Noahs Ark - Part 2 - Process
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Transcript of Noahs Ark - Part 2 - Process
� TABLE OF CONTENTS TABLE OF CONTENTS �
Introduction
Initial Brainstorming
Initial Project Description
Initial Scenario 1
Initial Scenario 2
Initial Scenario 3
Initial Ideas HF
Presentation at NASA
Feedback from NASA
Radiation Analysis
Function Analysis
Problem Analysis Solar Flare
Detailed Scenario
Selected Scenario
4-5
6-7
8-9
10-11
12-13
14-15
16-17
18-19
20-21
22-23
24-25
26-29
30-35
36-37
� �INTRODUCTION
After several lectures, discussion and round tours we started to have an idea about which challenges NASA faces with the goal of going to the Moon by 2020. By brainstorming different themes such as communication, different health kits and radiation protection we came to the conclusion that protect-ing against the harmful solar flares was the most crucial one and gave us the greatest challenge.
INTRODUCTION
� �
Noah´s Ark - Emergency Radiation Protection
Our goal is to design a solution that will protect thelunar explorers from the harmful effects of radiation.It will function as an emergency shelter when a solarflare event occurs.
Overall Vision
We would like to create a solution that facilitates every day life for humans in space and by design visualize complex concepts such as Noah’s Ark.
Background
Without the protection of the Earth’s atmosphere and magnetosphere as-tronauts are exposed to high levels of radiation. Galactic cosmic rays (GCR) gives constant radiation but is only lethal if exposed over a longer period of time. Solar Particle Events (SPE) and Solar Flare Event (SFE) on the other hand can kill an unprotected person in a single burst. In the habitat the crew will be protected but on longer excursions the astronauts might not have enough time to return if they receive a solar flare alarm. Within 30 minutes they have to be able to protect themselves for up to 4 days.
Assumptions
- The solution should be implementable on the moon 2020.
- The crew will use a pressurized vehicle to explore the surface.
- The maximum excursion duration will be 7 days.
INITIAL PROJECT DESCRIPTION INITIAL PROJECT DESCRIPTION
- The solution has to protect 2 crew members for up to 4 days.
- It is possible to utilize Regolith as a part of the protection solution.
- Within 30 minutes the crew has be in protection.
- The solution will set out from an existing rover concept or an already established lunar surface scenario.
Noah and Larry seek protection under the rover
They connect to the LSS via “umbilical cords”...
...and an additional suit layer fills up with water...and an inflatable shield folds out and fills up with water
Solar flare alarm goes off!
Water tanks in the rover floorfunctions as additional protection
NoahLarry
10 11INITIAL SCENARIO 1INITIAL SCENARIO 1
Noah and Larry transfer through a hatch
They park the rover above the bunker and lower the chassis
NoahLarry
Solar flare alarm goes off!
...or Noah and Larry use explosives to create a bunker
The regolith functions as a natural protection
An inflatable structure deploys
The bunkers are “pre-made”...
1� 1�INITIAL SCENARIO 2INITIAL SCENARIO 2
1�
...and Larry connects to the LSS
...and helps Larry to get in through a suit lock
Noah parks the rover above the hole and lowers the chassis
INITIAL SCENARIO 3
Solar flare warning goes off!
The shelter deploys and Noah transfers through the hatch...
Larry goes into the “pre-made” bunker
Noah
Larry
INITIAL SCENARIO 31�
�0 �1
Trust the soil?
Will cavities col-lapse when rover drives overDifferent soil compositions on different parts of moon
Dig holes in ad-vance
rover digs or in advance or on location.
Shape charges
safety, all ready exists ex-plosives in space? explosive bolts?
HMX explosives(her majesties exp.)PETN10-15 grams booster
PROTECTIONREGOLITH
Liquid Hydrogen
Best protection
Extra water tanks?
Might need ad-ditional water for protection...
Wastewaterrecycling
Water as protec-tion4 inches good protection = 10,16 cm
PROTECTIONWATER
Inflatable struc-ture has to adjust to hole, otherwise it will lift the rover
Zipper
Inflatable struc-ture folds down from two sides and connects with airtight zipper (like on spacesuits)
Belly lowers into bunker
PROTECTIONROOM STRUCTURE
Rotate water tanks
Lunar Water towersso water tanks can be refilled when needed
FEEDBACK FROM NASAFEEDBACK FROM NASA
Radiation monitors on their suits
Radiation sensors
up in rover, know when it is a safe to return.
COMMUNICATION MONITORSUPDATE STATUS
radiation levels..highs and lows
Scenario 1
More realistic because of lack of explosives(no holes)
Back-up systems
Combination of the different scenarios.Different levels of actions.
