L2 - Living & Working in Space Flashcards

1
Q

DESCRIBE WHAT DOES THE ISS PROVIDE

A

Research facility
Commercial platform for research
Test bed for advanced technology

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2
Q

DESCRIBE WHY IS USED THE SPACE ENVIRONMENT

A

Advance scientific knowledge
Live, explore and work
Use attributes of space to improve products on earth

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3
Q

WHO IS INVOLVED IN PLANNING THE WORK OF THE ASTRONAUTS?

A

User
Define science requirements
Provide payload planning requirements
Provide expertise
Payload facility
Provide integrated facility planning requirements
Provide expertise on facility operations
Integrate sub-rack payload requirements and interface
Partner (ESA COL-CC, NASA POIC, JAXA SSIPC, ROSCOSMOS MCC-M)
Provide planning requirements for another segment
Integrate payload planning requirements for segment
Develop segment payload planning
ISS payload (NASA POIC)
Integrate segment payload planning products
Provide ISS payload planning products
Manage payload resources
ISS integrated (NASA MCC-H)
Integrate system and payload planning products
Provide integrated ISS planning products

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4
Q

WHAT IS THE TIME DISTRIBUTION FOR ASTRONAUTS IN THE ISS?

A
Pre-sleep + sleep + post sleep + meals = 10.4 hours
	Exercise – 2.5 hours
	Daily planning – 0.5 hours
	Work preparation – 1 hour
	Scheduled work – 6.5 hours
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5
Q

WHAT ARE THE NUTRITIONAL REQUIREMENTSUERIMENTS FOR AN ASTRONAUT?

A
1600-2000 kcal of carbohydrates
	630-1000 kcal of fat
	400-600 kcal of protein
	Vitamins
	Minerals
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6
Q

DESCRIBE THE SPACE FOOD IN THE SPACE STATIONS

A

Mercury / Gemini: prepared, bite size or tube, dense, low taste
Apollo: dehydrated foods, canned, utensils, bars
Skylab: freezer and warmers, 72 items: 6-day cycle menu
Space shuttle: no freezer, re-hydration and oven, commercial, food tray
Mir: heating and re-hydration, containers, choices, fresh foods following re-supply
ISS: freezers, microwave/oven, water recycling, 30-day menu, extended shelf life, salad machine, labelling, earth-like diet

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7
Q

LIST THE FACTORS WHY THE FOOD HAVE REDUCED TASTE AND SMELL

A
Head body fluids
Sickness
Atmosphere
Stress
Radiation
Psychology
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8
Q

LIST SOME CONSIDERETION FOR HYGIENE AND LIVE IN SPACE

A
Washing
Hair
Waste collection system
Sleep
Tools
Leisure
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9
Q

DESCRIBE THE ADVANTAGES OF AN EVA MISSION

A

Access to the worksite
Versatility
Double unplanned sorties than planned

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10
Q

STATE THE CURRENT PERSPECTIVE OF EVA MISSIONS?

A

From 1965, longest ~ 9 hours, total ~ 700, 12 moon EVAs.
The wall of EVA -> from 1997 to 2003: ISS construction
The mountain of EVA -> from 2019 to 2030: Available lunar EVA, 3 “8 hours” EVA / week

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11
Q

WHAT ARE THE APPROACHES TO EVA CAPABILITY WITH ROBOTS?

A

Telerobotics: No preparation, excellent simple tasks, strength. No dexterity
Manned: Versatile. Safety issues, time limitations
Combined: advantage of both. Bottleneck problem.

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12
Q

STATE THE CONDITIONS OF AN EVA MISSION

A

Without spacesuit: Unconscious in 5 sec (hypoxia), saliba and tears fluids boil (below 0.6 atm), cold and trapped gas expansion.
Temperature: from 120º to 200º
Metabolic Rate: From 120w to 580w (rest is 60w-800w)
Duration average: 6 hours

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13
Q

DESCRIBE DECOMPRESSION SICKNESS EFFECTS

A

Spacecraft: 1 atm, spacesuits 30%: need airlock with reduced pressure
DCS: Nitrogen bubbles in joints and muscles (the bends) or brain
Saturation radio: Accepted risk from 1.22 to 1.6

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14
Q

COMPARE NASA SUITS WITH RUSSIAN SUITS

A
STS EMU (NASA): 3 parts, 300 hPa, 1013 hPa (4 h pre-breathing) or 700 hPa (1 h prebreathing). R=1.6
ORLAN DMA (RUSSIAN): 1 part, 400 hPa, 1013 (0.5 h pre-breathing). R=1.8
Both: pure oxygen, liquid cooling garment, water subliminator, LiOH cartridge CO2 Removal
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15
Q

WHAT ARE THE SPACESUIT OPTIONS?

