DAY-1: May 11, 2022
Time	Paper Title	Presenting Author / Session Chair	Affiliation	File Download
06h55 PDT	5 min session joining time
07h00	INTRODUCTORY REMARKS	Ed Boesiger, General Chairman	Lockheed Martin Space, Sunnyvale, CA
		Brandan Robertson, Host Chair	NASA Johnson Space Center, Houston, TX
		Center welcome - TBA	NASA Johnson Space Center, Houston, TX
07h15	Session I: INSTRUMENTS	Jonathan Wood	Lockheed Martin Space, Sunnyvale, CA
07h15	Design of a Deployable Vacuum Seal Cover for the Europa Clipper’s MASPEX Instrument	John Gordon	Sierra Space, Louisville, CO	gordon.pdf
07h40	Laterally Unconstrained Magnetic Joint for Pointing, Scanning, and Steering Applications	Aaron Castillo	Light Steering Technologies, Manchester, NH	krylov.pdf
08h05	Design, Manufacturing, and Testing of Precision Space Flight Qualified Single Degree of Freedom Flexure Based Linear Actuators / Mechanisms	Brandon Schneider	Danbury Mission Technologies (DMT), Danbury, CT	schneider.pdf
08h30	Active Thermal Architecture Cryo Cooler Mechanical Characterization and Thermal Performance Assessment including Practical Considerations of Exported Force and Torque Testing	Bill Zwolinski	Kistler Instrument Corp, Amherst, CT	zwolinski.pdf
08h55	X2B Wide Angle Steering Mirror	Alix Carson	Ball Aerospace & Technologies Corp., Boulder, CO	ostaszerski.pdf
09h20	Lubrication Concept Evaluated for Geared Actuators under Starved Conditions	Erik Nyberg	Luleå Tekniska Universitet, Luleå, Sweden	nyberg.pdf
09h45	15 min Break
10h00	Session II: COMPONENTS & RELEASE MECHANISMS	Adam Dokos	NASA Kennedy Space Center, Kennedy Space Center, FL
	5 min session joining time
10h05	Advances in Bending Flat Plate Shape Memory Alloy Actuation Modeling: Prediction of Actuation Behavior	Michael Halvorson	University of Alabama in Huntsville, Huntsville, AL	halvorson.pdf
10h30	Cost Efficient Space Micro-Switches Based on Contactless Eddy Current Sensor	Gérald Aigouy	Cedrat Technologies, Meylan, France	aigouy.pdf
10h55	Design and Qualification of a Restrain-Release Mechanism for a 600 kg Deployable Panel Array	Alberto Martín Ghiselli	Commision Nacional de Energia Atomica, Buenos Aires, Argentina	quiroz.pdf
11h20	NEA Mini for Low Load Applications – Development and Qualification	Ruben Betancourt	Ensign-Bickford - NEA Electronics, Inc., Moorpark, CA	betancourt.pdf
11h45	Application of Ballistic Modeling and Quasi-Static Severance Testing in the Design of a Bolt Cutter	Jason Kozmic	Chemring Energetic Devices, Downers Grove, IL	kozmic.pdf
12h10	20 min Break
12h30	SPECIAL PRESENTATION – ARGOS - see below	TBA
13h15	End of the Day 1
	DAY-2: May 12, 2022
Time	Paper Title	Author / Session Chair	Affiliation
07h00 PDT	Session III: ACTUATORS AND GIMBALS	Ben Nickless	NASA Langley Research Center, Hampton, VA
	5 min session joining time
07h05	Scan Mechanism Design for Large Deployable Reflector	Christian Hehr & Cristovao Cardoso	Airbus Defence & Space GmbH, Friedrichshafen, Germany	hehr.pdf
07h30	Development of a Thrust Vector Control Mechanism for Deorbitation System	Ewa Majewska	Łukasiewicz Research Network - Institute of Aviation, Warsaw, Poland	majewska.pdf
07h55	Engineering Design of a Thruster-pointing Mechanism (TPM-250) for Deep Space and IOS Nanosats	Emilia Wegrzyn	Added Value Solutions UK, Oxford, Great Britain	wegrzyn.pdf
08h20	Mars 2020 Motor Bearing Failure, Investigation and Response	David Suffern	Sierra Nevada Corporation, Durham, NC	suffern.pdf
08h45	15 min Break
09h00	Session IV: CUBESAT HARDWARE	Landon Moore	NASA Johnson Space Center, Houston, TX
	5 min session joining time
09h05	The GRASS Gravimeter Rotation Mechanism for ESA Hera Mission Onboard Juventas Deep-Space CubeSat	Matthias Noeker	Royal Observatory of Belgium, Brussels, Belgium	noeker.pdf
09h30	From PSYCHE PAM30 to Large Scale Free-Space Optical Communication	Gérald Aigouy	Cedrat Technologies, Meylan, France	aigouy2.pdf
09h55	Developing a Plunger-Based Liquid Propellant Delivery System for CubeSat Propulsion	Pilar Gonzalez Rueda Flores	University of Texas at El Paso Center for Space Exploration and Technology Research, El Paso, TX	gonzalez-rueda-flores.pdf
10h20	Flat Pack HDRM for Low Load Applications	Jason Nave	Ensign-Bickford - NEA Electronics, Inc., Moorpark, CA	nave.pdf
10h45	15 min Break
11h00	SUPPLIER SESSION	Ed Boesiger	Lockheed Martin Space, Sunnyvale, CA
		A rapid fire session of invited suppliers showcasing their latest and greatest products. Each supplier will give their best 3-minute pitch and of course contact information will be available for attendees to follow up.