Guidelines
Make recommen-dation for future rover designs.
GENERAL
Polyethylene good protection
10 inches enough = 25,4 cm
Food supply...
can be used for radiation shielding
PROTECTIONOTHER MATERIALS
INFORMATION
All in one
Optimize the most likely scenario but accomondate all of them so the solu-tion works for all 3 scenarios
Leapfrog system
Don’t drive around with all the supply
Shelters prepared in advance
IDEAS
PROBLEMS
OPINION
��RADIATION ANALYSISRADIATION ANALYSIS
RADIATION PROTECTION
COMMUNICATION
SAFETY
EFFICIENCY
WEIGHT
vOLUME
SYSTEM THINKING
CONSEqUENCES
TIME
POLITICS
RECYCLING
APPEARANCE
ROUTINES
TRANSFORMATION
FUTURE POSSIBILITIES
HEALTH
GEOLOGICAL IMPACT
warning system, fast, accurate, intuitive, status update, 2-way (between hab/rover/earth)
man-made bunkers
monitor, diagnose, treat, psychological health, physical health
nanotechnologies, prevention medicine/vaccination, magnetic field protection, exact prediction of solar flare events
explosive, from invisible to functional
standardized, speed of use, well rehearsed
protective, calming, mode indicating, ergonomic
closed loop ecosystem, supply as protection, waste as protection
moral dilemmas, cultural differences
day, night, work outside, work inside, drive, little time for preparation, excursion duration < 7 days, in protection 2h-4days
nausea, cancer, death, abandoned moon/no further exploration, economic
use rover’s life support system, umbilical cords, closed loop, leapfrog system, pre made solutions, reusable
compact when not in use, deployable/flexible structure, inflatable, ISRU
mobile, light-weight material/solution, ISRU
intuitive, user guidelines, minimal interaction, easy of use
back-up system (lifeboat), reliable, foolproof
��
�� ��FUNCTION ANALYSIS
USE EXISTING LSS
UMBILICAL CORDS
LEAPFROG SYSTEM
PRE-MADESOLUTIONS
REUSABLE
SYSTEM THINKING
DF
NF
NF
DF
DF
CLOSED LOOP DF
ECOSYSTEM
SUPPLY ASPROTECTION
WASTE AS PROTECTION
PROTECTIvE
CALMING
CLEAR INDICATION
ERGONOMICS
RECYCLING
APPEARANCE
DF
NF
DF
NF
NF
DF
DF
ROUTINES
STANDARDIZED
SPEED OF USE
REHEARSED
DIAGNOSIS
TREATMENT
PHYSICALWELLBEING
DF
TRANSFORMATION
NF
NF
NF
NF
DF
DF
NF
FAST
PASSIvE TOACTIvE
PSYCHOLOGICALWELLBEING
NF
MONITOR DF
HEALTH
FUNCTION ANALYSIS
COMMUNICATION
WARNING SYSTEM
FAST
ACCURATE
INTUITIvE
STATUS UP-DATE
2-WAY(hab/rover/earth)
BACK-UP SYSTEM
RELIABLE
FOOLPROOF
INTUITIvE
USER GUIDELINES
MINIMAL INTERACTION
EASE OF USENF
SAFETY
EFFICIENCY
DF
NF
DF
NF
DF
DF
NF
NF
NF
DF
DF
DF
WEIGHT
MOBILE
LIGHT-WEIGHT
ISRU
NF
vOLUME
DF
NF
NF
NF
COMPACT
FLEXIBLE STRUCTURE
ISRU DF
TIME
LITTLE TIME TO PREPARE
<4 DAYS IN BUNKER
NF
NF
HF=Head Function
NF=Necessary Function
DF=Desirable Function
RADIATION
SFE PROTECTION
GRR PROTECTION
HF
DF
�� ��
Rover navigation failure
Rover mobility failure
Too far to habitat
Stay on location someexposure
Prepare shelter
Back-up transport
Arriving at habitat
Picked up by other rover
Walk to habitat
Fast back-up system
Back to rover, some exposure, less time to prepare the shelter
IN PROTECTION
Pre made shelters
Rover mobility failure
Rover LSS failure
Rover navigation failure
Rover power failure
No rover back-up system
Rover back-up system
Manual back-up system
Drive back to habitat
Rover breakdown
Arriving at habitat
Picked up byother rover
Walk to habitat
Picked up byother rover
PROBLEM ANALYSIS SOLAR FLARE
Failure
Transport from earth
On the moon
Crash
Return to earth
SOLAR FLARE
Habitat
Excursion
Pressurized rover
Unpressurized rover
EvA
Alarm
No alarm
In rover
Outside rover
Return to habitat
Too far to rover
Return to rover
Solar flare detected
Solar flare not detected
PROBLEM ANALYSIS SOLAR FLARE
�� ��
Too far to habitat
Prepare shelter
IN PROTECTION
Rover mobility failure
Rover LSS failure
Rover navigation failure
Rover power failure
No rover back-up system
Rover back-up system
Manual back-up system
Transport from earth
On the moon SOLAR FLARE
Excursion
Pressurized rover
Alarm
In rover
Outside rover
Return to rover
PROBLEM ANALYSIS SOLAR FLAREPROBLEM ANALYSE SOLAR FLARE
Blast bunker (explosives)Pre made bunker/shelter-in connection to rover-stand aloneProtection in rover (heavy)Potential point of failure
