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1 INTRODUCTION
2 MISSION DESIGN SUMMARY
3 GOALS AND OBJECTIVES
4 CHALLENGES, CONSTRAINTS, RATIONALE
5 SITE SELECTION
6 PLANT HABITAT
7 EXTERIOR ARCHITECTURE
8 INTERIOR ARCHITECTURE
9 BIOME HABITATION SYSTEMS
10 MISSION CONTROL AND COMMUNICATIONS
11 PUBLIC PARTICIPATION
12 MANNED MISSION ARRIVAL AND FUTURE USE
ABOUT THE PROJECT
BUILDING AN
ATMOSPHERE
RESPONSIVE
MOBILE
ENVIRONMENTS
INTERDISCIPLINARY TEAM(S)
SKIN/
PRESSURE
INTERIOR
STRUCTURE
MECH
SYSTEMS
STRUCTURE /
DEPLOYMENT
LIGHT HEAT INTERIOR
ADAPTATION
PLANT
GROWTH
TECH
SYSTEMS
EARTH
INTERFACE
COMMS &
CONTROL
BAA RME
CHEMICAL
ENGINEERING
CIVIL
ENGINEERING
MECHANICAL
ENGINEERING
+MORE
HCIBIOLOGYPHYSICS HUMANITIES
ARCHITECTURE TECHNOLOGYART DESIGN
OUTCOMES
SCALE
PROTOTYPE
A to-scale
prototype of the
exterior structure
and skin deployed
at CMU by end of
semester
INTERIOR
PROTOTYPE
A working analog
prototype using
available Earth
materials and
technologies to
support plant
growth
THEORETICAL
DESIGN
End-to-end
mission design
for a future
deployment of a
plant habitat on
Mars
PUBLIC
EXHIBITION
Open event that
engages the
campus in a
celebration of our
interdisciplinary
outcomes.
MISSION DESIGN SUMMARY
NASA projects a possible human presence on Mars as early as 2030s.
Before such an event can happen, we must develop systems capable of sustaining
life on the red planet, lightweight and small enough to make the journey and resilient
enough to survive without help from home.
Many agree that the first step towards proving we can create a sustainable habitat is
to design one first for plants. Recognizing that this habitat may not only be a place to
survive but thrive and be a beacon and remote connection to and for life on Earth,
students from across campus have come together to develop a concept for
an deployable autonomous habitat that can sustain life on Mars.
GOALS AND OBJECTIVES
MISSION STATEMENT
Exploring Viability for Future of Humans on Mars
● Project Viriditas seeks to plant an exploratory biome on the surface of
Mars. This habitat will act as a precursor to manned missions to the
Red planet
● The project’s main focus is to provide an inspirational monument to
human exploration of space. The design of the structure is intended to
engage the public with a uniquely shaped habitat
● The biome will also function as an experiment in organism viability and
will be consistently collecting data that can be applied in various fields
3. HUMAN
CONTACT AND
PSYCHOLOGICAL
CONNECTION
Plants within
habitat would
serve as a
biophilic agent for
any future
manned missions
2. VIABILITY OF
OXYGEN
PRODUCTION
Sixty plants for
two years will
produce enough
oxygen for a crew
of two humans for
two months
1. VIABILITY OF
FOOD
PRODUCTION
Acres of plants
will be needed to
completely
support human
life, but fresh food
may enhance diet
4. ENDURING
MONUMENT TO
HUMAN
EXPLORATION
Inspiration of
sustaining life on
another planet will
encourage
communal efforts
in space exploring
MISSION TIMELINE
2016:
Prototyping
begins
2080:
Plants have
produced enough
oxygen to sustain
crew
2030:
Mission is
sent with
roughly 60
plants
2032:
Habitat erected,
air is stored
and plants are
monitored
2038: Enough
air is stored
for two people
for 2 months
2040:
Humans arrive,
maintain hab
and add plants
Focus on Data Gathering
& Oxygen Production
Focus on Proof of
Concept
Focus on support
for human habitation
DESIRED IMPACT
Third Party Takeaway
● The process of keeping a closed-loop ecosystem functioning on
another planet will provide a useful testing ground for design and
creation of a human habitat
● The data gathered from the habitat will be informative to plant
lifecycle and adaptation research
● The technology used in the monitoring and control of the biome
will augment current extraterrestrial communication protocols
● The earth interaction component will provide inspiration to people
living on earth as they get to experience a martian environment
with familiar earth organisms.
