Title: Wastes in Space
1Wastes in Space
- David P. Chynoweth
- Agricultural and Biological Engineering
- University of Florida
2Scope
- Categories of wastes
- Kinds of space missions
- Criteria for waste management
- Air revitalization
- Water reclamation
- Solid waste management
- Conclusions
3Overview of System Integration, Modeling, and
Analysis Documents
4ALS Subsystems and Interfaces
- Subsystems
- Air
- Biomass
- Food
- Thermal
- Waste
- Water
- Interfaces
- Crew
- Cooling
- Extravehicular Support
- Human Accommodations
- In-situ resource utilization
- Integrated control
- Power
- Radiation protection
5Current ALS Reference Missions
- Orbiting Research Facility, e.g. International
Space Station - Independent Exploration Mission
- mars transit vehicle
- surface habitat lander
- mars decent/ascent lander
- Extended Mission, e.g. Evolved Mars Base
6Function and Performance Criteria
- Waste Streams
- Functional Performance
- Mass Flow Schematic
- Gravity Dependance
- Technology Flexibility
- Operation and Maintenance
- Monitoring and Control
- System Integration
- Noise Level and Frequency
- Radiation Susceptibility
7Orbital in Near-Earth Space
- Gravity microgravity
- Air air revitalization (HEPA, mol. sieve,
activated carbon catalytic oxidizer) pressure
and humity control oxygen generation by
electrolysis of water hydrogen venting to space - Food packaged and fresh food dehydrated drinks
- Human Wastes solids collected in canisters and
returned to earth urine dewatered by vapor
compression distillation - Solid Wastes compacted, stored and returned to
earth - Liquid Wastes grey water collected and treated
to potable water quality (multi-filtration,
heating, catalytic oxidation, iodine
disinfection checked for microbial quality and
conductivity)
8Concentrated Mars Exploration Mission
- Duration 180 days transit descent 600 days
surface (or longer for evolved mission) ascent
180 day ascent - Vehicles two concurrent flights
- cargo flight lands on Mars with a Mars ascent
vehicle, in situ resource utilization plant, and
inflatable habitat - second flight is an earth return vehicle that
orbits Mars - Gravity hypogravity (37.5 earth gravity)
- Heat Rejection not a problem
- Radiation unknown
- Resources water and CO2
9Extended Mars Base
- Two aluminum shelled pressurized habitats of 90
m3 each - Voluminous inflatable structure providing for a
bioregenerative system for food production, water
recovery, and air revitalization - Transfer opportunity between Earth and Mars every
24 months - Facility lifetime of 15 years
- Power Generation 250 kWe (nuclear)
10Air Subsystem
- Total pressure in all systems 70.3 kPa
- Two systems
- Biomass production module has elevated CO2 (0.12
kPa), reduced O2 (17.3 kPa), 70 humidity, and
temp. to promote biomass growth - Crew quarters have more comfortable temperature
and humidity and normal CO2 and O2 concentrations - Atmospheric gas loss is expected to be 0.18 (by
mass) per day resupplied by pressurized or
cryogenic gases - A trace contaminant control subsystem controls
air quality using catalytic oxidation and
reusable filters
11Biomass Subsystem
- Higher plants will be grown hydroponic to provide
water regeneration (degrade organics),
atmospheric revitalization (use CO2 and produce
O2), and food - Crops
- High Carbohydrate (white and sweet potato, wheat,
rice) - Protein and Fat (peanut and soybean)
- Salad Crops (cabbage, carrot, chard, fresh herbs,
lettuce, onion, spinach, and tomato) - Artificial Light (wavelength/photoperiod
optimized)
12Thermal Subsystem
- Collects heat loads and rejects heat to
environment
13Water Subsystem
- Plant chamber is primary water processor combined
with support physicochemical systems to remove
solids and inorganic impurities and for final
polishing - Transpired water is pure and collected
- Advanced microbial control technology is employed
14Waste Subsystem
- Wastes inedible biomass, food-processing, urine
and feces, sweat solids, filters, paper - Dried before storage
- Treatment oxidation by incineration is current
baseline process other options under
