Evaluating Lumbar Shape Deformation With Fabric Strain Sensors

Objective To better study human motion inside the space suit and suit-related contact, a multifactor statistical model was developed to predict torso body shape changes and lumbar motion during suited movement by using fabric strain sensors that are placed on the body. Background Physical interactions within pressurized space suits can pose an injury risk for astronauts during extravehicular activity (EVA). In particular, poor suit fit can result in an injury due to reduced performance capabilities and excessive body contact within the suit during movement. A wearable solution is needed to measure body motion inside the space suit. Methods An array of flexible strain sensors was attached to the body of 12 male study participants. The participants performed specific static lumbar postures while 3D body scans and sensor measurements were collected. A model was created to predict the body shape as a function of sensor signal and the accuracy was evaluated using holdout cross-validation. Results Predictions from the torso shape model had an average root mean square error (RMSE) of 2.02 cm. Subtle soft tissue deformations such as skin folding and bulges were accurately replicated in the shape prediction. Differences in posture type did not affect the prediction error. Conclusion This method provides a useful tool for suited testing and the information gained will drive the development of injury countermeasures and improve suit fit assessments. Application In addition to space suit design applications, this technique can provide a lightweight and wearable system to perform ergonomic evaluations in field assessments.

Skylab, the Apollo-Soyuz Test Program, and Other Development Suits

This chapter discusses the space suits used aboard the Skylab and Apollo-Soyuz Test Program flights and outlines their differences from the lunar mission suits. It includes details of advanced suits ILC worked on at the time in support of the future Space Shuttle missions NASA had on their drawing boards.

Preserving Our Treasures

When the Apollo program was over, the items that were returned to Earth became treasures to be shared with the American taxpayers who funded this great adventure and with people from around the world. The space suits are the only life-support equipment that was taken to the moon’s surface and brought back to Earth. That we have relatively few items back from lunar missions makes the preservation of equipment and moon rocks all the more important. Fortunately, America has some of the best museums in the world. The Smithsonian’s National Air and Space Museum, located on the Mall in Washington, DC, began as the National Air Museum in 1946. Funding for the present building was approved in 1971 and the museum opened its doors on July 1, 1976.

Lunar and Mars analogue research performed at the HI-SEAS research station in Hawaii, part of the EuroMoonMars - IMA - HI-SEAS campaigns

<p>As of 2018, the International MoonBase Alliance (IMA), has been organizing regular simulated missions to the Moon and Mars at the Hawaii Space Exploration Analog and Simulation (HI-SEAS) habitat. HI-SEAS is a lunar and Martian analog research station located on the active volcano Mauna Loa in Hawaii. The missions that take place at HI-SEAS can be of varied duration, from several days to several months, depending on the needs of the researchers. They are open to space agencies, organizations and companies worldwide to take part in, provided their research and technology testing will help contribute to the exploration of the Moon and Mars. The crews are supported by a Mission Control Center based on the Big Island of Hawaii as well. A series of EuroMoonMars IMA HI-SEAS (EMMIHS) missions have been taking place at HI-SEAS since 2019. These missions bring together researchers from the European Space Agency (ESA), IMA, the International Lunar Exploration Working Group (ILEWG), European Space Research and Technology Centre (ESTEC), VU Amsterdam and many other international organizations. Crews on these missions perform geological, astrobiological and architectural research; technological tests using drones, 3Dprinters and rovers; as well as performing outreach and educational projects. The EMMIHS missions typically last for two weeks each. During this time, the crew is isolated within the HI-SEAS habitat, which they cannot leave without performing EVAs (Extra-Vehicular Activities) in analog space-suits and with the permission of Mission Control. The EMMIHS campaigns aim to increase the awareness about the research and technology testing that can be performed in analogue environments, in order to help humans become multiplanetary species. Furthermore, the research and technological experiments conducted at HI-SEAS are going to be used to help build a Moon base in Hawaii, and ultimately to create an actual Moon base on the Moon, as part of IMA’s major goals. Future missions at HI-SEAS include more EMMIHS campaigns, collaborative missions with ESA, NASA, University of Hawaii, University of South Florida and with companies, such as SIFT and Ketone Technologies.</p>

The Return of Manned Missions

The United States space program has been without a launch vehicle for human spaceflight since 2011. That was when the space shuttle Atlantis returned on its final flight. Since then, NASA has relied on the Russian Soyuz spacecraft to take its astronauts to the International Space Station. However, if all goes to plan this could soon change, as two private companies are working with NASA to launch the first astronauts into orbit. The companies, SpaceX and Boeing, are building crew capsules and rockets, designing space suits, and training astronauts to fly these new vehicles into space.

A First-Order Design Requirement to Prevent Edema in Mechanical Counter-Pressure Space Suit Garments

ABSTRACTIntroductionMechanical counter-pressure (MCP) space suits may provide enhanced mobility relative to gas-pressure space suits. One challenge to realizing operational MCP suits is the potential for edema caused by spatial variations in the applied body-surface pressure (dP). We determined a first-order requirement for these variations.MethodsDarcy’s law relates volume flux, of fluid from capillaries to the interstitial space, to transmural hydraulic and osmotic pressure differences. Albumin and fibrinogen levels determine, to first order, the capillary oncotic pressure (COP). We estimated dP, neglecting hydrostatic pressure differences, by equating the volume flux under MCP and under normal with the volume flux under abnormal variations in COP; then we compared these estimates to results from MCP garment studies.ResultsNormal COP varies from 20-32 mm Hg; with constant hydraulic conductivity, dP≈12 mm Hg. In nephrotic syndrome, COP may drop to 11 mm Hg, yielding dP≈15 mm Hg relative to mid-normal COP. Previous studies found dPmax =151 mm Hg (MCP glove; finger and hand dorsum relative to palm), dPmax=51 mm Hg (MCP arm; finger, hand dorsum, and wrist relative to arm), and dP=52, 90 and 239 mm Hg (three MCP lower leg garments).ConclusionsMCP garments with dPmax≤12 mm Hg are unlikely to produce edema or restrict capillary blood flow; however, garments with dPmax>12 mm Hg will not necessarily produce edema. For example, the hydrostatic pressure gradient at the feet in 1g can range from 70-90 mm Hg. Current garment prototypes do not meet our conservative design requirement.