CHALLENGES, CONSTRAINTS,
AND RATIONALE
Understanding the Problem
TRANSPORTATION
Deployable Architecture
4.1.1 Travel Duration
With current technology 6month travel time
4.1.2 Payload Size
Fits into the payload bay of the SpaceX Falcon Heavy or SLS
Rocket (15’ (4.6m) inner diameter)
Structure is meant to transport in the collapsed state
4.1.3 Materials and Seed Survival in Transit
Plants remain dormant in seed state during transit
MARTIAN ENVIRONMENT
Environmental Issues
Temperature Ranges Soil Water
Atmosphere Light Dust
Radiation
Precipitation
-133C to 27C
MONTH LONG DUST
STORMS
SEASONAL CO2
FROST
600PA (~0.6% EARTH)
PERCHLORATES
MEAN SOLAR
IRRADIANCE 588.6
W/m2 (40% EARTH
INTENSITY)
POLES
SUBSURFACE
LIQUID BRINE
Little Protection
from Solar
Radiation; avg. of
300 mSv
MARTIAN ENVIRONMENT
Design Constraints
Temperature Ranges Soil Water
Atmosphere Light Dust
Radiation
Precipitation
Use Martian light to grow
plants
Settle far from where
dust storms originate
and use vibration of the
drill to shake off dust.
Surfaces which are not
conducive to dust
collection
Create earth like
atmosphere inside
habitat for plants despite
the outside atmosphere
being 0.6% that of earth’s
Use partial sunlight to
light the plants in the
habitat; be wary of
radiation plants are
receiving
Collect water from
martian substrate using
drill
Not using Martian soil for
plant substrate
MISSION OPERATIONS
Communications Constraints
● One way transmission delay ranges from 13 min to 24 min
● 2 week period of time when Mars is out of view (i.e, no contact)
● Habitat must operate completely autonomously
● Data must be stored onboard for a brief amount of time
SITE SELECTION
Finding the Balance
(site map)
AVAILABILITY OF RESOURCES
Light Water
Month Hours of Sunlight
January 11.25
February 11.50
March 11.85
April 12.25
May 12.70
June 13.00
July 13.00
August 12.75
September 12.40
October 12.00
November 11.60
December 11.30
PLANT HABITAT
A Constructed Ecosystem
ECOSYSTEM PRECEDENTS
Our Question: Can we create a closed loop system based on
symbiotic biological interactions?
Biosphere 2 MELiSSA Project - ESA Living Machines: John Todd
Interacting Layers
Photosynthesizing, decomposing, and
algal layers are, grown simultaneously.
By designing symbiotic relationships, we
are replicating Earth ecosystems in Martian
terrains and beyond.
The layers provide supplemental nutrition
to future space crews, along with gas and
nutrient exchanges between layers.
Gas exchange
The decomposer layer produces
carbon dioxide when it breaks down
organic matter from the
photosynthesizing layer.
This provides necessary gases for
the photosynthesizing and algal
layers, which in turn produces
oxygen for the decomposer layer.