A

Self-contained
Umbilical to Stationary LSS
Detached Portable LSS
Pod

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16
Q

WHAT ARE THE HEALTH RISKS DURING EVA?

A
Separation from spacecraft
Debris and micrometeorite
Foreign body injuries (inhalation, ocular)
Worksite injuries (crush, electrical)
Arms/Suit injuries (burn)
Shoulder/torque injuries
Toxic substances
Hypobaric pressure
LSS failures
Suit leaks
Metabolic loading
Thermal injuries
Light glare / darkness
Radiation
DCS
Dust toxicity
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17
Q

STATE THE EVA PRIMARY REQUIREMENTSUERIMENTS

A
Pressurized volume and breathable atmosphere
CO2 removal
Thermal control and insulation
Physical protection from objects
Waste management
Radiation shielding
Micrometeorites/debris shielding
Communications
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18
Q

STATE THE EVA SECONDARY REQUIREMENTSUERIMENTS

A
Interface for mobility system
Interface for Restraint system
Hydration / nutrition
Comfort
Access to tools; lighting
Immediate access to instructions
User friendliness
Minimal preparation
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19
Q

DESCRIBE THE EXTRAVEHICULAR MOBILITY UNIT (EMU) MATERIALS

A

Inner cooling garment - 2 layers
Pressure garment - 2 layers
Thermal micrometeroid garment - 8 layers
Outer cover - 1 layer

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20
Q

WHAT IS THE RATIO OF PREPARATION VS TIME OUTSIDE?

A

3.6 hours outside – 10 hours of preparation and post-EVA activities

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21
Q

STATE THE MONITORING REQUIREMENTSUIREMENTS OF A SPACESUIT

A
Suit pressure
Suit temperature
O2 consumption
CO2 partial pressure
ECG / heart rate
Body temperature
Radiation exposure
Constant voice communication
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22
Q

STATE THE PROBLEMS EXPERIENCED DURING EVA

A
Eye irritation
Improper boot fit
Vomiting
Toxic exposure
Visor steamed up
Suit ripped at helmet
Rotator cuff tear
Shoulder injury while lunar drilling
Hypothermia and frostbites
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23
Q

LIST THE MEDICAL PROBLEMS THAT MIGHT HAPPEN ON AN EVA MISSION

A
Hypoxia / hyperoxia
Hypercarbia (too much CO2)
DCS
Thermoregulation
Thermal injury
Cardiac dysrhythmias
Waste management
Injuries
Penetrating trauma
Radiation
Toxic contamination
Nuisance substances
How well did you know this?
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24
Q

DEFINE THE HARDWARE DESIGN GUIDELINE

A
Foot restraints
Tethers
Avoid unaided load transfer
Minimize finger and wrist requirementsuirements
Include “soft capture”
Design tasks for productive use
Illumination extremes
Visual status indicators
Placards, labels
25
Q

DEFINE EVA TRAINING CONDITIONS AND TASKS

A

1G mock-ups: fixed position, small equipment, quick-look evaluations, < 30 min
0G parabolic flights: behaviour evaluations, hi-fi cable behaviour, EMU donning/doffing
Neutral buoyancy: crew translation, body positions, equipment exchange, mobility aid, > 30 min

26
Q

DESCRIBE THE NEUTRAL BUOYANCY TRAINING

A

Limitations:
Viscosity: in water hard to initiate motion, easy to stop
Gravity: uncomfortable work upside down, tools are heavy
Day/night transitions: fully lighted pool, thermal constant
Predicting amount of time is difficult

27
Q

DESCRIBE THE EVA RULES OF THUMB

A
Each crewmember should check out his or her own suit
“Make before break” tether protocol
“Slower is faster”
“EVA is an art”
Glove is not a hammer
90% body positioning
28
Q

DESCRIBE THE CHARACTERISTICS OF A SURFACE EVA SUIT

A
Apollo EVA – 22 h
Dust abrasion
Wrist deformation
Impaired function due to dust
Enhancements:
Dexterity, mobility, fatigue
Durability and weight
Susceptibility to dust and abrasion
Onsite cleaning and maintenance
Recharging of consumables
29
Q

DESCRIBE THE ADVANCED EVA SYSTEM WISH LIST

A
No pre-breathe
Modular design
Durability
Regenerable
Rapid check-out
Flexibility
Real-time telecommunication
Rapid donning / doffing
Enhanced restrain system
Increase mobility and dexterity
Comfort level up to 8 h
For planetary surface EVA:
Dust controlled
Easy replacement for short-life components
Discardable covers
Enhancement of manual dexterity
Number of suits per crewmember
Augmented reality
30
Q

DESCRIBE WHAT DOES THE ISS PROVIDE

A

Research facility
Commercial platform for research
Test bed for advanced technology

31
Q

DESCRIBE WHY IS USED THE SPACE ENVIRONMENT

A

Advance scientific knowledge
Live, explore and work
Use attributes of space to improve products on earth

32
Q

WHO IS INVOLVED IN PLANNING THE WORK OF THE ASTRONAUTS?

