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Transhab

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A cut away view of a TransHab concept.

TransHab was a concept pursued by NASA to develop the technology for expandable habitats inflated by air in space. Specifically, TransHab was intended as a replacement for the already existing rigid International Space Station crew Habitation Module. When deflated, inflatable modules provide an 'easier to launch' compact form. When fully inflated, TransHab would expand to 8.2 meters in diameter (compare to the 4.4 meter diameter of the Columbus ISS Module).

Contents

History

The name of the project is a contraction of Transit Habitat reflecting the original intention to design an interplanetary vehicle to transfer humans to Mars.

Considerable controversy arose during the TransHab development effort due to delays and increased costs of the ISS program. In 1999, the National Space Society issued a policy statement recommending that NASA cease development of TransHab. Finally in 2000, despite objections from The White House, House Resolution 1654 was signed into law banning NASA from conducting further research and development of TransHab. An option to lease an inflatable habitat module from private industry was included in the bill.

Since that time, the private company Bigelow Aerospace has purchased the rights to the patents developed by NASA and is pursuing a similar scheme for a private space station design. The company has launched the Genesis I and Genesis II pathfinder spacecraft, with plans for additional experimental craft culminating in their BA 330 production model.

Technology

The TransHab design called for a hybrid structure that combines the packaging and mass efficiencies of an inflatable structure with the advantages of a load bearing hard structure.

Multi-Layer Inflatable Shell

Cut-away view of the TransHab multi-layer, space debris and micrometeroid ballistic-shield.

TransHab's inflatable shell consisted of multiple layers of blanket insulation, protection from orbital and meteoroid debris, an optimized restraint layer and a redundant bladder with a protective layer.

TransHab’s foot-thick inflatable shell design had almost two dozen layers. The layers were fashioned to break up particles of space debris and tiny meteorites that might hit the shell with a speed seven times as fast as a bullet. The outer layers protect multiple inner bladders, made of a material that holds in the module’s air. The shell also provides insulation from temperatures in space that can range from plus 121 degrees Celsius (plus 250 degrees Fahrenheit) in the Sun to minus 128 degrees Celsius (minus 200 degrees Fahrenheit) in the shade.

The key to the debris protection in the design and prototype units was successive layers of Nextel, a material commonly used as insulation under the hoods of many cars, spaced between several-inches-thick layers of open cell foam, similar to foam used for chair cushions on Earth. The Nextel and foam layers cause a particle to shatter as it hits, losing more and more of its energy as it penetrates deeper.

Many layers deep in the shell was a layer of superstrong woven Kevlar to hold the module’s shape. The air was held inside by three bladders of Combitherm, a material commonly used in the food-packing industry. The innermost layer, forming the inside wall of the module, was Nomex cloth, a fireproof material that also protected the bladder from scuffs and scratches.

TransHab layout

TransHab was intended to be composed of four levels/floors.

Level 1
The first level houses a kitchen with a refrigerator-freezer, microwave oven, water dispenser, and food preparation equipment as well as a table that seats 12, enough to allow an entire Station resident crew and replacement crew to sit together for meetings or meals. There are three galley racks, a large wardroom table, an Earth-viewing window and a soft stowage array. The Earth-viewing window is 51 centimeters (20 inches) in diameter and is located near the dining area. The window has four panes totaling 10.2 centimeters (4 inches) thick and a hard frame around each window that attaches to all layers of the shell.
Level 2
Crew Quarters -- The crew quarters area has six individual crew quarters which are sized at 2.3 cubic meters (81 cubic feet) of volume per crew quarter and a central passageway located within the second level central core structure and water tanks. Each compartment contains a sleeping bag/sleep restraint, an area for stowing personal items, and a computer entertainment center for recreation and personal work.
Mechanical -- The mechanical room is external to the core structure and uses only half the floor space. It is acoustically and visually isolated. The other half of this area is a clerestory above the wardroom area. The mechanical room consists of an environmental control and life support system, power equipment and avionics equipment and provides return airflow from Level One and Level Three through openings.
Level 3
Level Three houses an exercise area with a treadmill and stationary bicycle. Exercise is important to keep astronauts healthy in weightlessness for long periods. The area also contains a complete health care system with all types of medical and emergency equipment and a type of "space bath" area provided for body cleansing. In addition, this level contains a soft stowage area identical to level one.
Crew Health Care Area -- The crew health care area incorporates two ISS Crew Health Care System racks, a Full Body Cleansing Compartment, changing area, exercise equipment (treadmill and ergometer), a partitionable area for private medical exams and conferencing, and an Earth-viewing window. The Earth-viewing window is 51 centimeters (20 inches) in diameter and is located near the exercise area. The window has four panes totaling 10.2 centimeters (4 inches) thick and a hard frame around each window that attaches to all layers of the shell.
Stowage -- Soft-sided cabinets provide stowage for spare parts, supplies, clothing and other equipment. TransHab would double the stowage room available on the International Space Station.
Level 4
The Pressurized Tunnel Area provides a passageway between TransHab and the vehicle to which it is attached. The tunnel has two standard International Space Station hatches and houses critical equipment required during inflation, such as avionics and power equipment.

