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RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
31
IOTA
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
32
DIMENSIONS + VOLUME
FRONT VIEWSIDE VIEW
TOP VIEW
2.33 m
IOTA is a form most efficient
for construction and being
repurposable. It has a symmetrical
exterior with modules (2 endcaps
and 1 core) that are repeatable.
Total volume
8.7 cubic meter
(307.2 cubic feet)
2.14 m
3.14 m
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
33
ENDCAP OVERVIEW
The endcaps section houses the
seats, console, and food and water
storage. All four astronauts are
facing towards the center so they
have the maximum visual view.
TOP VIEW
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
34
CONSOLE
umbilical cord
attachments
joystick
& controls
The console unit consists of the
retractable displays, umbilical
connectors and food/water access.
In addition, standard flight, navigation
and other MAV systems controls are
integrated into accessible zones.
screens
water access
food storage
FRONT VIEW
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
35
SEATS
The seats are placed at the two
ends facing the center at an angle
to conform the curved profile of
the exterior shell, whilst ensuring
astronaut comfort.
TOP VIEW
CONSTRUCTION SKETCH
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
36
COMMANDER AND PILOT OPERATIONAL SEQUENCE
Screen is hinged above astronauts. The display retracts through
pushing the handle back.
Buttons, switches and controls are all located
within easy reach of astronauts hands during
launch and orbit.
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
37
CORE OVERVIEW
TOP VIEW
FRONT VIEW
The core section houses the bulk of
the MAV systems such as electronics,
life support and sample stowage.
Space is optimized through modular
and standardized forms.
STORAGE COMPARTMENTS
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
38
HATCH
The hatch placement is optimized
for movement during ingress
and egress. The design is based
on the assumption that pilot and
commander will be the first to be
seated whilst mission specialists
will move about performing various
duties.
TOP VIEW
hatches closed
TOP VIEW
both hatches open
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
39
SAMPLES BAG
The sample bag is a standardized
form that can be fit into any of the
stowage containers. It offers thermal
insulation and shock protection
whilst preserving flexibility in the
various samples that will be stowed.
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
40
MISSION SPECIALISTS OPERATIONAL SEQUENCE
Astronauts enter MAV and load samples to bottom storage. Sample bag fits snuggly into storage.
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
41
BATHROOM
TOP VIEW
CURTAIN
The bathroom utilizes the hatch
space that is empty. The curtain,
tissue paper, and hose are hidden
in a compartment near the hatch.
fecal storage
curtain
hose (liquid waste)
toilet (solid waste)
recessed handles
QUARTER SCALE MODEL
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
42
SLEEPING BAG
FRONT VIEW
SLEEPING PLACEMENT
The focus of the sleeping was to
use a cradle inspired head piece
to create a sense of privacy.
canopy
zipper
pockets
Sleeping bags connect to handles.
all positions
accessible to toilet
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
43
LIGHTING
The lighting is distributed through
two types of lights: the long
‘bar’ that stretches the length of
the core section which provides
ambient light and the spotlights in
the endcap section which ensure
astronauts can clearly see their
controls.
