NASA has continued the development of space systems by applying and integrating improved technologies that include safety issues, lightweight materials, and electronics. One such area is extravehicular (EVA) spacesuit development with the most recent Mark III spacesuit. In this paper the Mark III spacesuit is discussed in detail that includes the various components that comprise the spacesuit, materials and their chemical composition that make up the spacesuit, and a discussion of the 3-D CAD model of the Mark III spacesuit. In addition, the male (CAM) and female (CAF) computerized anatomical models are also discussed in detail. We combined the spacesuit and the human models, that is, we developed a method of incorporating the human models ...
NASA's long-range plans include possible human exploratory missions to the moon and Mars within the ...
Reported herein are results from the Eril Research, Inc. (ERI) participationin the NASA Johnson Spa...
This paper evaluates key functional data parameters that must be considered for suborbital spaceflig...
Ongoing assembly and maintenance activities at the International Space Station (ISS) require much mo...
The International Space Station (ISS) provides significant challenges for radiation protection of th...
We present a design study for a wearable radiation-shielding spacesuit, designed to protect astronau...
We present a design study for a wearable radiation-shielding spacesuit, designed to protect astronau...
The normal working and living areas of the astronauts are designed to provide an acceptable level of...
TransHab, a habitable inflatable structure, has been proposed as a possible module for the Internati...
It is well known that outside the Earth\u27s protective atmosphere and magnetosphere, the environmen...
Reported herein are results from the Eril Research, Inc.(ERI) participationin the NASA Johnson Space...
Human exposure to trapped radiations in low Earth orbit (LEO) are evaluated on the basis of a simple...
Presented is an overview of the development of the integral thermal/micrometeoroid garment (ITMG) us...
NASA Engineers design spacesuits for ultimate protection and functionality in the extreme environmen...
The NASA Extravehicular Mobility Unit (EMU) micrometeoroid and orbital debris protection ability has...
NASA's long-range plans include possible human exploratory missions to the moon and Mars within the ...
Reported herein are results from the Eril Research, Inc. (ERI) participationin the NASA Johnson Spa...
This paper evaluates key functional data parameters that must be considered for suborbital spaceflig...
Ongoing assembly and maintenance activities at the International Space Station (ISS) require much mo...
The International Space Station (ISS) provides significant challenges for radiation protection of th...
We present a design study for a wearable radiation-shielding spacesuit, designed to protect astronau...
We present a design study for a wearable radiation-shielding spacesuit, designed to protect astronau...
The normal working and living areas of the astronauts are designed to provide an acceptable level of...
TransHab, a habitable inflatable structure, has been proposed as a possible module for the Internati...
It is well known that outside the Earth\u27s protective atmosphere and magnetosphere, the environmen...
Reported herein are results from the Eril Research, Inc.(ERI) participationin the NASA Johnson Space...
Human exposure to trapped radiations in low Earth orbit (LEO) are evaluated on the basis of a simple...
Presented is an overview of the development of the integral thermal/micrometeoroid garment (ITMG) us...
NASA Engineers design spacesuits for ultimate protection and functionality in the extreme environmen...
The NASA Extravehicular Mobility Unit (EMU) micrometeoroid and orbital debris protection ability has...
NASA's long-range plans include possible human exploratory missions to the moon and Mars within the ...
Reported herein are results from the Eril Research, Inc. (ERI) participationin the NASA Johnson Spa...
This paper evaluates key functional data parameters that must be considered for suborbital spaceflig...