cryogenic and vacuum compatible metrology systems...cryogenic and vacuum compatible metrology...
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Cryogenic and Vacuum Compatible Metrology Systems 2012 SBIR Phase I Project
1 August 2012
Mirror Tech Days – Rochester, NY
Prepared by:
Gregory Scharfstein
President
Flexure Engineering
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Started at Johns Hopkins …
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• Radiation-hardened Neutron Monochromator @ JHU
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CryoVac Engineering
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80K IR Camera (WIYN WHIRC) @ JHU
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CryoVac Opto-Mechanical Systems
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• JWST … 30K Engineering – Opto-mechanical designs – Cryogenic Calibration
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Flexure’s Customer List
• NASA JWST (NIRCam, ISIM), MMS, ICESat-II • NASA SBIR Program • QinetiQ North America • Oceaneering • NIST • Brown University • Advanced Magnet Lab • Micro Aerospace Solutions • ASU Biodesign Institute
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Purpose of Our Phase I Project
• To create a cryogenic and vacuum compatible LIDAR scanning head (LSH), integrated to a thermal-vacuum chamber, that can produce better than 5 micron, 3 sigma, measurement uncertainties on optical structures and systems at a range of 10 meters, in high vacuum, and at temperatures down to 20 Kelvin.
• To identify two metrology instruments that can leverage the technology of the cryo/vac LSH and extend the capabilities of in-situ, cryogenic metrology.
• Technology Innovation: DeepCryo Actuation, Knowledge, and Control
We define “DeepCryo” as an environment whose room
temperature is below 100K (-173 deg C / -279 deg F).
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Multi-headed Metrology System
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(3X) LIDAR
SCANNING HEAD
PAYLOAD TABLE
20K ACTIVE
RADIATION SHIELD
INTERNAL WINDOW
100K ACTIVE
RADIATION SHIELD
VIBRATION
ISOLATION SYSTEM
PAYLOAD /
METROLOGY
STAND
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Applications of Our Innovation …
• NASA – JWST, WFIRST, NEO Missions [ISRU] to Cryogenic Destinations (Lunar
Poles, Asteroids)
– In Situ measurement of large structures in thermal-vac chambers (non-cryogenic, cryogenic)
• Non-NASA / Commercial – Superconducting Innovations for Renewable Energy (HTS Wind
Turbines, HTS Flywheels)
– The Navy’s All-Electric Ship (requires large cryogenic volumes for superconducting power creation and storage)
– Cryogenic Data Centers
– Other Extreme Environment Facilities (Beryllium manufacturing, Salt Water Test Facilities)
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DeepCryo Actuation, Knowledge and Control
20K to 80K Test
Chambers
HTS Test Facility
NEO/Lunar Test
Chambers
DeepCryo Robotic
Cleanroom
DeepCryo Electronics
DeepCryo Mechanisms
DeepCryo Sensors
DeepCryo Human Interfaces
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Technologies and Facilities
NEO/Lunar Test
Chambers
CubeSats Test Chambers
Lunar Crater / Asteroid Analog
Chambers
Lunar Rover Test Chambers
Lunar Volatiles Test Chambers
DeepCryo Robotic
Cleanroom
Lunar and Asteroid ISRU
/ Mining
Cryogenic Propellant Storage
and Delivery
Cryogenic Curation Facilities
Orbiting Propellant Storage
and Delivery
HTS Test Facility
HTS Power Creation, Storage
and Delivery
HTS Actuation and Control
HTS Electronics
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Current Cryogenic Systems
The state-of-the-art in space environment simulation does not offer truly DeepCryo and vacuum compatible actuation, knowledge, and control.
• DeepCryo: an environment where the room temperature is below
100 K • Current technology solves the vacuum problem, but only marginally
solves the cryogenic problem … as a system • NASA Projects are challenged to take the cryogenic problem head-
on due to cost and schedule. Therefore work-arounds are typically implemented.
• In order to truly solve the cryogenic problem, it must be given the proper venue … A Research and Development Project (such as SBIR/STTR) is better suited to begin solving the DeepCryo problem.
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Path to All Cold Systems
• Achievable solutions include systems that operate at higher cryogenic temperatures (220K+, i.e. mil spec COTS)
• Building hardware operable at 220K begins the long-term development path to engineer complete, DeepCryo and vacuum compatible systems.
• Continued development and funding will then bring the operating temperatures down to our target of 20K.
Essential design note: Any DeepCryo, All-Cold System, must start at about 300K (perhaps 350K to 400K for a bake-out) and “travel along the temperature dimension” until the system arrives at its operating DeepCryo destination.
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Laser Radar
• Non-contact metrology
• Direct measurement of hardware surface
• 75 mircon uncertainties for a 10m range
• Not cryo or vacuum compatible
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Schematic of LSH
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FOCUSING OPTICS
SCANNING OPTICS
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LIDAR Scanning Optics Conceptual Design from Flexure’s 2011 SBIR Phase I
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ELEVATION
AXIS
LIDAR
BEAM
AZIMUTH AXIS
SCANNING
MIRROR
BELT DRIVE,
BOTH AXES
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LIDAR Scanning Optics Conceptual Design from Flexure’s 2011 SBIR Phase I
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LIDAR Focusing Optics Designed for 20K Operation
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SCANNING
MIRROR
INVAR-
METERED
DOUBLET
50 mm
TRANSLATION
STAGE
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LIDAR Focusing Optics Designed for 20K Operation
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CROSS
ROLLER
BEARINGS
2-2-2
KINEMATIC
MOUNTING
2-2-2
KINEMATIC
MOUNTING
2-2-2
KINEMATIC
MOUNTING
FLEXURE
MECHANISMS
FLEXURE
MECHANISMS
FLEXURE
MECHANISMS
FLEXURE
MECHANISMS
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LIDAR Focusing Optics: Cross Section Designed for 20K Operation
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INVAR
METERED
DOUBLET
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LIDAR Focusing Stage Designed for 20K Operation
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Phase I / Phase II Activities…
• Phase I: – Integrate Scanning and Focusing Optics Assemblies
• Add motion control and positional feedback
– Flexure mechanism analysis – Baffling / Coatings – Venting / Light-weighting – Complete Error Budget for single LSH
• Phase II – Thermal Analysis and Design – STOP Analysis – Multi-Headed Error Budget (trilateration) – ETU Fabrication and Testing
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Encoders from BEI
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• 24-bit Resolution
• Vacuum Compatible
• Operates down to -55 degrees C [218 K]
• First Step: separate head from electronics
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The Mobile Chamber
• Customized and modular thermal-vacuum metrology system
• Creates the shortest path to science by integrating the required metrology instrumentation with The Mobile Chamber.
• A leasing program for Project’s provides following benefits:
– Offload the cryogenic engineering work and start with a working chamber.
– More easily upgrade or downgrade the chamber based on changes in testing requirements
– Rely on Flexure’s extensive maintenance program to make sure The Mobile Chamber stays functional.
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The Mobile Chamber
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The Path Forward …
• Phase II Opportunities
– Encoders / Motion Control
– STOP Analysis
– Multi-Headed Error Budget (trilateration)
Proposal Due: 23 August 2012
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