A

User
Define science requirements
Provide payload planning requirements
Provide expertise
Payload facility
Provide integrated facility planning requirements
Provide expertise on facility operations
Integrate sub-rack payload requirements and interface
Partner (ESA COL-CC, NASA POIC, JAXA SSIPC, ROSCOSMOS MCC-M)
Provide planning requirements for another segment
Integrate payload planning requirements for segment
Develop segment payload planning
ISS payload (NASA POIC)
Integrate segment payload planning products
Provide ISS payload planning products
Manage payload resources
ISS integrated (NASA MCC-H)
Integrate system and payload planning products
Provide integrated ISS planning products

33
Q

WHAT IS THE TIME DISTRIBUTION FOR ASTRONAUTS IN THE ISS?

A
Pre-sleep + sleep + post sleep + meals = 10.4 hours
	Exercise – 2.5 hours
	Daily planning – 0.5 hours
	Work preparation – 1 hour
	Scheduled work – 6.5 hours
34
Q

WHAT ARE THE NUTRITIONAL REQUIREMENTSUERIMENTS FOR AN ASTRONAUT?

A
1600-2000 kcal of carbohydrates
	630-1000 kcal of fat
	400-600 kcal of protein
	Vitamins
	Minerals
35
Q

DESCRIBE THE SPACE FOOD IN THE SPACE STATIONS

A

Mercury / Gemini: prepared, bite size or tube, dense, low taste
Apollo: dehydrated foods, canned, utensils, bars
Skylab: freezer and warmers, 72 items: 6-day cycle menu
Space shuttle: no freezer, re-hydration and oven, commercial, food tray
Mir: heating and re-hydration, containers, choices, fresh foods following re-supply
ISS: freezers, microwave/oven, water recycling, 30-day menu, extended shelf life, salad machine, labelling, earth-like diet

36
Q

LIST THE FACTORS WHY THE FOOD HAVE REDUCED TASTE AND SMELL

A
Head body fluids
Sickness
Atmosphere
Stress
Radiation
Psychology
37
Q

LIST SOME CONSIDERETION FOR HYGIENE AND LIVE IN SPACE

A
Washing
Hair
Waste collection system
Sleep
Tools
Leisure
38
Q

DESCRIBE THE ADVANTAGES OF AN EVA MISSION

A

Access to the worksite
Versatility
Double unplanned sorties than planned

39
Q

STATE THE CURRENT PERSPECTIVE OF EVA MISSIONS?

A

From 1965, longest ~ 9 hours, total ~ 700, 12 moon EVAs.
The wall of EVA -> from 1997 to 2003: ISS construction
The mountain of EVA -> from 2019 to 2030: Available lunar EVA, 3 “8 hours” EVA / week

40
Q

WHAT ARE THE APPROACHES TO EVA CAPABILITY WITH ROBOTS?

A

Telerobotics: No preparation, excellent simple tasks, strength. No dexterity
Manned: Versatile. Safety issues, time limitations
Combined: advantage of both. Bottleneck problem.

41
Q

STATE THE CONDITIONS OF AN EVA MISSION

A

Without spacesuit: Unconscious in 5 sec (hypoxia), saliba and tears fluids boil (below 0.6 atm), cold and trapped gas expansion.
Temperature: from 120º to 200º
Metabolic Rate: From 120w to 580w (rest is 60w-800w)
Duration average: 6 hours

42
Q

DESCRIBE DECOMPRESSION SICKNESS EFFECTS

A

Spacecraft: 1 atm, spacesuits 30%: need airlock with reduced pressure
DCS: Nitrogen bubbles in joints and muscles (the bends) or brain
Saturation radio: Accepted risk from 1.22 to 1.6

43
Q

COMPARE NASA SUITS WITH RUSSIAN SUITS

A
STS EMU (NASA): 3 parts, 300 hPa, 1013 hPa (4 h pre-breathing) or 700 hPa (1 h prebreathing). R=1.6
ORLAN DMA (RUSSIAN): 1 part, 400 hPa, 1013 (0.5 h pre-breathing). R=1.8
Both: pure oxygen, liquid cooling garment, water subliminator, LiOH cartridge CO2 Removal
44
Q

WHAT ARE THE SPACESUIT OPTIONS?

