase efficiency and effectiveness, addition of new components to optimize microfluidic mixing and better-define sample volumes, reduction of sample cross-contamination potential, complete system assembly into a rack-mount enclosure, and accelerated life testing of the completed unit.
Ragucci, Tony, Kim, Jinseong, Maldonado, Francisco, Lewis, Brian, Gonzalez-Martin, Anuncia
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