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Apollo 13 Workplace BC 'work environment' branch (WORKPLACES…
Apollo 13 Workplace BC
'work environment' branch
WORKPLACES
EMPLOYMENT DESIGN
INTERFACE
FEEDBACK
CONTROLS
WARNING SYSTEMS
DISPLAYS
EASE OF USE
WORK ENVIRONMENT
LIGHTING
SPACECRAFT
BRIGHT FLASHES OF LIGHT ASSOCIATED WITH PLASMA AT ATMOSPHERIC RE-ENTRY
ARTIFICIAL LIGHTING
NEAR DARKNESS
CONTRIBUTES TO BONE DEMINERALISATION
(WILLIAMS
ET. AL.
, 2009)
LACK OF VITAMIN D FROM THE SUN
OCCURS IMMEDIATELY UPON ARRIVAL IN SPACE
(WILLIAMS
ET. AL.
, 2009)
POWER CONSERVATION
BACKLIT BUTTONS ON CONTROL PANELS
DIFFERENT COLOURED BUTTONS FOR DIFFERENT FUNCTIONS
DIFFERENT SHAPED BUTTONS FOR DIFFERENT FUNCTIONS
HIGH CONTRAST MONITORS
MISSION CONTROL
LOW ARTIFICIAL LIGHT
EASIER TO SEE SCREENS/CONTROL PANEL
BACKLIT BUTTONS ON CONTROL PANEL
HIGH CONTRAST MONITORS
TEMPERATURE
ATRIFICIAL ATMOSPHERE/ENVIRONMENT
POWER CONSERVATION
NO HEATING, VERY COLD
3 DEGREES CELCIUS
CONDENSTATION ON SURFACES INSIDE THE SPACECRAFT
SPACECRAFT DESIGNED
WITH HEAT SHIELDS
PROTECT ASTRONAUTS FROM BURNING ENGINES
PROTECT ASTRONAUTS DURING
RE-ENTRY THROUGH THE ATMOSPHERE
VIBRATION
EXPLOSION
'BANGS AND SHIMMYS' (APOLLO 13 MOVIE)
FRICTION BETWEEN CM AND ATMOSPHERE ON RE-ENTRY
CHEMICAL EXPOSURE
LOW OXYGEN, HIGH CO2 CONCENTRATION
SOLAR RADIATION
(SCHEURING ET AL 2008)
NOISE
EXPLOSION
'BANGS AND SHIMMYS' (APOLLO 13 MOVIE)
ROARING NOISE GENERATED BY FRICTION WITH THE ATMOSPHERE ON RE-ENTRY
ALARMS
AIR / OXYGEN
ARTIFICIAL ATMOSPHERE
WITHIN SPACECRAFT
RELIANT ON ENVIRONMENTAL SYSTEMS PERFORMING WITHIN THE DESIGNED PARAMETERS.
DEADLY OUTSIDE SPACECRAFT WITHOUT PORTABLE ARTIFICIAL ATMOSPHERE AND SPACESUIT
PURE OXYGEN CUASED A FIRE ON APOLLO 1
WIRING WAS CHANGED
WIRING WAS PROTECTED
TEFLON WIRING CRACKED DUE TO HEAT
AND FELL OFF IN APOLLO 13 OXYGEN TANK
EXPOSED WIRING TO PURE OXYGEN
CONTRIBUTING FACTOR IN APOLLO 13 EXPLOSION
CHANGES TO INSULATION/PROTECTION ON WIRING BEHIND SPACECRAFT CONTROL PANELS
MINIMISED THE RISK OF SHORT CIRCUITING WHEN APOLLO 13 COMMAND MODULE WAS RESTARTED WITH CONDENSATION EVERYWHERE
FLAMMABLE MATERIAL REMOVED WHERE POSSIBLE
TEFLON COATING USED
INSIDE OXYGEN TANKS
TEFLON NOT COMBUSTIBLE UNLESS EXPOSED
TO EXTREME HEAT AND PRESSURE
OXYGEN TANK 2 - HIGH PRESSURE AND TEMPERATURE MAY HAVE CONTRIBUTED TO THE EXPLOSION
LITHIUM HYDROXIDE CANNISTERS/CO2 SCRUBBERS
MICRO GRAVITY
HEALTH IMPACTS
NORMAL PHYSIOLOGY, ABNORMAL ENVIRONMENT
(WILLIAMS
ET. AL.