A

Self-contained
Umbilical to Stationary LSS
Detached Portable LSS
Pod

45
Q

WHAT ARE THE HEALTH RISKS DURING EVA?

A
Separation from spacecraft
Debris and micrometeorite
Foreign body injuries (inhalation, ocular)
Worksite injuries (crush, electrical)
Arms/Suit injuries (burn)
Shoulder/torque injuries
Toxic substances
Hypobaric pressure
LSS failures
Suit leaks
Metabolic loading
Thermal injuries
Light glare / darkness
Radiation
DCS
Dust toxicity
46
Q

STATE THE EVA PRIMARY REQUIREMENTSUERIMENTS

A
Pressurized volume and breathable atmosphere
CO2 removal
Thermal control and insulation
Physical protection from objects
Waste management
Radiation shielding
Micrometeorites/debris shielding
Communications
47
Q

STATE THE EVA SECONDARY REQUIREMENTSUERIMENTS

A
Interface for mobility system
Interface for Restraint system
Hydration / nutrition
Comfort
Access to tools; lighting
Immediate access to instructions
User friendliness
Minimal preparation
48
Q

DESCRIBE THE EXTRAVEHICULAR MOBILITY UNIT (EMU) MATERIALS

A

Inner cooling garment - 2 layers
Pressure garment - 2 layers
Thermal micrometeroid garment - 8 layers
Outer cover - 1 layer

49
Q

WHAT IS THE RATIO OF PREPARATION VS TIME OUTSIDE?

A

3.6 hours outside – 10 hours of preparation and post-EVA activities

50
Q

STATE THE MONITORING REQUIREMENTSUIREMENTS OF A SPACESUIT

A
Suit pressure
Suit temperature
O2 consumption
CO2 partial pressure
ECG / heart rate
Body temperature
Radiation exposure
Constant voice communication
51
Q

STATE THE PROBLEMS EXPERIENCED DURING EVA

A
Eye irritation
Improper boot fit
Vomiting
Toxic exposure
Visor steamed up
Suit ripped at helmet
Rotator cuff tear
Shoulder injury while lunar drilling
Hypothermia and frostbites
52
Q

LIST THE MEDICAL PROBLEMS THAT MIGHT HAPPEN ON AN EVA MISSION

A
Hypoxia / hyperoxia
Hypercarbia (too much CO2)
DCS
Thermoregulation
Thermal injury
Cardiac dysrhythmias
Waste management
Injuries
Penetrating trauma
Radiation
Toxic contamination
Nuisance substances
53
Q

DEFINE THE HARDWARE DESIGN GUIDELINE

A
Foot restraints
Tethers
Avoid unaided load transfer
Minimize finger and wrist requirementsuirements
Include “soft capture”
Design tasks for productive use
Illumination extremes
Visual status indicators
Placards, labels
54
Q

DEFINE EVA TRAINING CONDITIONS AND TASKS

A

1G mock-ups: fixed position, small equipment, quick-look evaluations, < 30 min
0G parabolic flights: behaviour evaluations, hi-fi cable behaviour, EMU donning/doffing
Neutral buoyancy: crew translation, body positions, equipment exchange, mobility aid, > 30 min

55
Q

DESCRIBE THE NEUTRAL BUOYANCY TRAINING

A

Limitations:
Viscosity: in water hard to initiate motion, easy to stop
Gravity: uncomfortable work upside down, tools are heavy
Day/night transitions: fully lighted pool, thermal constant
Predicting amount of time is difficult

56
Q

DESCRIBE THE EVA RULES OF THUMB

A
Each crewmember should check out his or her own suit
“Make before break” tether protocol
“Slower is faster”
“EVA is an art”
Glove is not a hammer
90% body positioning
57
Q

DESCRIBE THE CHARACTERISTICS OF A SURFACE EVA SUIT

A
Apollo EVA – 22 h
Dust abrasion
Wrist deformation
Impaired function due to dust
Enhancements:
Dexterity, mobility, fatigue
Durability and weight
Susceptibility to dust and abrasion
Onsite cleaning and maintenance
Recharging of consumables
58
Q

DESCRIBE THE ADVANCED EVA SYSTEM WISH LIST

A
No pre-breathe
Modular design
Durability
Regenerable
Rapid check-out
Flexibility
Real-time telecommunication
Rapid donning / doffing
Enhanced restrain system
Increase mobility and dexterity
Comfort level up to 8 h
For planetary surface EVA:
Dust controlled
Easy replacement for short-life components
Discardable covers
Enhancement of manual dexterity
Number of suits per crewmember
Augmented reality