Communication -status update (access rover equipment when radiation is lower)-hab/second crew/second roverLSS-oxygen-food-water-hygiene-thermal control-air pressureHuman factors-physical comfort (ergonomics, light, colors)-psychological comfort (colors, occupancy)
mechanical solutiondisconnect parts long umbelicalcordsmanual blasting
Mobility failureManual backup-push rover into position-disconnect parts for protection-portable solution for EvAsSpare parts for replacementAlternative to wheels-walk, role,crawl, glide, jump, flyLast way out (stay in rover)-water sleeping-bag-compressed materialLifeboat system -if leapfrog systems existsRover controlled from outside
Navigation failureUse existing backup systemSee project by Emma Lööf (flags, low tech solution)
Power failureUsing existing backup systemSolar panelsPower generator, additional batteryNuclear power bar
LSS failureUse existing backup systemExternal lifesupport (portable)Possibility to access rover during radiation minimumEmergency food supplyOxygen masks
Weight/ volumeLimited possibility to bring extra material-pressurized rover + fuel-radiation protection material
Pre positioned supplies?-pressurized rover/rovers-navigation system-pre made radiation shelters
Crew needs quick protectionotherwise the outcome might be lethal
Pre planned excursionsScientific research is the main focusExplore as much as possible of the surface
Functions as mini habitatMore than one rover? -facilitates collaborationLonger excursions are possibleFlexibility / Mobility-no space suit while driving-preparations inside rover-easier to communicate-sort and evaluate samplesLSS, self sufficient <7 daysPartial environment protection
Possibility to use existing solutions?Alarm in rover (monitors & warning system)Alarm on spacesuits (personal warning system)Potential point of failure
Bunkers are constructed in advance ac-cording to planned excursion route
Leapfrog system
Solar flare alarms are located on the rover and the space suits. More detailed information is found on a monitor inside the rover.
When a solar flare alarm occurs the astronauts have to return to the rover. Three scenarios are possible:-both are out on excursion-one of them is on excursion and the other one is in the rover-both are in the rover
The astronauts transfer into the rover through suitlocks. It takes approx. 15min.
Explosives are used as a back-up sys-tem to quickly create a bunker substi-tute if a pre made bunker is unavailable
PROBLEM ANALYSIS SOLAR FLAREPROBLEM ANALYSE SOLAR FLARE�0 �1
The rover is either driven or remote controlled over the bunker
The rover lowers down and seals the cavity
If a mobility failure occurs a part of the rover structure containing water and food can manually be moved to seal the cavity
If a power failure occurs the rover can be pushed into position and mechani-cally lowered
The shelter structure deploys The rover pressurizes the shelter
�� ��PROBLEM ANALYSIS SOLAR FLAREPROBLEM ANALYSE SOLAR FLARE
�� TABLE OF CONTENTS TABLE OF CONTENTS ��
The astronauts transfer down into the shelter through a hatch in the rover floor
The astronauts are now in protection, 30min has elapsed. When outside the shelter, umbilical cords are used to connect to the LSS.
ROvER FLOOR DETAILThe astronauts have access to the LSS through the floor:-water-food-light-oxygen-communication system-staus up-date
On radiation minimum the astronauts can transfer back into the rover to utilize hygene facilities and advanced equipment.
When danger is over the rover is moved. If the shelter has been used it folds back into the rover floor.
When danger is over the astonauts are picked up by a second rover
In the future it might be possible to leave the shelter for other explorers to use. After some time there will be an infrastructure of shelters on the moon
The astronauts drive back to the habitat
��
The astronauts transfer down into the shelter through a hatch in the rover floor
The astronauts are now in protection, 30min has elapsed. When outside the shelter, umbilical cords are used to connect to the LSS.
The astronauts have access to the LSS through the floor:-water-food-light-oxygen-communication system-staus up-date
The rover lowers down and seals the cavity
The shelter structure deploys The rover pressurizes the shelter
SELECTED SCENARIOSELECTED SCENARIO��