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THE WAITProject- LESS Flow EVA : SINGLE- PERSON

BRAND GRIFFIN FISO 9 - 16- 20 GENESIS ENGINEERING 1 https://genesisesi.com/ 1 Page 1 Trend

Single Suit Solution Separate Launch/Entry and EVA Lunar Gravity Lunar GravityWeightless Weightless Past Future

Launch/Entry Launch/Entry Options

ApolloApollo A7-LB ExtravehicularApollo A7-LB Orlan DMA ExtravehicularEMU Orlan DMA XEMU Mobility Unit Mobility Unit 180 lbs 310 lbs < 344 lbs*

* Project Technical Requirements Specification, For the Exploration Extravehicular Mobility Unit (XEMU), June 5, 2019, Rev. C, CTSD-ADV-1188 Page 2 “Spacewalking”Walk on - Fly in space

Surface EVA Weightless EVA SPS Weightless Operations Legs Used for Walking Arms Used for Walking Propulsion for “Walking” Arms Used for Operating Tools Arms Used for Operating Tools Manipulators Used for Tools

Legs not used for walking

Page 3 3 Page 3 Weightless EVA Options

Current Planned Planned

= For Weightless Overhead

Extravehicular Exploration Extravehicular Single-Person Mobility Unit (EMU) Mobility Unit (xEMU) Spacecraft (SPS)

Page 4 Page 4 Single-Person Spacecraft

Weightless Posture Baseline Configuration Dual Mode Operation

Crew Enclosure Crown Assembly

External Equipment Bay

Ingress/Egress /Debris Shield Piloted Tele-op

RETIRED

Manned Maneuvering Unit Single-Person Spacecraft Page 5 Progress

Engineering Design University Full Scale Flight Taurus Dome Impact Test Neutral Propulsion System Advanced Life Informatics Proto-Flight and Analysis Competition Mockup Simulator VR Simulator Tests Robotics Support GEN6000 Tests

Applications

ISS Servicing HST Lunar Gateway Mars Transit

Page 6 Page 6 SPS = Wait-less EVA (reduction~70 hours per EVA)

“Nothing happens fast during the preparations for a space walk...it takes several days over about a week to prepare for a space walk.” Don Pettit

“For an astronaut, going outside is a dangerous undertaking that requires days of preparation.” Astronaut

Page 7 Wait-less = Cost-less ~$1.2 M per EVA

Why are Mass and Time Important? 1 hr. ISS Crew Time = $17,500 (approx. $300/min.)

Interim ISS Use and Pricing*

Preparation 58.25 hr. Post-EVA 15.83 TOTAL 74.08 hr.

$17,500/hr. = $1,296,400

Preparation 0.16 hr. Post-EVA 0.16 TOTAL 0.32 hr.

$17,500/hr. = $5,600

*Human Continuity and the International Space Station, 2019 International Astronautical Congress, Washington D.C., Samuel Scimemi, Director, International Space Station,

Page 8 Summary Comparison

Task Suited EVA SPS Wait-less EVA EVA Preparation 58 hours 10 minutes (6 min. for MMU) fit 12 hours No sizing (one size fits all) depress 30-40 minutes No airlock (direct access) Translation 12-34% of EVA Minutes Airlock repress 15 minutes Minutes (pressure equalization) Suit doffing 25 minutes No doffing (direct ingress) Post EVA 15 hours 10 minutes (10 min. for MMU) Training 100 NBL hrs./EVA TBD Simulator hours Gateway Ops No EVA for first 4 years Early and continuous ops

Page 9 Weighs-less: No Airlock for SPS (up to 21,000 lbs. with ISS type Airlock)

ISS Quest Airlock SPS Vestibule (no airlock) (Can be any airlock) (mates with International Dock Sys)

Equipment Lock

Crew Lock

21,896 lbm* 250 lbm ORU/Sample through

Astronauts in Equipment Lock

*NASA EVA Office (EVA) and Alternative Ingress/Egress Methods Document, NASA, EVA-EXP-0031, Baseline, 04/18/2018 Page 10 Wait-less: Rapid Access to Space

Suited EVA Presents Risk Pre- What is Different? No Risk of the Bends Sickness (Bends) To Avoid Getting Bends PAST (Purge ) Apollo System Common Oxygen Atmosphere

SPS 14.7 psi, O2/N2 NOW and FUTURE Common Spacecraft Atmosphere 14.7 psi, O2/N2 (Draft Inter-operability Std. for Gateway) No Pre-breathing Required

ISS Lunar Gateway Spacecraft 14.7 psi, O2/N2

Soyuz Starliner 100 Crew Dragon Orion

Page 11 Wait-less: On-orbit Sizing (12 hrs. for sizing suits)

Large population range requires 106 suit SPS: One size fits all sizing parts on ISS No additional sizing parts

Weightless simulation verified sizing

“A proper space suit fit is particularly challenging because of NASA’s desire to fit an incredibly diverse population (males and females from the 1st to 99th percentile) while developing a minimum number of space suit sizes.”

