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For every 1 hour scheduled for a spacewalk, astronauts spend roughly _____ to ____ hours training underwater in the NBL.
5 to 7
Two methods to help astronauts practice bracing, torque control, and movement mechanics in space
Partial Gravity System (POGO) and Active Reaction Gravity Offload System (ARGOS)
Support divers for the NBL training
2 safety divers, 2 utility divers, 1 camera/float diver
The Thermal Control System contains the ____ and ____ thermal conrol systems.
active, passive
The Passive Thermal Control System (PTCS) utilizes:
coatings, insulation, sun shields, louvers
The Active Thermal Control System (ATCS) utilizies:
coolant bags, cold-plates, pumps, heat exchangers
The internal ATCS (IATCS) uses ______, while the external ATCS (EATCS) uses _____.
water, ammonia
Two thermal control systems are needed because….
humans do not respond well to sudden temperature changes
Each solar array wing (SAW) and photovoltaic array (PVA) are ___ x ___ m
35 × 12
SAWs and PVAs are able to rotate because of the _____.
Solar Array Rotating Joint (SARJ)
The range of power between the SAWs and PWAs is:
120-84 kW
Why does the range of power for the SAWs and PVAs exist?
eclipse
An eclipse between the ISS, Earth, and the Sun lasts for ____ minutes.
30
SAWs are located at ____ - _____ at the end of each arm
P4-P6 and S4-S6
The radiators are located at ____ and ____ on the ISS.
P1 and S1
Communication between the solar array wings and ISS
SAWs → Sequential Shunt Unit (SSU) → Main Bus Switch Unit (MBSU)
Two uses for GNC
orbital reboost, debris avoidance
The four GNC modes
CMG Attitude Control, CMG Thruster Assist, User Data Generation, Wait & Standby
Command, communication, and data-handling link between MCC and ISS
MCC → White Sands Test Facility → Tracking Data Relay Satellite → ISS
The _____ is used to relay temperature, humidity, attitude, and speed info.
S-band
The S-band has an upload speed of ____ kbps.
1024
The _____ is used to communicate audio, video, and payload data.
Ku-band
The Ku-band has an uplink speed of ____ Mbps and a downlink speed of ____ Mbps.
25, 300
The ___________ is used to help with tracking data.
deep-space network
The deep space network (DSN) has three locations in _____, ______, and _____.
Goldstone, Madrid, Canberra
The ______________ manages communication between satellites, ISS, ISS crewmembers, and spacecraft visiting the ISS and MCC.
Communication Radio Frequency Onboard Network Utilization Specialist (CRONUS)
The _____________ monitors and commands spacecraft.
Space Operations Control Center (SOCC)
The _______ oversees payload instruments.
Payload Operations Control Center
The MCC for NASA is located in:
Houston, TX
The MCC for ESA is located in:
Oberptattenhoten, Germany
The MCC for JAXA is located in:
Tsukuba, Japan
The MCC for CSA is located in:
St. Hubert, Quebec
The MCC for ROSCOSMOS is located in:
Star City
ISS Station Modes:
standard, microgravity, reboost, proximity operations, external operations, survival, assured safe crew return
____ kg/crewmember/day of materials consumed on the ISS (mass balance)
5
The ISS has ___ life support subsystems
6
USOS ISS LSS + Assemblies
ACS Atmosphere Control System - maintaining pressure - NPRv, PPRV, MPRV, HPGT, OGA
ARS Atmosphere Revitalization System
THC Temperature & Humidity Control
FDS Fire Detection & Suppression
WRM Water Recovery & Management
VS Vacuum System
(EVA Spport - 7th subsystem)
Atmosphere Control & Supply (ACS)
maintains pressure and partial pressure
modules: positive pressure relief valve, negative pressure relief valve, manual pressure relief valve, high pressure gas tanks (HPGT), oxygen generating assembly (linked to water recovery management)
Time-between maintenance (TBM) and time-between repair (TBR) and time-between failure (TBF)
Atmosphere Revitalization (ARS)
consequence of this system failing: hypercapnia
0.03% amount of CO2 can be breathed in
Carbon Dioxide Removal Assembly (CDRA)
Advanced Closed Loop System (ACLS) - produces water from CO2 then oxygen from water
Trace Contaminant Control System (TCCS) - removes volatile organic compounds (VOC)
Major Constituent Analyzer (ACA) detects levels of VOCs, tells TCCS if there is a leak
Temperature & Humidity Control (THC)
maintains temperature and humidity levels within the comfort box
18-26 degrees C, 25-75% humidity
Common Cabin Air Assembly CCAA - filters particulates
PDMS scrubbers
intramodule or intermodule
Fire Detection and Suppression System FDS
portable breathing apparatus PBA
portable fire extinguisher PFE
Water Recovery Management System WRMS
Urine Processing Assembly - separation, filtration, distillation
Vacuum System
JEM, Columbus
creates a vacuum for experiments
The Advanced Resistive Exercise Device (ARED) is located in ____
Tranquility
On Apollo missions, they used a ________ to exercise.
bungee cord
On the russian space station, they used the _____ and __________.