6.1.3 Algae
Spirulina
N2
, P, CO2
, and light consumer
O2
producer
Growth rate: 30% per day (cont.
light)
Air Temp: 25-38ºC
Water Temp: 25ºC
Rel. Humidity: 50-75%
pH Range: 9-10
Light: irradiance 60-100µE m-2
s
6.1.2. Decomposers
Oyster Mushrooms (Grey Dove &
Italian)
Air Temp: 18 -50ºC (ideal early
stage T range), 10-18ºC (ideal
fruiting T range)
Water Temp: 25ºC
Rel. Humidity: 80-90%
pH Range: 5-6.5
ORGANISM SELECTION + DIVERSITY
6.1.1 Photosynthesizers
Baby Bibb Lettuce
125 PPM of Nitrogen during all
growth stages
UA CEAC nutrient blend
Air Temp: 24/19ºC Day/Night
Water Temp: 25ºC
Rel. Humidity: 50-75%
pH Range: 5.5-6.5
D.O >3 ppm
Light: 17 mol/m2
per 24 hrs
GROWTH MECHANISMS
Soil Based
High weight payload
Inability to restore nutrients in
soil
Quantity of nutrients in
Martian soil might be hard to
ascertain
Aeroponics
Faster growth than soil
Less water usage than
hydroponics
Less weight payload than
hydroponics or soil-based
growing methods
Hydroponics
Uses a larger amount of
water
Smaller selection of plants
Energy expenditure and
system maintenance of
pumps
EXTERIOR ARCHITECTURE
Structure, Skin, and Deployment
FORMAL DEVELOPMENT
02 03
STRUCTURE LIFECYCLE + DEPLOYMENT
01
EXTERIOR SKINNING SYSTEM
MATERIAL FUNCTION KEY PROPERTIES PHYSICAL PROPERTIES
BETAGLASS FABRIC
GFRP / PTFE
Atomic Oxygen protective layer Protection from outer elements/ high durability/ fire
resistant
Thicker outer-layer of Betacloth
BETACLOTH
Silica Glass / Silicon
(Actually Silica fiber)
Multi-layer Insulation Layer (MLI) Protect against outer elements/ insulative properties/
fire resistant
(NASA REALLY hates fire)
Multi-layer fabric (astronaut space suits)
MYLAR
PET/PET
Actually (BoPET) / (stretched PET)
Multi-layer Insulation Layer (MLI) Radiation shielding/ thermal properties Shiny
DRACON
PET
Multi-layer Insulation Layer
(MLI)
Thermal blanket White Thermal Fabric
POLYURETHANE FOAM
Polyurethane
Micrometeoroid Orbital Debris (MMOD)
protection layer (in between nexetel layers)
Low density/ high absorption. Allows for easy folding
of outer shell.
Foam
NEXTEL
Alumina
MMOD protection layer High strength fabric, fire resistant Ceramic fabric
KEVLAR
Polyamide
Resistant layer/ inner layer Puncture resistant, helps keep physical structure of
inflatable
Woven fabric
COMBITHERM
Nylon/EVOH/Nylon/High Ethylene Vinyl
Acetate Polyethylene/LLDPE
(Complex Polymer film)
Bladder (redundant layering) Decreases habitat Permeability (0.1 cc/100 in2-24
hour-atm)
Clear plastic material [Combination of
polyethylene, nylon, and EVOH (vinyl alcohol)
layers]
NOMEX Inner layer Puncture resistant/ fire resistant Woven fabric (fire fighter suits)
SOLAR COLLECTION ARRAY
PARABOLIC REFLECTOR
Optical Cable
INTERIOR ARCHITECTURE
Plants, Support, and Systems
Overall Structure
Light Diffusion Layer
Plant Layer
Misters + Roots
Schroom Layer
Algae + Water Coil
Water Pump
INTERIOR LAYER PLANS
Plant Layer Mushroom LayerOverhead Light Diffusing Layer Algae Layer
BIOME HABITATION SYSTEMS
Mechanical and Technical Systems
MECHANICAL SYSTEMS
Power, Water, Heat, Air, Light
WATER
POWER
Via Wikipedia
HEAT
Systems diagram
PRESSURE/INFLATION
LIGHT DISTRIBUTION AND CONTROL
Calculations Natural v
Artificial?
