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Procedures for rapid microbiological analysis were performed during simulated surface extra-vehicular activity (EVA) at Meteor Crater, Arizona. The fully suited operator swabbed rock (‘unknown’ sample), spacesuit glove (contamination control) and air (negative control). Each swab sample was analyzed for lipopolysaccharide (LPS) and β-1, 3-glucan within 10 minutes by the handheld LOCAD PTS instrument, scheduled for flight to ISS on space shuttle STS-116. This simulated a rapid and preliminary ‘life detection’ test (with contamination control) that a human could perform on Mars. Eight techniques were also evaluated for their ability to clean and remove LPS and β-1, 3-glucan from five surface materials of the EVA Mobility Unit (EMU). While chemical/mechanical techniques were effective at cleaning smooth surfaces (e.g. RTV silicon), they were less so with porous fabrics (e.g. TMG gauntlet).

As Extra-Vehicular Activity (EVA) is becoming more challenging and a renewed interest into planetary exploration is being pursued, having a spacesuit glove that is able to perform more complex and dexterous tasks with less hand fatigue is critical. In an effort to build upon an already proven foundation a new investigation has been made into reducing the torque of the Phase VI Glove Thermal Micrometeoroid Garment (TMG) along with improving dexterity and tactility. This paper addresses the makeup of the Phase VI Glove TMG and details the investigation into improving the current design. An investigation into alternative heating methods was also pursued.

The I-Suit has been tested in varying environments at Johnson Space Center (JSC). This includes laboratory mobility testing, KC-135 partial gravity flights, and remote field testing in the Mojave Desert. The experience gained from this testing has provided insight for design improvements. These improvements have been an evolutionary process since 1998 to the present. The design improvements affect existing suit components and introduce new components for systems processing and human/robotic interface. Examples of these design improvements include improved mobility joints, a new helmet with integrated communications and displays capability, and integration of textile switches for control of suit functions and tele-robotic operations. This paper addresses an overview of I-Suit design improvements and results of manned and unmanned performance tests.

Since the early 1980’s, the Shuttle Extra Vehicular Activity (EVA) glove design has evolved to meet the challenge of space based tasks. These tasks have typically been satellite retrieval and repair or EVA based flight experiments. With the start of the International Space Station (ISS) assembly, the number of EVA based missions is increasing far beyond what has been required in the past; this has commonly been referred to as the “Wall of EVA’s”. To meet this challenge, it was determined that the evolution of the current glove design would not meet future mission objectives. Instead, a revolution in glove design was needed to create a high performance tool that would effectively increase crewmember mission efficiency. The results of this effort have led to the design, certification and implementation of the Phase VI EVA glove into the Shuttle flight program.

With the initial construction of the International Space Station (ISS) underway, NASA has increased the number of astronauts to meet the demands of such a large construction effort. Both American astronauts and international partners will use NASA's space suit, the Space Shuttle Extravehicular Mobility Unit (EMU) to construct ISS. An increasing number of these new astronauts are females who do not adequately fit in the existing sizes of the EMU. In order to accommodate these astronauts, a smaller version of the EMU is under development. This development will examine all aspects of the EMU and design and fabricate new components to provide the astronauts with a space suit which provides adequate fit and is highly mobile.

Experience with the Space Shuttle Extravehicular Mobility Unit (EMU) and A7LB spacesuits has shown the need to investigate new spacesuit technologies for future missions requiring highly mobile, light weight and lower cost Extravehicular Activity spacesuit alternatives. An experimental spacesuit designated the I-Suit was developed to show the feasibility of attaining all three major design goals. The I-Suit is a highly mobile, multi-bearing, all soft fabric, prototype full pressure suit designed to operate effectively in zero gravity as well as in planetary applications. The I-Suit was designed with several fixed design requirements and a long list of goals. Once the prototype suit was fabricated, laboratory environment testing was performed in order to compare the I-Suit to the Shuttle EMU spacesuit and the Apollo A7LB spacesuit.

The continuous development of Extravehicular Activity (EVA) spacesuit gloves has lead to an effective solution for performing EVA to date. Some aspects of the current EVA gloves have been noted to affect crew performance in the form of limited dexterity and accelerated onset of fatigue from high torque mobility joints. This in conjunction with the fact that more frequent and complex EVAs will occur with the fabrication and occupation of Space Station Freedom, suggest the need for improved spacesuit gloves. Therefore, several efforts have been conducted in the recent past to enhance the performance of the spacesuit glove. The following is a description of the work performed in these programs and their impact on the design and performance of EVA equipment. In the late 1980's and early 1990's, a spacesuit glove design was developed that focused on building a more conformal glove with improved mobility joints that could function well at a higher operating pressure.

The success of astronauts performing Extra-Vehicular Activity (EVA) is highly dependent on the performance capabilities of their spacesuit gloves. Thermal protection of crewmember's hands has always been a critical concern but has recently become more important because of the increasing role of the crewmember in the manipulation of objects in the environment of space. The utilization of EVA for challenging missions, such as the Hubble Space Telescope (HST) repair and Space Station assembly missions, has prompted the need for improved glove thermal protection. The increased manipulation of hot and cold objects is necessary to complete these complex missions. Thermal protection of the spacesuit glove is accomplished by the Thermal and Micrometeoroid Garment (TMG). The TMG is a multilayered cover that fits over the restraint layer of the spacesuit glove. The TMG is engineered to provide thermal protection for crewmember's hands as well as for the glove bladder and restraint.

ILC Dover successfully designed and developed an advanced high pressure (8.3 psia) Spacesuit Glove for use on the space station. As an aide to fabrication of this glove, a feasibility study has been performed to use laser or photo optical, non contact scanning, CAD and CAM technologies. The current process for fabrication of spacesuit gloves starts by taking hand casts of a crewman's hands in one or more positions. The castings are subsequently measured by hand in critical areas, and a manual system of defining the glove bladder and glove restraint patterns follows. The proposed process will involve collecting dimensional data on hands using laser or photo optical scanning techniques. Key dimensions will be identified on a CAD system. Algorithms pre-programmed in the CAD system along with some CAD modeling will be used to manipulate the scanned data to define the glove bladder and glove restraint.