Chibis and penguin suit (very strong elastic bands)
Exercise Physiology & Countermeasures (EPC) lab
perform aerobic & anaerobic respiration
assess performance during activities
perform task analysis & human in the loop testing
specialized regimen to each astronaut
General training metrics
#reps x #lbs = 1 set
high frequency: 30-45 mA/45 mR
T2: 20.4 kmh
CEVIS: 350W @ 120 rpm
Aerobic: 55-75% VO2
Internal: 60-90% VO2
ARED: 272 kg resistance
Other systems
MARES: Muscle atrophy research exercise system (Columbus)
CEVIS: Cycle ergometer vibration isolation system (Destiny)
VO2 Max
mL of O2 per day of body weight per min
__________ is how the body moves when performing movements
biomechanics
Hybrid Ultimate Lifting Kit (HULK)
similar to rowing machine
Astronaut Strength, Conditioning, & Rehabilitation (ASCR) training
45 days postflight
proprioception: close your eyes and put dinger on nose
postflight reconditioning program
Radiation countermeasures
dosimeters - small radiation detection device
Space Radiation Assessment Group (SRAG) - tracks the amount of radiation each astronaut is exposed to
absolute career radiation limit: 600
radiation shielding material on the ISS: polyethylene
AstroRAD - vest that provides up to 150 mSv of radiation
Zarya
launched 20 Nov 1998
birthing mechanisms
connects to USOS Unity module
Unity
launched Dec 4, 1998
first USOS module
connects to Zarya
Zvezda
attached to Zarya
command center
life support systems
this is where cosmonauts sleep
safest module :)
Destiny
glove box
window
CPR table
JEM
robot arm
Japanese module
connected to Harmony
Harmony
where astronauts sleep
attached to JEM
vacuum system module
Caution & Warning
Class 1: beeps, life-threatening
Class 2: siren, loss of GNC, loss of attitude
Class 3: constant tone, loss of backup GNC, failure of S-band
Class 4: advisory
EMUs
7 hour use: 15 min don, 6 hour EVA, 15 min doff, 30 min reserve
- snoopy cap was derived from Apollo
Internal & External features:
gloves, boot, lower torso, helmet
hard upper torso, portable life support system, communication carrier assembly, liquid cooling and ventilation garment
prebreathe procedures
prevents decompression sickness (DCS)
dissolved gases coming out of solution in body fluids form a gas bubble
denitrogenation - replacing the nitrogen in the body with oxygen
Tasks:
Breathe O2 for 50 min, 10 min exercise at 75% max O2 uptake
30 min O2 breathing while pressure reduced from 14.7 to 10.2 psi
30 min breathing O2 during suit donning
40 min breathing O2 while in suit
In Situ Light Exericise (ISLE)
one countermeasure to DCS, done during prebreathe
Other risks of EVA
drowning in space! happened to Luke
Simplified Aid for EVA Rescure (SAFER)
backpack on astronaut suits
used in case an astronaut is disconnected from the LSS
general eva suit functions
carrying, holding, and grabbing things
bending/stretching
moving upper torso
moving shoulders frequently
moving waist
donning/doffing
MMOD protection
consumables (lss)
space suit materials
vectran
kevlar
nextrel
nomex
Bailout
preparing the cabin - altitude window: 20,000-10,000 feet, auto pilot engaged to keep shuttle stable, crew manually depressurizes cabin
deploying the escape pole - pryotechnic bolts blow the main side hatch off the shuttle, 12 foot escape pole extended outwards
advanced crew escape suit
was worn by flight crew during launch/reentry
O2 from orbiter’s ECLSS supplied to crew
ACES incorporated anti-exposure, anti-gravity suit to prevent pooling of body fluids
Identify:…. on slide
detachable gloves, suit ventilator vale and suit control valve
ISPRL
individual single person life raft
emergency protection
protected astronauts if shuttle lost cabin pressure or if they have to bail out during an emergency at altitudes up to 100,000 feet
High visibility
look at slides idk man
Donning suit
LCG
step in and pull up
sleeve alignment
zipping the pressure layer
gloves and connections
helmet
Suit weighs ____ lbs within harness, parachute, and life raft and ______ lbs with
28, 64
The d ring connects to the __________
parachute pack
airlock functions
ingress
egress
pressurization
depressurization
donning suit
doffing suit
pre breathe
recharge
EVA different parts
Lock:
Power Supply Assembly
Battery Storage Assembly
Don/Doff Assembly
Commeon Berthing Mechanism and Node Hatch
Battery Charging Assembly
In-Flight Refill Unit
Extravehicular Mobility Unit
Water Recharge Bag
Crew Lock:
Intravehicular hatch
EVA hatch