, 2009)
FLUID RE-DISTRIBUTION IN ALTERED ENVIRONMENT
(WILLIAMS
ET. AL.
, 2009)
SPACE SICKNESS
(WILLIAMS
ET. AL.
, 2009)
TYPICALLY SUBSIDES WITHIN
2-3 DAYS AFTER FLIGHT COMMENCEMENT
(WILLIAMS
ET. AL.
, 2009)
INDIVIDUAL RESPOSNSE - SOME EXPERIENCE SPACE SICKNESS FOR ENTIRETY OF JOURNEY
(WILLIAMS
ET. AL.
, 2009)
ALTERED PERCEPTION
(WILLIAMS
ET. AL.
, 2009)
DISORIENTATION
3D ENRIVOMENT OF SPACE - NO 'UP OR DOWN'
(WILLIAMS
ET. AL.
, 2009)
AFFECTS PERFORMANCE, ESPECIALLY AT THE START AND END OF MISSIONS WHEN THE CHANGES ARE MOST EXTREME
(WILLIAMS
ET. AL.
, 2009)
SYMPTOMS
NAUSEA / VOMITING
(WILLIAMS
ET. AL.
, 2009)
STOMACH AWARENESS
(WILLIAMS
ET. AL.
, 2009)
COLD SWEATING
(WILLIAMS
ET. AL.
, 2009)
HEADACHE
(WILLIAMS
ET. AL.
, 2009)
LETHARGY
(WILLIAMS
ET. AL.
, 2009)
TYPICALLY OCCURS WITHIN
1-2 DAYS OF ARRIVNG IN SPACE
(WILLIAMS
ET. AL.
, 2009)
AFFECTS PERFORMANCE, ESPECIALLY AT THE START AND END OF MISSIONS WHEN THE CHANGES ARE MOST EXTREME
(WILLIAMS
ET. AL.
, 2009)
AFFECTS ALL ORGANS OF
THE BODY
(WILLIAMS
ET. AL.
, 2009)
REACLIMATISATION
(WILLIAMS
ET. AL.
, 2009)
GAIT DISTURBANCE
(WILLIAMS
ET. AL.
, 2009)
MOTION SICKNESS
(WILLIAMS
ET. AL.
, 2009)
VERTIGO
(WILLIAMS
ET. AL.
, 2009)
LIGHT-HEADEDNESS
(WILLIAMS
ET. AL.
, 2009)
TYPICALLY 1-2 DAYS DURATION
(WILLIAMS
ET. AL.
, 2009)
WORKPLACE DESIGN
WORKSTATION CONFIGURATION
MISSION CONTROL
SPACECRAFT
LAUNCH CONTROL
ACCESSIBILITY
NASA MISSION CONTROL
THROUGH AN OFFICE BUILDING
SECURITY DOORS
3RD FLOOR
ELEVATOR ACCESS TO FLOOR
MULTI TIERED WORKSTATION PLATFORM LAYOUT
FIRST ROW
NASA HQ
DEPARTMENT OF DEFENCE
(USUALLY A MILITARY GENERAL)
PAO - PUBLIC AFFAIRS OFFICER
DFO - DIRECTOR OF FLIGHT OPERATIONS
SECOND ROW
INCO - INSTRUMENT AND COMMUNICATIONS
O&P - ORGANISATION AND PROCEDURES
FLIGHT - FLIGHT DIRECTOR AND ASSISTANT FLIGHT DIRECTOR
FAO - FLIGHT ACTIVITIES OFFICER
NETWORK - NETWORK CONTROLLER
THIRD ROW
TELMU - TELEMETRY, ELECTRICAL AND EVA MOBILITY UNIT (LM EECOM)
GNC - GUIDANCE, NAVIGATION, AND CONTROL
EECOM - ELECTRICAL, ENVIRONMENT AND COMMUNICATIONS
CAPCOM - CAPSULE CONTROLLER
SURGEON - LIFE SYSTEMS OPERATOR/FLIGHT SURGEON
CONTROL - LM GUIDANCE AND NAVIGATION
FOURTH ROW
RETRO - RETROFIRE OFFICER