consideration - Regenerative catalytic beds treat effluent gases
- Carbon dioxide and nutrients returned to plant
growth system - Excess carbon dioxide is vented
15Alternate Life Support Formats Under Consideration
- In-situ Resource Utilization
- rocket fuel from hydrogen and oxygen
- replacement of gases lost by leakage
- water (direct use or source of oxygen and
hydrogen) - minerals for plant growth
- Mars atmosphere has 95 CO2, 2.7 N2, and 0.02
H20 vapor - Bioregeneration
- capturing light for photosynthetic
- construction of large greenhouses using CO2,
H20,and nutrients derived from Mars environment - Solar Power
- requires large systems in outer space
- politically more acceptable than nuclear
16Contingencies From a Life Support Perspective
- accidents
- environmental hazards
- equipment failure
- excessive consumption
- inadequate performance of life support and
related systems - leakage
- human error
17Considerations for Alternative Space Missions
- Bases on Luna
- long nights
- availability of support commodities (hydrogen,
nitrogen, and carbon) - rejection of life support loads during the Lunar
day - wide environmental swings
- Near-earth space or asteroids
- weightlessness
- mission duration
- radiation protection
18Equivalent Systems Mass Criteria
- Mass
- Volume
- Power
- Cooling
- Crew Time
- Scaling Factors
- R D Costs
19Daily Solid Waste Stream for 6-person Crew
During a 600-day Exploratory Mission
(Adapted from Solid Waste Processing and Resource
Recovery Workshop Report. 2001)
Bioastronautics Workshop 2002, Galveston, TX
20Space Mission Waste Composition
( Dry Basis)
Bioastronautics Workshop 2002, Galveston, TX
21Wastewater Characteristics
22Air Contaminants
- Carbon dioxide
- Hydrogen (from electrolysis of water to obtain
oxygen) - Trace organics, e.g. methane, ethanol (used for
disinfection??) - Trace inorganics (ozone, hydrogen sulfide, carbon
monoxide, oxides of sulfur and nitrogen)
23Solid Waste Handling and Pre-Processing
- Collection/Separation (including phase, metals)
- Storage
- Drying freeze, thermal, vacuum, air
- Compaction/Pelletization
- Size reduction wet, dry
- Transport fluid, gas, vacuum, mechanical
conveyance - Mixing
24Physical-Chemical Technologies
- Lyophilization
- Supercritical wet oxidation
- Incineration
- Pyrolysis
- Wet carbonization
- Solubilization
- Transformation (activated carbon, paper)
25Biological Technologies
- Slurry bioreactors (aerobic and anaerobic)
- Aerobic composting
- Anaerobic composting
- Enzymatic digestion
- Transformation into useful products (methane,
ethanol, etc.)
26Advantages and Limitations of Physical/Chemical
and Biological Waste Management Options
27Space Toilet
28Space Toilets
29Post-Processing
- Treating useable product gases, liquids and
solids - Treating non-useable residues (toxic products,
ash, refractory organics)
30Proposed System Schematic
31ESM Comparison of Different Waste Technologies
(without crew time)
(Adapted from Maxwell et.al 2001)
32Schematic of HSLAD with other Subsystem
33Integration Potential Analysis
34Prototype Station Digester
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36Snowed In
37Intelligent Compactor
38Headin for the Hills
39Hope the Chutes Dont Tangle
40When is it Going to Rain?
41Now we can breath again
42Viking, the nonviolent type
43Viking Sucks
44Hello!
45Mars Pathfinder Actual View
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47Mars Surveyer
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52CLLS Module, 70s-80s
53Biosphere 2
54International Space Station
55BIOPLEX
56Space Station Earth
57Outline Of Problems (1)
- Atmosphere
- green house gases (climate change)
- acid rain
- ozone (uv light penetration)
58Outline Of Problems (2)
- Ecosphere
- habitat loss
- freshwater supply
- bioinvasion
- alteration of fire cycles
- persistent organic pollutants
- nitrogen pollution
- overfishing
59Outline Of Problems (3)
- Social Sphere
- population growth
- infectious disease
- economic exploitation
- natural resource exploitation
- human resource exploitation
60What is Global Warming?
61Diagram of Acid Rain
62Development of Ozone Hole