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AAE450 Senior Spacecraft Design
Crystal WilcoxWeek 3: February 1st, 2007
Structures Group
Mars Habitat , Transfer Vehicle (Crew Hab)
AAE450 Senior Spacecraft Design
Mars Habitat SpecificationsMass, Volume, Thickness of Radiation Shielding and Material
Living Quarters: Surface Area (m2) Volume (m3)
69.115 43.9823
Thickness (m) Volume (m3) Mass (kg)
Polyethylene 0.16 11.0584 11058.4
Aluminum 0.05 3.45575 9606.99
Total LQ Shielding 0.21 14.51415 20665.39
Common Area: Surface Area (m2) Volume (m3)
175.929 150.796
Thickness (m) Volume (m3) Mass (kg)
Polyethylene 0.02 3.51858 3518.58
Aluminum 0.01 1.75929 4890.83
Total CA Shielding 0.03 5.27787 8409.41
Material Thickness (m) Volume (m3) MassAL (kg)
Aluminum 7075 0.139669 10.3469 29074.8
Structure + Shielding 0.169669 15.62477 37484.21
Systems Section:
Thickness (m) Volume (m3) Mass (kg)
Polyethylene 0.02 3.51858 3518.58
Aluminum 0.01 1.75929 4890.83
Aluminum 7075 0.139669 10.3469 29074.8
Total SS Shielding 0.169669 15.62477 37484.21
Mitchell's Numbers from Human Factors For Radiation Shielding
Mass Consumables Shielding Material Systems
(kg) 21793.5 29074.8 29074.8 5639.25
Volume Consumables Shielding Material Systems
(m^3) 149.136 19.792 10.3469 9.086
Total Mass (kg) 85582.35
Total Volume (m^3) 188.3609
Total Volume of Shell (m^3) 30.1389
AAE450 Senior Spacecraft Design
Height (m) Diameter (m) Surface Area (m2)
Living Quarters: 3.5 4 69.115
Common Area: 3 8 175.929
Systems Section: 3 8 175.929
AAE450 Senior Spacecraft Design
Backup – Schematic
• Living Quarters– Center of Habitat.– Taller Than the Common Area surrounding it. – More Radiation Shielding.– Separated in 4 Sections for Private Quarters.– One Bed on Floor. – One Bed that Comes out of the inner wall
Closest to the center.
AAE450 Senior Spacecraft Design
Backup – Schematic
• Common Area– Kitchen Area– Bathroom Area– Small Food Storage Area– Rest is Split up into 4 common rooms
• Supply Area – Below the Common Area/Living Quarters– Atmosphere Supply– Water Supply– Mass Food Storage
AAE450 Senior Spacecraft Design
Backup – Material Properties
Elastic Modulus
(Pa) Poisson's Ratio Density (kg/m^3)Yield Strength
(Pa) Ultimate Tensile
Strength (Pa)
Shear Modulus (Pa)
Aluminum 7075 72400000000 0.33 2780 440000000 572000000 28000000000
Density (kg/m^3) Volume (m^3) for thickness in living quarters Volume (m^3) for thickness in Common Area
Polyethylene 1000 11.0584 3.51858
Aluminum 2780 3.45575 1.75929
Volume = Surface Area x Thickness
AAE450 Senior Spacecraft Design
Backup – Forces and Stress
Common Area
Mars Earth
Forces (N) 216696 570253
Stress (Pa) 159647 420123
System Area
Mars Earth
Forces 297910 783974
Stress 219479 577576
These Stresses pass the Yield Strength of the Aluminum 7075
AAE450 Senior Spacecraft Design
Backup – Calculations
Surface Area of a Cylinder = 2*pi*r^2 +2*pi*r*h
Mass = Density x Volume
Volume = MAL7075 / DensityAL7075
Volume = pi*h*tAL7075*(D – tAL7075)
Stress = Force / (Base*thickness)
Fmars = (Mrs + MAL7075)x(0.38g)
FEarth = (Mrs + MAL7075)x(1g)
AAE450 Senior Spacecraft Design
Backup – Kate Mitchell’s TotalsTotal Mass and Volume for Habitat 2
Max Water on board (at one time) 25022.624 kgWater Storage Volume 25.02 m3