We use growth LEDs
that output light in the
red and blue spectrum
which the plant is able
to use most efficiently
High Level Plant Layer
LED array and fiber optics above
Decomposer Layer
Four LED strips in a cross pattern as
the Oyster mushrooms require little
light
Algae Layer
LED strips along outside of clear
tubes containing algae in the algae
compartment
LIGHT DISTRIBUTION AND CONTROL
TECHNICAL SYSTEMS
Monitoring, Automation, Adaptation
PLANT PODS
Sensor List
• pH Level
• Soil Moisture
• Lux (light)
• Each pod in the plant layer will be
equipped with its own set of sensors
• Each section in the decomposer layer
will be equipped with a set of sensors
• These sensor will be used to monitor
the growth and health of each plant
PLANT MONITORING
Cameras
• Mounted on Gantries
• Controllable Autonomously
• Moves in 4 axes
• Attached to Central Column
BIOME MONITORING
Sensor List
● Camera
● Temperature
● Humidity
● Ambient Light
● Air pressure
● CO2
● O2
• Each layer of the biome will be equipped
with ambient sensors
• These sensors will be used to monitor the
health of the habitat and the ecosystem
• The habitat will make decisions based on
the values of these sensors
• Triple redundant sensors will be placed
(Adaptation systems will use the median
value to make decisions)
CONTROL AND
COMMUNICATIONS
Data Transmission, Use, and Interface
DATA AND TRANSMISSION
How do we get and store the data?
● Sensor data can be
gathered at any interval
- currently 5 minutes
● Queued on-site and
transmitted whenever
possible
● Aggregated and
presented in friendly
interface for perusal by
public
COMMUNICATIONS
Redundancy
DATA USES AND INTERFACES
Big Martian Data
PUBLIC ENGAGEMENT
Data Transmission, Use, and Interface
PRINCIPLES FOR PUBLIC ENGAGEMENT
From Earth to Mars and Back Again
Earth Mars
Astronauts
● Bring the experience of the Martian
biome to a global audience.
● Use digital media as a medium to
explore an otherwise isolated space.
● Educate viewers and explore data
through analogous systems.
PUBLIC ENGAGEMENT STRATEGY
Systems for Interplanetary Connection
VR Experience for
General Public
VR Tool for Astronauts
and Researchers
Monumental Installation
for Education
VIRTUAL REALITY SIMULATION
Digital Recreation of Martian Growth
VIRTUAL REALITY RESEARCH TOOLS
Data Exploration and Psychological Engagement
MONUMENTAL INSTALLATION
Education Through a Built Environment
FUTURE USE
Extending the Life of the Biome
Biomes create an artificial “forest” on the planet in anticipation of a human habitation.
The biome then becomes integrated with human habitats allowing humans to tend to them.
THANK YOU
Generously supported by:
NASA Pennsylvania Space Grant Consortium
The Frank-Ratchye Fund for Art @ the Frontier
Carnegie Mellon's ProSEED/Crosswalk Initiative
MarsHabitat

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MarsHabitat

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  • 2. 1 INTRODUCTION 2 MISSION DESIGN SUMMARY 3 GOALS AND OBJECTIVES 4 CHALLENGES, CONSTRAINTS, RATIONALE 5 SITE SELECTION 6 PLANT HABITAT 7 EXTERIOR ARCHITECTURE 8 INTERIOR ARCHITECTURE 9 BIOME HABITATION SYSTEMS 10 MISSION CONTROL AND COMMUNICATIONS 11 PUBLIC PARTICIPATION 12 MANNED MISSION ARRIVAL AND FUTURE USE
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  • 7. INTERDISCIPLINARY TEAM(S) SKIN/ PRESSURE INTERIOR STRUCTURE MECH SYSTEMS STRUCTURE / DEPLOYMENT LIGHT HEAT INTERIOR ADAPTATION PLANT GROWTH TECH SYSTEMS EARTH INTERFACE COMMS & CONTROL BAA RME CHEMICAL ENGINEERING CIVIL ENGINEERING MECHANICAL ENGINEERING +MORE HCIBIOLOGYPHYSICS HUMANITIES ARCHITECTURE TECHNOLOGYART DESIGN
  • 8. OUTCOMES SCALE PROTOTYPE A to-scale prototype of the exterior structure and skin deployed at CMU by end of semester INTERIOR PROTOTYPE A working analog prototype using available Earth materials and technologies to support plant growth THEORETICAL DESIGN End-to-end mission design for a future deployment of a plant habitat on Mars PUBLIC EXHIBITION Open event that engages the campus in a celebration of our interdisciplinary outcomes.