References

  1. ^ a b c d e f Kim Dismukes (curator) (2003-06-27). "TransHab Concept". NASA.gov. http://spaceflight.nasa.gov/history/station/transhab/. Retrieved 2007-06-10. 
  2. ^ Kennedy, Kriss (2002). "Lessons from TransHab: An Architect's Experience". AIAA Space Architecture Symposium. Houston, Texas. AIAA 2002-6105. 
  3. ^ National Space Society (NSS.org) (1999-06-10). "National Space Society Announces Policy on TransHab". Press release. http://nss.org/news/releases/release74.html. Retrieved 2007-06-10. 
  4. ^ Office of the Press Secretary via SpaceRef.com (2000-10-30). "President signs H.R. 1654, the "National Aeronautics and Space Administration Authorization Act of 2000."". Press release. http://www.spaceref.com/news/viewpr.html?pid=2949. Retrieved 2007-06-10. 
  5. ^ 106th Congress (2000-01-24). "National Aeronautics and Space Administration Authorization Act of 2000". Library of Congress. http://thomas.loc.gov/cgi-bin/query/z?c106:H.R.1654.ENR:. Retrieved 2007-05-26. 
  6. ^ Sensenbrenner, F James (2000-09-12). "National Aeronautics and Space Administration Authorization Act of 2000, Conference Report". Library of Congress. http://thomas.loc.gov/cgi-bin/cpquery/T?&report=hr843&dbname=106&. Retrieved 2007-06-10. 
  7. ^ Abbey, George W S (2001-02-27). "Letter from NASA JSC Center Director: Actions Required to Address ISS Budget Challenges". NASA via SpaceRef.com. http://www.spaceref.com/news/viewsr.html?pid=2261. Retrieved 2007-06-10. 
  8. ^ Schrimpsher, Dan (2006-08-21). "Interview: TransHab developer William Schneider". TheSpaceReview.com. http://www.thespacereview.com/article/686/1. Retrieved 2007-06-10. 
  9. ^ International Space Station Imagery, image S99-05362, "Computer Generated Still -- Cutaway of the TransHab Module shell showing the various layers," 2001-08-30
  10. ^ 3M Nextel Woven Ceramic Fabric
  11. ^ DuPont, Surlyn-resin, Combitherm-film case study
  12. ^ a b c d e "HSF -- Transhab". NASA. http://spaceflight.nasa.gov/history/station/transhab/transhab_levels.html. Retrieved 2010-02-09. 

External links

v  d  e
Space stations and habitats
Active International Space Station
Defunct
Salyut (Salyut 1 · DOS-22 · Salyut 21, 3 · Cosmos 5571 · Salyut 33 · Salyut 4 · Salyut 53 · Salyut 6 · Salyut 7) · Polyus2 · Mir
Cancelled
ISS-incorporated
Developmental
Proposed
1 Never inhabited 2 Failed launch 3 Part of the Almaz military program
Retrieved from "http://en.wikipedia.org/wiki/TransHab"


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