Water total and Food Total
Max Food on board (at one time) 19430.4 kg
Food Volume 67.584 m3
Component Mass (kg) Volume (m3)
Consumables* 57730.57 126.84
Crew Accommodations 4994.90 27.07
Water Recycling System 200.00 0.80
Atmospheric Supply System 5440.85 8.37
Private Quarters - 60.00
Crew Common Area - 60.00
Radiation Shielding 26638.00 -
Totals 95004.32 283.08
Conservative (120%) Totals 114005.18 339.70
AAE450 Senior Spacecraft Design
Backup – Kate Mitchell’s
Components Mass (kg/p) Mass (kg) Volume (m3/p)Volume
(m3)
Sabatier Reactor (2x) [5] 76 304 0.14 0.56
O2 Tankage [1] - 1128.15 - 2.15
N2 Tankage [1] - 3888.7 - 4.86
Contaminant Control System [5] 20 80 0.15 0.6
Redundant Parts (10% system hardware) - 38.4 0.116
Totals 5439.25 8.286
Water Recycling System
CO2 Removal/Oxygen Generation System
Water Recycling System Mass Units Mass (kg) Volume Units Volume (m3)
Vapor Compression Distillation (VCD) (2x)[5] 50 kg/p 200 0.2 m3/p 0.8
AAE450 Senior Spacecraft Design
Backup – Kate Mitchell’s Mass Mass Units Subtotal (kg) Volume Volume Units Subtotal (m3)
Galley and Food Systems
Cooking/eating supplies (pans, plastic dishes, plates, etc.) 5 kg/p 30 0.0014 m3/p 0.0084
Freezers 0.75 kg/kg food 14572.8 0.00393 m3/kg food 76.361472
Conventional Oven 50 kg 50 0.25 m3 0.25
Microwave oven 35 kg 35 0.15 m3 0.15
Sink, spigot for hydration of food and drinking water 15 kg 15 0.00135 m3 0.00135
Dishwasher 40 kg 40 0.56 m3 0.56
Waste Collection System
Waste Collection System (1 toilet) 45 kg 45 2.18 m3 2.18
Personal Hygiene
Shower 75 kg 75 1.41 m3 1.41
Handwash/mouthwash faucet 8 kg 8 0.01 m3 0.01
Personal hygiene kit 1.8 kg/p 10.8 0.005 m3/p 0.03
Clothing
Washing machine 100 kg 100 0.75 m3 0.75
Clothes dryer 60 kg 60 0.75 m3 0.75
Recreational Equipment and Personal Stowage
Personal stowage/closet space 50 kg/p 300 0.75 m3/p 4.5
Housekeeping
Vacuum (prime + 1 spare) 8.7 kg 8.7 0.05 m3 0.05
Trash compactor/trash lock 150 kg 150 0.3 m3 0.3
Crew Health Care
Exercise equipment 145 kg 145 0.19 m3 0.19
Medical/Surgical/Dental suite 1000 kg 1000 4 m3 4
Medical/Surgical/Dental consumables 500 kg 500 2.5 m3 2.5
AAE450 Senior Spacecraft Design
Backup – Mitchell’s Consumables
Consumable Mass Mass Units HAB1 (kg) HAB2 (kg)
Kitchen/oven cleaning supplies (fluids, sponges, etc) 0.25 kg/d 391 528
WCS supplies (toilet paper, cleaning solutions, filters, etc.) 0.05 kg/p/d 312.8 422.4
Contingency fecal and urine collection mittens/bags 0.23 kg/p/d (15 days) 13.8 13.8
Hygiene supplies 0.075 kg/p/d 469.2 633.6
Clothing 99 kg/p 396 396
Trash bags 0.05 kg/p/d 312.8 422.4
Total Mass 1895.6 2416.2
Consumable Volume Volume Units HAB1 (m3) HAB2 (m3)
Kitchen/oven cleaning supplies (fluids, sponges, etc) 0.0018 m3/d 2.8152 3.8016
WCS supplies (toilet paper, cleaning solutions, filters, etc.) 0.0013 m3/p/d 8.1328 10.9824
Contingency fecal and urine collection mittens/bags 0.0008 m3/p/d (15 days) 0.048 0.048
Hygiene supplies 0.0015 m3/p/d 9.384 12.672
Clothing 0.336 m3/p 1.344 1.344
Trash bags 0.002 m3/p/d 12.512 16.896
Total Volume 34.236 45.744
AAE450 Senior Spacecraft Design
Backup – References
• Specifications From Breanne and Kirk
• Kate Mitchell’s Mass and Volume Numbers From Human Factors
• www.braeunig.us/space/specs/ares.htm
• AAE 454 Webct Detailed notes