  • 9. MISSION DESIGN SUMMARY NASA projects a possible human presence on Mars as early as 2030s. Before such an event can happen, we must develop systems capable of sustaining life on the red planet, lightweight and small enough to make the journey and resilient enough to survive without help from home. Many agree that the first step towards proving we can create a sustainable habitat is to design one first for plants. Recognizing that this habitat may not only be a place to survive but thrive and be a beacon and remote connection to and for life on Earth, students from across campus have come together to develop a concept for an deployable autonomous habitat that can sustain life on Mars.
  • 11. MISSION STATEMENT Exploring Viability for Future of Humans on Mars ● Project Viriditas seeks to plant an exploratory biome on the surface of Mars. This habitat will act as a precursor to manned missions to the Red planet ● The project’s main focus is to provide an inspirational monument to human exploration of space. The design of the structure is intended to engage the public with a uniquely shaped habitat ● The biome will also function as an experiment in organism viability and will be consistently collecting data that can be applied in various fields
  • 12. 3. HUMAN CONTACT AND PSYCHOLOGICAL CONNECTION Plants within habitat would serve as a biophilic agent for any future manned missions 2. VIABILITY OF OXYGEN PRODUCTION Sixty plants for two years will produce enough oxygen for a crew of two humans for two months 1. VIABILITY OF FOOD PRODUCTION Acres of plants will be needed to completely support human life, but fresh food may enhance diet 4. ENDURING MONUMENT TO HUMAN EXPLORATION Inspiration of sustaining life on another planet will encourage communal efforts in space exploring
  • 13. MISSION TIMELINE 2016: Prototyping begins 2080: Plants have produced enough oxygen to sustain crew 2030: Mission is sent with roughly 60 plants 2032: Habitat erected, air is stored and plants are monitored 2038: Enough air is stored for two people for 2 months 2040: Humans arrive, maintain hab and add plants Focus on Data Gathering & Oxygen Production Focus on Proof of Concept Focus on support for human habitation
  • 14. DESIRED IMPACT Third Party Takeaway ● The process of keeping a closed-loop ecosystem functioning on another planet will provide a useful testing ground for design and creation of a human habitat ● The data gathered from the habitat will be informative to plant lifecycle and adaptation research ● The technology used in the monitoring and control of the biome will augment current extraterrestrial communication protocols ● The earth interaction component will provide inspiration to people living on earth as they get to experience a martian environment with familiar earth organisms.