TOP VIEW
LIGHTING PLACEMENT
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
44
PROCESS
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
45
PROCESS - INITIAL IDEA
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
46
PROCESS - FULL SCALE CARDBOARD
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
47
PROCESS - QUARTER SCALE MODEL
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
48
PROCESS - FINAL CONSTRUCTION
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
49
PROCESS - FINISHED MODEL
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
50
PROCESS - FINISHED MODEL
RHODE ISLAND SCHOOL OF DESIGN
Design for Extreme Environments 2016
51
IOTA FAMILY
MICHAEL LYE
PROFESSOR
KENTA KONDO
BROWN ENG 2017
AZLEE YU
RISD ID 2017
MEGAN VALANID
RISD ID GRAD
JIHYO KIM
RISD ID 2017
SUNGWHA KANG
RISD ID 2017
MINJU KIM
RISD ID 2017
ROBERT WANG
RISD ID 2017
SAVANNA LI
RISD ID 2017
JEREMY BASS
RISD ID GRAD

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Project IOTA

  • 1. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 31 IOTA
  • 2. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 32 DIMENSIONS + VOLUME FRONT VIEWSIDE VIEW TOP VIEW 2.33 m IOTA is a form most efficient for construction and being repurposable. It has a symmetrical exterior with modules (2 endcaps and 1 core) that are repeatable. Total volume 8.7 cubic meter (307.2 cubic feet) 2.14 m 3.14 m
  • 3. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 33 ENDCAP OVERVIEW The endcaps section houses the seats, console, and food and water storage. All four astronauts are facing towards the center so they have the maximum visual view. TOP VIEW
  • 4. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 34 CONSOLE umbilical cord attachments joystick & controls The console unit consists of the retractable displays, umbilical connectors and food/water access. In addition, standard flight, navigation and other MAV systems controls are integrated into accessible zones. screens water access food storage FRONT VIEW
  • 5. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 35 SEATS The seats are placed at the two ends facing the center at an angle to conform the curved profile of the exterior shell, whilst ensuring astronaut comfort. TOP VIEW CONSTRUCTION SKETCH
  • 6. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 36 COMMANDER AND PILOT OPERATIONAL SEQUENCE Screen is hinged above astronauts. The display retracts through pushing the handle back. Buttons, switches and controls are all located within easy reach of astronauts hands during launch and orbit.
  • 7. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 37 CORE OVERVIEW TOP VIEW FRONT VIEW The core section houses the bulk of the MAV systems such as electronics, life support and sample stowage. Space is optimized through modular and standardized forms. STORAGE COMPARTMENTS
  • 8. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 38 HATCH The hatch placement is optimized for movement during ingress and egress. The design is based on the assumption that pilot and commander will be the first to be seated whilst mission specialists will move about performing various duties. TOP VIEW hatches closed TOP VIEW both hatches open
  • 9. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 39 SAMPLES BAG The sample bag is a standardized form that can be fit into any of the stowage containers. It offers thermal insulation and shock protection whilst preserving flexibility in the various samples that will be stowed.
  • 10. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 40 MISSION SPECIALISTS OPERATIONAL SEQUENCE Astronauts enter MAV and load samples to bottom storage. Sample bag fits snuggly into storage.
  • 11. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 41 BATHROOM TOP VIEW CURTAIN The bathroom utilizes the hatch space that is empty. The curtain, tissue paper, and hose are hidden in a compartment near the hatch. fecal storage curtain hose (liquid waste) toilet (solid waste) recessed handles QUARTER SCALE MODEL
  • 12. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 42 SLEEPING BAG FRONT VIEW SLEEPING PLACEMENT The focus of the sleeping was to use a cradle inspired head piece to create a sense of privacy. canopy zipper pockets Sleeping bags connect to handles. all positions accessible to toilet
  • 13. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 43 LIGHTING The lighting is distributed through two types of lights: the long ‘bar’ that stretches the length of the core section which provides ambient light and the spotlights in the endcap section which ensure astronauts can clearly see their controls. TOP VIEW LIGHTING PLACEMENT
  • 14. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 44 PROCESS
  • 15. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 45 PROCESS - INITIAL IDEA
  • 16. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 46 PROCESS - FULL SCALE CARDBOARD
  • 17. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 47 PROCESS - QUARTER SCALE MODEL
  • 18. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 48 PROCESS - FINAL CONSTRUCTION
  • 19. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 49 PROCESS - FINISHED MODEL
  • 20. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 50 PROCESS - FINISHED MODEL
  • 21. RHODE ISLAND SCHOOL OF DESIGN Design for Extreme Environments 2016 51 IOTA FAMILY MICHAEL LYE PROFESSOR KENTA KONDO BROWN ENG 2017 AZLEE YU RISD ID 2017 MEGAN VALANID RISD ID GRAD JIHYO KIM RISD ID 2017 SUNGWHA KANG RISD ID 2017 MINJU KIM RISD ID 2017 ROBERT WANG RISD ID 2017 SAVANNA LI RISD ID 2017 JEREMY BASS RISD ID GRAD