	Redwire	William Francis	redwirespace.com
	Artemis Space	Geoff Carter	artemis-space.com
	BEI Precision	John Beasley	beiprecision.com
	Diamond-Roltran	Jeffrey Gilling	diamond-roltran.com
	Cobham Advanced Electronic Solutions	Boz Sharif	caes.com
	Ensign-Bickford Aerospace & Defense	Jason Nave	www.ebad.com
	Kistler Instrument Corporation	Bill Zwolinski	www.kistler.com
	Blue Line Engineering	Greg Ames	www.bluelineengineering.com
	Spinner Rotary Joint	Kevin Cody	www.spinner-group.com
	ThinGap, Inc.	John Baumann	www.thingap.com
	Arquimea	Marcello Collado	www.arquimea.com
	Ducommun Incorporated	Francis Castelo	ducommun.com
11h45	15 min Break
12h00	Session V: THE STU LOEWENTHAL TRIBOLOGY SESSION	Stu Loewenthal	Lockheed Martin Space (Retired), Sunnyvale, CA
	5 min session joining time
12h05	Updated Phenolic Ball Bearing Retainer Testing for Space/Vacuum Environments	John Renaud	The Timken Corporation, Keene, NH	renaud.pdf
12h30	Preventing the “Brown Sugar” Lubricant Phenomenon: The Relationship Between PFPE Chemical Compositions and their Susceptibility to Lewis Acid-Catalyzed Degradation	Amanda Stubbs	NYE Lubricants, Inc. Fairhaven, MA	stubbs.pdf
12h55	Performance of MoS2 Coated Gears Exposed to Humid Air During Storage	Tysen Mulder	NASA Glenn Research Center, Cleveland, OH	mulder.pdf
13h20	Bearing Starting Torque Measurements Down to –100°C	Kim Aaron	Jet Propulsion Laboratory, Pasadena, CA	aaron.pdf
13h45	End of the Day 2
	DAY-3: May 13, 2022
Time	Paper Title	Author / Session Chair	Affiliation
07h00 PDT	Session VI: SPACE EXPLORATION	Louise Jandura	NASA Jet Propulsion Laboratory, Pasadena, CA
	5 min session joining time
07h05	Project Orion Crew Impact Attenuation System (CIAS)	Nic Williams	Northrop Grumman, Chandler, AZ	kennedy.pdf
07h30	First Steps to Develop a Triboelectric Wind Turbine for Mars Exploration	Borja Pozo Larrocha	Tekniker, Gipuzkoa, Spain	pozo.pdf
07h55	Mars Sample Handling End-Effector Breadboarding	Isacco Pretto	OHB Italia S.p.A., Milano, Italy	pretto.pdf
08h20	Lunar Dust: Its Impact on Hardware and Mitigation Technologies	Dorota Budzyn	University of Glasgow, Glasgow, Scotland	budzyn.pdf
08h45	Establishment of a Lunar Surface Docking/Mating System Standard	James Lewis	NASA Johnson Space Center, Houston, TX	lewis.pdf
09h10	Design and Test of the Orion Crew Module Side Hatch	Lance Lininger	Lockheed Martin Space, Littleton, CO	lininger.pdf
09h35	15 min Break
09h50	Session VII: ANOMALY & FAILURE ANALYSIS	Łukasz Wiśniewski	Astronika Sp. z o.o., Warsaw, Poland
	5 min session joining time
09h55	Remote Diagnosis and Operational Response to an In-Flight Failure of the Drill Feed Mechanism Onboard the Mars Science Laboratory Rover	Megan Richardson Lin	Jet Propulsion Laboratory, Pasadena, CA	kinnett.pdf
10h20	Radial Loading of Hydrodynamic Bearings due to Magnetic Variation	Warrick Leigh	Jet Propulsion Laboratory, Pasadena, CA	leigh.pdf
10h45	15 min Break
11h00	Session VIII: DEPLOYMENT	Jared Dervan	NASA Marshall Space Flight Center, Huntsville, AL
	5 min session joining time
11h05	Conceptual Design of an Extendable Rope-Inspired Module Space Orbit Arm for Maneuvering: ERM- SOA	Bhivraj Suthar	Chungnam National University, Korea	suthar.pdf
11h30	SWOT and NISAR Boom Ground Deployment Test Challenges & Resolution	Paul Lytal	Jet Propulsion Laboratory, Pasadena, CA	lytal.pdf
11h55	Flatness Adjustment in the Design and Integration of a 35-m2 Space Deployable SAR Antenna	Leonel Garategaray	Commision Nacional de Activides Espaciales, Buenos Aires, Argentina	garategaray.pdf
12h20	15 min Break
12h35	SPECIAL PRESENTATION – Astronaut Don Pettit		Don Pettit is a veteran of two long-duration stays aboard the International Space Station, one space shuttle mission and a six-week expedition to find meteorites in Antarctica.
13h20	TECHNICAL SESSIONS CONCLUSION Herzl Award Presentation	Jonathan Wood	Lockheed Martin Space, Sunnyvale, CA
13h30	End of the Day 3

SPECIAL PRESENTATION – ARGOS

The Active Response Gravity Offload System (ARGOS) is designed to simulate reduced gravity environments such as Lunar (1/6G), Martian (1/3G), or microgravity (0G). ARGOS achieves six degree of freedom motion using an active XYZ system similar to a bridge crane whereas rotational degrees of freedom are passively managed by a gimballing mechanism at the payload interface. ARGOS’ control system continuously tracks and offloads of a percentage of a human or robotic payload’s weight during a wide range of partial gravity and microgravity activities. The facility supports surface operation studies, suit and vehicle requirements development, suit and vehicle design evaluation, robotic development, mass handling studies, and crew training with both suited and shirt-sleeved subjects.