FDO - FLIGHT DYNAMICS OFFICER
BOOSTER - BOOSTER SYSTEMS ENGINEER
GUIDO - GUIDANCE OFFICER
SPACECRAFT
STRONG, PROTECTIVE STRUCTURE
DESIGNED TO KEEP ASTRONAUTS IN
ACCESSIBILITY TO CM FOR INITIAL BOARDING
ASTRONAUTS ASSISTED WHEN BOARDING DUE TO BULKY SUITS AND SMALL HATCH
ASTRONAUTS STRAPPED FIRMLY
IN PLACE BY ASSISTANTS
SPACE
VIA AN AIRTIGHT SPACECRAFT
ARTIFICIAL ATMOSPHERE
ARTIFICIAL LIGHTING
STRONG, PROTECTIVE STRUCTURE
ROCKET LAUNCH VEHICLE
VERY TALL REQUIRING AND
ELEVATOR TO REACH TO EMBARK
110M HIGH
FLYING FOX TYPE TOWER EMERGENCY ESCAPE METHOD
TECHNICALLY COMPLEX
ACHIEVE THRUST SUFFICIENT TO BREAK THROUGH THE ATMOSPHERE
NEED TO ACHIEVE THRUST SUFFICIENT TO TAKE OFF
MAINTAIN THRUST UNTIL ORBIT CAN BE ACHIEVED
ADDITIONAL THRUST TO BREAK OUT OF ORBIT TOWARDS THE MOON
PHYSICALLY DIFFICULT
ADDITIONAL THRUST TO BREAK OUT OF ORBIT TOWARDS THE MOON
MAINTAIN THRUST UNTIL ORBIT CAN BE ACHIEVED
ACHIEVE THRUST SUFFICIENT TO BREAK THROUGH THE ATMOSPHERE
NEED TO ACHIEVE THRUST SUFFICIENT TO TAKE OFF
ASTRONAUT MOBILITY IN MICROGRAVITY
(WILLIAMS
ET. AL.
, 2009)
SPACE SUITS ARE BULKY AND CONSTRICTING
FACILITY LAYOUT
3 SPACE VEHICLES
SERVICE MODULE
LUNAR MODULE
COMMAND MODULE
USED DURING FLIGHT
ASTRONUTS RETURN TO EARTH AND SPLASH DOWN
ASTRONAUTS STRAPPED IN FOR BLAST-OFF
MISSION CONTROL
FOUR MAIN PLATFORMS WITHIN MISSION CONTROL
(
https://arstechnica.com/science/2012/10/apollo-flight-controller-101-every-console-explained/
)
SECOND ROW
INCO - INSTRUMENT AND COMMUNICATIONS
O&P - ORGANISATION AND PROCEDURES
FLIGHT - FLIGHT DIRECTOR AND ASSISTANT FLIGHT DIRECTOR
FAO - FLIGHT ACTIVITIES OFFICER
NETWORK - NETWORK CONTROLLER
FIRST ROW
NASA HQ
PAO - PUBLIC AFFAIRS OFFICER
DFO - DIRECTOR OF FLIGHT OPERATIONS
DEPARTMENT OF DEFENCE
(USUALLY A MILITARY GENERAL)
THIRD ROW
TELMU - TELEMETRY, ELECTRICAL AND EVA MOBILITY UNIT (LM EECOM)
GNC - GUIDANCE, NAVIGATION, AND CONTROL
EECOM - ELECTRICAL, ENVIRONMENT AND COMMUNICATIONS
CAPCOM - CAPSULE CONTROLLER
SURGEON - LIFE SYSTEMS OPERATOR/FLIGHT SURGEON
CONTROL - LM GUIDANCE AND NAVIGATION
FOURTH ROW
RETRO - RETROFIRE OFFICER
FDO - FLIGHT DYNAMICS OFFICER
BOOSTER - BOOSTER SYSTEMS ENGINEER
GUIDO - GUIDANCE OFFICER