Exploration EVA Workshop
July 25, 2019
in partnership with NASA Johnson Space Center
The Technology Collaboration Center, in partnership with the NASA Johnson Space Center, will hold a Exploration EVA (ExtraVehicular Activity) Workshop at the NASA Johnson Space Center, on Thursday, July 25.
During the morning sessions, there will be briefings on the Exploration EVA program strategy and challenges. In the afternoon, there will be collaboration forum sessions with group discussions on several topic areas covering NASA's interests and potential opportunities for the outside community.
If your organization is interested in exploration EVA or spacesuit technologies, please visit the TCC’s website to register for the workshop.
Tickets for the workshop are $100, with TCC members eligible for a 50% discount. Also, for $150 a TCC Individual membership and full workshop ticket can be purchased, which includes a member discount on TCC events for the next year.
Details on the workshop, including the agenda, presenters, and workshop location will be provided to registered attendees, prior to the workshop.
Please contact the TCC about submitting a Collaboration Request or for workshop sponsorship opportunities.
7:30 Networking Breakfast, sponsored by Aerospace Corporation
8:00 Welcome & Announcements
8:20 Guest Speaker
8:45 Exploration EVA Strategic Roadmap
9:05 xEMU Demonstration Status
9:40 National Policy Directives & EVA
10:00 Networking Break, sponsored by Oceaneering
10:20 Lunar & Mars Mission
10:50 Exploration EVA Challenges: Planetary Science
11:15 Exploration EVA Challenges: Human Health & Performance
12:00 Guest Speaker & Lunch, sponsored by UTC Aerospace
1:00 Collaborative Forum: Exploration EVA Challenges - Hardware Development & Gaps
2:45 Networking Break
3:00 Collaborative Forum: Paving a Path to an EVA Suit "Standard"
5:05 Closing Remarks
6:00-7:30 Networking Reception
Next Generation Spacesuit Technology Challenges:
Cis-Lunar (microgravity EVA beyond LEO) – Needed for flight in next 5-7 years
- High Strength-to-Mass Ratio Components (Enhancing; Enabling for surface)
- Need mass/stress-optimized structures for PGS upper torso, bearings, and brief to bring PGS mass below 150 lb
- Previously evaluated chopped fiber composite bearings, composite upper torso and brief, and titanium bearings
- Low-Consumable Trace Contaminant Removal (Enhancing)
- Need a continuous trace contaminant removal capability that is regenerative (not a routinely consumable item).
- Activated charcoal is the state of the art and provides a logistics hit to all exploration reference missions to remove NH3, CO, CH2O, CH3SH, etc. The minimum objective would be to remove all of the significant compounds that threaten to exceed the 7-day SMAC during an EVA with the optimal objective to enable removal of less significant compounds.
- Graphical Display and Input Device (Enabling)
- Need a radiation tolerant graphical display that is compatible with the suit (either 100% O2 compatible and inside the PGS -OR-compatible with the helmet & visors) and operable by the suited crewmember.
- Dust Tolerant Mechanisms (Enabling for surface)
- Need bearings and mechanisms (relief valves, purge valves, disconnects, rear entry hatch, actuators, etc) that function after being exposed to direct dust and/or that are easily maintained during a mission
- Active Tintable Electronic Visor Coating (Enhancing)
- Need to incorporate active tintable electronic coating technologies such as electrochromics or variable solar reflectance into a polycarbonate helmet
Lunar Surface (partial gravity) – Needed for flight in next 6-10 years
- Environmental Protection Garment (Enabling)
- Need dust tolerant and maintainable/cleanable fabric and suit integration mechanism with thermal protection sufficient for vacuum thermal environment.
- Previous testing has shown advantages to coated fabrics with bonded seams at preventing dust migration but coatings failed early in presence of abrasive lunar regolith
- Also need refined methodology for assessing abrasion resistance of materials and dust migration through EPG.
- Surface Optimized Space Suit Boots (Enabling)
- Need boots compatible with mobility (ankle and mid-foot) required for walking in gravity environments that maintain stability on loose and uneven terrain, can be adjusted at pressure to improve fit during EVA, provide proper insulation from conductive ground contact (+/-250F), durable for abrasive dirt and dust environment, and comfortable for multi-hour wear
- Previous boot iterations have highlighted ankle transition as key design problem: need volume to don/doff boot but also provide stability to prevent heel slip and blisters during active use
Mars Surface (partial gravity, partial atmosphere) – Needed for flight in next 10-20 years
- Environmental Protection Garment (Enabling)
- Need dust tolerant and maintainable/cleanable fabric and suit integration mechanism with more thermal protection for non-vacuum thermal environment.
- Non-vacuum Continuous CO2/RH Removal (Enabling)
- Need continuous CO2/RH removal capability that can operate within the vacuum and Martian atmospheres
- Specific areas of interest include:
- Update/supersede amine state of the art
- Improvements in amine uptake
- Alternative processes such as temperature swing adsorption, selective permeable membranes, etc.
- Augment amine operation using thermal swing adsorption approach
- Augment amine operating using boost compressor to enable pressure swing operation in the Martian atmosphere
- Dust Tolerant Mechanisms (Enabling)
- Need protection of bearings, relief valves, purge valves, disconnects, rear entry hatch, actuators and other mechanisms to preclude dust from hampering motion / function over operational life on Martian surface
- Soil constituent parts are dissimilar to lunar soil in both physical and chemical properties
- Heat Rejection for Vacuum and Non-vacuum Applications (Enhancing)
- Need heat rejection compatible with vacuum and Martian environment.
- The current state of the art is the Spacesuit Water Membrane Evaporator (SWME) with degraded performance under Martian conditions.
- LiCl radiators that capture the H2O vapor from the SWME provide a potential solution. A boost compressor on the SWME vapor outlet could potentially yield improved cooling.
- Bio-med sensor (Enabling)
- Need a radiation hardened, wearable biomedical system which does not require the crew to shave that provides heart rate and rhythm data, at a minimum
- Must be compatible with 100% oxygen environment
- Multi-gas Monitoring (Enhancing)
- Need a system to measure/monitor (O2, CO2, H2O), (NH3, CO, CH2O, CH3SH), etc.
- Measuring of the trace contaminants becomes more necessary with a pressure or temperature swing adsorption continuous removal approach for trace contaminants as it would remove the traditional activated charcoal cartridge from the list of logistics items but would require some level of validation that the function was operating beyond the human nose.
EVA or Spacesuit Collaboration Requests:
Any organization can submit a Collaboration Request to the TCC related to EVA or spacesuit technologies, and have the TCC highlight that request at the workshop and on the TCC's website.
The TCC waives normal program fees for all Collaboration Requests submitted in conjunction with a TCC workshop.
For more information on submitting a Collaboration Request, please contact the TCC.
Available Workshop Sponsorships:
Organizations interested in sponsorships for the Exploration EVA Workshop should contact Bob Prochnow, Executive Director of the Technology Collaboration Center at 281-969-7801 or via e-mail at Bob.Prochnow@techcollaboration.center.
Sponsorships are available for the afternoon networking break and the networking reception.