  • 16. TRANSPORTATION Deployable Architecture 4.1.1 Travel Duration With current technology 6month travel time 4.1.2 Payload Size Fits into the payload bay of the SpaceX Falcon Heavy or SLS Rocket (15’ (4.6m) inner diameter) Structure is meant to transport in the collapsed state 4.1.3 Materials and Seed Survival in Transit Plants remain dormant in seed state during transit
  • 17. MARTIAN ENVIRONMENT Environmental Issues Temperature Ranges Soil Water Atmosphere Light Dust Radiation Precipitation -133C to 27C MONTH LONG DUST STORMS SEASONAL CO2 FROST 600PA (~0.6% EARTH) PERCHLORATES MEAN SOLAR IRRADIANCE 588.6 W/m2 (40% EARTH INTENSITY) POLES SUBSURFACE LIQUID BRINE Little Protection from Solar Radiation; avg. of 300 mSv
  • 18. MARTIAN ENVIRONMENT Design Constraints Temperature Ranges Soil Water Atmosphere Light Dust Radiation Precipitation Use Martian light to grow plants Settle far from where dust storms originate and use vibration of the drill to shake off dust. Surfaces which are not conducive to dust collection Create earth like atmosphere inside habitat for plants despite the outside atmosphere being 0.6% that of earth’s Use partial sunlight to light the plants in the habitat; be wary of radiation plants are receiving Collect water from martian substrate using drill Not using Martian soil for plant substrate
  • 19. MISSION OPERATIONS Communications Constraints ● One way transmission delay ranges from 13 min to 24 min ● 2 week period of time when Mars is out of view (i.e, no contact) ● Habitat must operate completely autonomously ● Data must be stored onboard for a brief amount of time
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  • 23. AVAILABILITY OF RESOURCES Light Water Month Hours of Sunlight January 11.25 February 11.50 March 11.85 April 12.25 May 12.70 June 13.00 July 13.00 August 12.75 September 12.40 October 12.00 November 11.60 December 11.30
  • 25. ECOSYSTEM PRECEDENTS Our Question: Can we create a closed loop system based on symbiotic biological interactions? Biosphere 2 MELiSSA Project - ESA Living Machines: John Todd
  • 26. Interacting Layers Photosynthesizing, decomposing, and algal layers are, grown simultaneously. By designing symbiotic relationships, we are replicating Earth ecosystems in Martian terrains and beyond. The layers provide supplemental nutrition to future space crews, along with gas and nutrient exchanges between layers.
  • 27. Gas exchange The decomposer layer produces carbon dioxide when it breaks down organic matter from the photosynthesizing layer. This provides necessary gases for the photosynthesizing and algal layers, which in turn produces oxygen for the decomposer layer.
  • 28. 6.1.3 Algae Spirulina N2 , P, CO2 , and light consumer O2 producer Growth rate: 30% per day (cont. light) Air Temp: 25-38ºC Water Temp: 25ºC Rel. Humidity: 50-75% pH Range: 9-10 Light: irradiance 60-100µE m-2 s 6.1.2. Decomposers Oyster Mushrooms (Grey Dove & Italian) Air Temp: 18 -50ºC (ideal early stage T range), 10-18ºC (ideal fruiting T range) Water Temp: 25ºC Rel. Humidity: 80-90% pH Range: 5-6.5 ORGANISM SELECTION + DIVERSITY 6.1.1 Photosynthesizers Baby Bibb Lettuce 125 PPM of Nitrogen during all growth stages UA CEAC nutrient blend Air Temp: 24/19ºC Day/Night Water Temp: 25ºC Rel. Humidity: 50-75% pH Range: 5.5-6.5 D.O >3 ppm Light: 17 mol/m2 per 24 hrs
  • 29. GROWTH MECHANISMS Soil Based High weight payload Inability to restore nutrients in soil Quantity of nutrients in Martian soil might be hard to ascertain Aeroponics Faster growth than soil Less water usage than hydroponics Less weight payload than hydroponics or soil-based growing methods Hydroponics Uses a larger amount of water Smaller selection of plants Energy expenditure and system maintenance of pumps
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  • 34. 02 03 STRUCTURE LIFECYCLE + DEPLOYMENT 01