Complexity of Sizing for Space Suit Applications, Benson E., Rajulu S. (2009) Complexity of Sizing for Space Suit Applications. In: Duffy V.G. (eds) Digital Human Modeling. ICDHM 2009. Lecture Notes in Computer Science, vol 5620. Springer, Berlin, Heidelberg Page 12 Rad-less: Radiation Protection

Exploration Environment Exposed to Radiation Protected Exposed

Radiation Vests Space Suits SPS No Interference Lunar Gateway outside Earth’s Protective Magnetic Field Vest interferes with suit

Inside or Outside

ILC Stemrad Page 13 Pain-less: Induced Trauma

Suit Trauma SPS No ”Suit” Trauma Suit induced trauma can occur even with minimal EVA time1

25 Astronaut Shoulder Surgeries2

Cooling Garment Impressions

Delaminated Fingernails3

Swelling, Inflammation Knee abrasion

1 Extravehicular Activity – Challenges in Planetary Exploration, Carl Walz / Mike Gernhardt, 27 February, 2008, Third Conference and Exhibit, Denver, CO 2 Shoulder Injuries in US Related to EVA Suit Design, R. Scheuring, DO, MS, FAsMA, FAAFP 3 Opperman RA, Waldie JM, Natapoff A, Newman DJ, Jones JA , Probability of spacesuit-induced fingernail trauma is associated with hand circumference, Aviation Space Environ Med 2010 Oct; 81(10):907-13. Page 14 Wet-less: Managing Weightless Liquids

Space Suit SPS Water in Suit Helmet Life-threatening condition

Can’t get hands in helmet SPS has “Hands-in” Operation

Since 2010, 5 EVA water incidents, 1 visual impairment*

*NASA, “Significant Incidents and Close Calls in : EVA Operations,” July 27, 2016

Lessons Learned Conducting Spacewalks from the International Space Station, 88th Annual Scientific Meeting, Joe Dervay M.D. -Flight Surgeon -NASA , Keith Brandt M.D. –Flight Surgeon –KBRWyle, Andrew Washington –ISS Biomedical -KBRWyle Page 15 Wait-less: Reduced Time To/from Work Site (12-34% of EVA for Translation, life support consumables) Suited EVA SPS EVA “In space there’s no resistance to any move you make, so you have MMU ~ SPS to go really slow.” Astronaut

Percent Seven US and Russian ISS EVAs 60 80 EVA Time 0 20 40 100 Work Overhead

7 45 2 1 Troubleshooting Worksite Prep. “MMU can return to the airlock from the furthest Support Equip. point on Space Station (about 146.30 m (480 ft)) in Translation less than 1 minute.”2 Rest

1. Quantifying EVA Task Efficiency, C. Looper and Z. Ney, AIAA 2006-5766 2. Extravehicular Activity Task Work Efficiency, C Looper and Z. Ney, SAE 2005-01-3014 Page 16 Wet-less: Development and Training

Space Suits $$$ SPS Flight Simulator $ (Over 100 hrs. Training per EVA) “Office-like” Environment

•Large unique facility •Many test personnel •No unique training •Conventional Office •Many skilled staff •Safety issues •No certification •Available projectors Divers •Certification Training •No safety issues •Available computers Suit techs •Pressurized gases •On-orbit training •Proven software Overhead crane •Control room •Laptop platform •Few test personnel •Hyperbaric chamber •No on-orbit training

Page 17 Minimal Overhead = New Way for EVA

Day 1 Day 2 Day 3 Overhead Excursion Extensive overhead encourages long EVAs

Crew Rest Day Crew A Re-charge PLSS A

2 Astronauts Suits

Minimal overhead with no pre-breathe allows short or long excursions

Re- Re- Re- charge charge charge A B C (Auto- C A A (Auto- B (Auto- mated) mated) mated)

Different Astronauts Multiple Excursions SPS Short or long excursions No day of rest between EVA Single-Person Not physically demanding No suit re-sizing for different crew Spacecraft : No strength or conditioning requirements No suit cleaning

No prebreathe with automated checkout allows rapid and frequent space access

Page 18 Wait-less: For Gateway EVA Operations

No Suited EVA for Four years Crew Presence (one month/year) Suited EVA No Airlock

20202020 2021 2022 2023 2024 2025 2026 2027 2028 2029

Airlock (last element)

Gateway Buildup

Continuous EVA SPS EVA

Page 19 SPS is the Wait-less EVA Solution

• Rapid access to space • Minimal post EVA overhead • No inventory of suit parts and no “suit fit” issue • One size fits all • SPS enables short EVAs by different crew • Safer • No risk of “bends” • Less flammable • No risk of helmet water • No suit trauma

• Ready access to video, camera views, check lists with onboard Information Management System Extravehicular Mobility Unit (EMU) • Simulator training is agile and less expenses expensive than neutral buoyancy • Piloted and teleop modes offer continuous EVA

Page 20 Page 20 End

Page 21 Suited EVA Overhead Time

ALCLR = Airlock Cooling Loop Recovery Unit

1 EVA Office Extravehicular Activity (EVA) Airlocks and Alternative Ingress/Egress Methods Document, NASA, EVA-EXP-0031, Baseline, 04/18/2018 Page 22