This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Micrometeoroid and Orbital Debris Enhancements of Shuttle Extravehicular Mobility Unit Thermal Micrometeoroid Garment
ISSN: 0148-7191, e-ISSN: 2688-3627
Published July 17, 2006 by SAE International in United States
Annotation ability available
As NASA is preparing to extend man's reach into space, it is expected that astronauts will be required to spend more and more time exposed to the hazards of performing Extra-Vehicular Activity (EVA). One of these hazards includes the risk of the space suit bladder being penetrated by hypervelocity micrometeoroid and orbital debris (MMOD) particles. Therefore, it has become increasingly important to investigate new ways to improve the protectiveness of the current Extravehicular Mobility Unit (EMU) against MMOD penetration.
ILC Dover conducted a NASA funded study into identifying methods of improving the current EMU protection. The first part of this evaluation focused on identifying how to increase the EMU shielding, selecting materials to accomplish this, and testing these materials to determine the best lay-up combinations to integrate into the current thermal micrometeoroid garment (TMG) design. Part of this study included using extensive hypervelocity testing to identify potential candidate materials. The last part of this study expanded on the previous results by conducting a more thorough investigation into the performance of the top three candidate lay-ups for micrometeor protection. The ability to manufacture the candidates into the current TMG and their effects on the torque of a mobility joint were the main focus points. This paper summarizes the findings of this study.
CitationJones, R., Graziosi, D., Ferl, J., Splawn, K. et al., "Micrometeoroid and Orbital Debris Enhancements of Shuttle Extravehicular Mobility Unit Thermal Micrometeoroid Garment," SAE Technical Paper 2006-01-2285, 2006, https://doi.org/10.4271/2006-01-2285.
- Cadogan D. Shear C. Dixit A. Ware J. Ferl J. Cooper E. Kopf P. “Intelligent Flexible Materials For Deployable Space Structures (INFLEX).” 36th ICES Conference SAE 2006