  • 36. MATERIAL FUNCTION KEY PROPERTIES PHYSICAL PROPERTIES BETAGLASS FABRIC GFRP / PTFE Atomic Oxygen protective layer Protection from outer elements/ high durability/ fire resistant Thicker outer-layer of Betacloth BETACLOTH Silica Glass / Silicon (Actually Silica fiber) Multi-layer Insulation Layer (MLI) Protect against outer elements/ insulative properties/ fire resistant (NASA REALLY hates fire) Multi-layer fabric (astronaut space suits) MYLAR PET/PET Actually (BoPET) / (stretched PET) Multi-layer Insulation Layer (MLI) Radiation shielding/ thermal properties Shiny DRACON PET Multi-layer Insulation Layer (MLI) Thermal blanket White Thermal Fabric POLYURETHANE FOAM Polyurethane Micrometeoroid Orbital Debris (MMOD) protection layer (in between nexetel layers) Low density/ high absorption. Allows for easy folding of outer shell. Foam NEXTEL Alumina MMOD protection layer High strength fabric, fire resistant Ceramic fabric KEVLAR Polyamide Resistant layer/ inner layer Puncture resistant, helps keep physical structure of inflatable Woven fabric COMBITHERM Nylon/EVOH/Nylon/High Ethylene Vinyl Acetate Polyethylene/LLDPE (Complex Polymer film) Bladder (redundant layering) Decreases habitat Permeability (0.1 cc/100 in2-24 hour-atm) Clear plastic material [Combination of polyethylene, nylon, and EVOH (vinyl alcohol) layers] NOMEX Inner layer Puncture resistant/ fire resistant Woven fabric (fire fighter suits)
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  • 41. Overall Structure Light Diffusion Layer Plant Layer Misters + Roots Schroom Layer Algae + Water Coil Water Pump
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  • 43. INTERIOR LAYER PLANS Plant Layer Mushroom LayerOverhead Light Diffusing Layer Algae Layer
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  • 45. BIOME HABITATION SYSTEMS Mechanical and Technical Systems
  • 47. WATER
  • 51. LIGHT DISTRIBUTION AND CONTROL Calculations Natural v Artificial? We use growth LEDs that output light in the red and blue spectrum which the plant is able to use most efficiently
  • 52. High Level Plant Layer LED array and fiber optics above Decomposer Layer Four LED strips in a cross pattern as the Oyster mushrooms require little light Algae Layer LED strips along outside of clear tubes containing algae in the algae compartment LIGHT DISTRIBUTION AND CONTROL
  • 54. PLANT PODS Sensor List • pH Level • Soil Moisture • Lux (light) • Each pod in the plant layer will be equipped with its own set of sensors • Each section in the decomposer layer will be equipped with a set of sensors • These sensor will be used to monitor the growth and health of each plant
  • 55. PLANT MONITORING Cameras • Mounted on Gantries • Controllable Autonomously • Moves in 4 axes • Attached to Central Column
  • 56. BIOME MONITORING Sensor List ● Camera ● Temperature ● Humidity ● Ambient Light ● Air pressure ● CO2 ● O2 • Each layer of the biome will be equipped with ambient sensors • These sensors will be used to monitor the health of the habitat and the ecosystem • The habitat will make decisions based on the values of these sensors • Triple redundant sensors will be placed (Adaptation systems will use the median value to make decisions)
  • 58. DATA AND TRANSMISSION How do we get and store the data? ● Sensor data can be gathered at any interval - currently 5 minutes ● Queued on-site and transmitted whenever possible ● Aggregated and presented in friendly interface for perusal by public
  • 60. DATA USES AND INTERFACES Big Martian Data
  • 62. PRINCIPLES FOR PUBLIC ENGAGEMENT From Earth to Mars and Back Again Earth Mars Astronauts ● Bring the experience of the Martian biome to a global audience. ● Use digital media as a medium to explore an otherwise isolated space. ● Educate viewers and explore data through analogous systems.
  • 63. PUBLIC ENGAGEMENT STRATEGY Systems for Interplanetary Connection VR Experience for General Public VR Tool for Astronauts and Researchers Monumental Installation for Education
  • 64. VIRTUAL REALITY SIMULATION Digital Recreation of Martian Growth
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  • 66. VIRTUAL REALITY RESEARCH TOOLS Data Exploration and Psychological Engagement
  • 68. FUTURE USE Extending the Life of the Biome
  • 69. Biomes create an artificial “forest” on the planet in anticipation of a human habitation.
  • 70. The biome then becomes integrated with human habitats allowing humans to tend to them.
  • 71. THANK YOU Generously supported by: NASA Pennsylvania Space Grant Consortium The Frank-Ratchye Fund for Art @ the Frontier Carnegie Mellon's ProSEED/Crosswalk Initiative