The Cloud-Aerosol Transport System (CATS) A New Earth Science Capability for ISS Matthew McGill, Goddard Space Flight Center, Principal Investigator John.

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The Cloud-Aerosol Transport System (CATS) A New Earth Science Capability for ISS Matthew McGill, Goddard Space Flight Center, Principal Investigator John Yorks, Goddard Space Flight Center, Science Lead & Algorithms Charles Trepte, Langley Research Center, Algorithm Support Hal Maring, NASA HQ, Program Scientist 1

The Cloud-Aerosol Transport System (CATS) is a lidar remote sensing instrument built for use on the International Space Station. CATS is a directed opportunity funded by the ISS Program. Payload Developer is NASA-Goddard Space Flight Center “customer” is the ISS Program (HEOMD) SMD is assisting with funding algorithm/processing development (which is a joint effort with LaRC/CALIPSO team) CATS was designed to provide vertical profiles of cloud and aerosol properties at up to 3 wavelengths (355, 532, 1064 nm) CATS is based on existing instrumentation built and operated on the high-altitude NASA ER- 2 aircraft The CATS project has three simultaneous goals: Provide long-term (6 months to 3 years) science from ISS Prove that low-cost, streamlined project approach can work Provide tech demo on-orbit (target ACE mission) – high rep rate laser – photon-counting detection – UV (355 nm) laser operation in space – HSRL receiver concept ISS | Earth Science CATS Overview 2

Use what we already have (i.e., the ISS) to achieve rapid results within an affordable budget – essential in our cost-constrained environment ISS payloads can easily trade mass for cost – the impact on cost can be huge Embrace strict build-to-cost/build-to-schedule mentality to minimize development cycle and cost – multiple lower-cost Class D instruments can accomplish more than one giant Class B instrument Incrementally enhance the ISS Earth observing capability, and grow it to become a vital part of the Earth Science system Build international partnerships for collaborative climate monitoring and exploration ISS orbit covers significant portion of the Earth’s surface, land area, and populated areas 3 ISS | Earth Science Why the ISS makes sense for Earth Science: Why ISS and Why CATS? With that rationale, CATS was funded to be a forcing function for Earth Science from ISS and to be a pathfinder for NASA-developed ISS payloads.

ISS provides a low-cost platform for earth science capabilities CATS will be installed on the Japanese Experiment Module – Exposed Facility (JEM-EF) Orbit is a 51 o inclination orbit at an altitude of about 405 km – Provides comprehensive coverage of tropics and mid-latitudes Primary aerosol transport paths – Permits study of diurnal changes in clouds/aerosols Japanese Experiment Module-Exposed Facility (JEM-EF) on the International Space Station (ISS) ISS | Earth Science ISS Utilization 4

JEM-EF payloads Japanese Experiment Module – Exposed Facility (JEM-EF) ISS | Earth Science ISS & JEM-EF 5

CATS Processing Center NASA GSFC ISS Operational Aerosol Forecast Models VOLCANIC PLUME TRACKING AIR QUALITY MONITORING CLOUD PROPERTIES WILDFIRE DETECTION AEROSOL PROPERTIES Research Forecasting ISS | Earth Science CATS Science Applications

Ice CloudsWater CloudsDustSmokeSea Salt Vertical profiles of backscatter provide important climate information on Earth’s radiation budget However, layer type (i.e., composition) cannot be determined using backscatter at a single wavelength Determining layer type is important because: –Different layers have different microphysical properties which impact radiative balance in different ways –Climate models need to know the vertical/horizontal distribution and properties of atmospheric layers –Current climate models do not accurately predict the vertical structure of cloud and aerosol layers –Lidar data can be used to initialize models for better vertical structure in model output We want to take the measured profile data And turn it into a vertically-resolved “feature mask” that identifies the different types of layers. ISS | Earth Science Backscatter Measurements 7

Depolarization ratio (  ) provides information about particle shape Multiple wavelengths provide information about particle size by ratio of the backscatter (color ratio,  ) Both are needed to accurately determine layer type Ice Clouds:  > 0.40  > 0.85 Dust: 0.20 <  < 0.30 Water Clouds:  ~ 0.0  > 0.85 Smoke:  ~ 0.20 ISS | Earth Science Multiple Wavelengths and Depolarization 8

Science Modes Backscatter: 532, 1064 nm No HSRL Depolarization: 532, 1064 nm Backscatter: 532, 1064 nm No HSRL Depolarization: 532, 1064 nm Backscatter: 532, 1064 nm HSRL: 532 nm Depolarization: 1064 nm Backscatter: 532, 1064 nm HSRL: 532 nm Depolarization: 1064 nm Backscatter: 355, 532, 1064 nm No HSRL Depolarization: 532, 1064 nm Backscatter: 355, 532, 1064 nm No HSRL Depolarization: 532, 1064 nm Mode 1: Multi-Beam Mode 2: HSRL DemoMode 3: UV Demo 405 km m diameter -0.5 o +0.5 o 7 km LFOV RFOV 405 km m diameter FFOV m diameter AFOV 405 km

Laser 1 TypeNd: YVO 4 Laser 1 Wavelengths532, 1064 nm Laser 1 Rep. Rate5000 Hz Laser 1 Output Energy~1 mJ/pulse Laser 2 TypeNd: YVO 4, seeded Laser 2 Wavelengths355, 532, 1064 nm Laser 2 Rep. Rate4000 Hz Laser 2 Output Energy~2 mJ/pulse Telescope Diameter60 cm View Angle0.5 degrees Telescope FOV110 microradians CATS employs 2 high repetition rate lasers – One operates at 532, 1064 nm – Second is seeded to provide narrow linewidth for HSRL measurements and frequency-tripled for use at 355 nm CATS has a 60 cm beryllium telescope with narrow field-of-view (FOV) – 4 instantaneous fields of view (IFOV) Primary Power Supply Telescope Payload Interface Unit (PIU) HSRL Detector Box Telescope Cover Other Detector Boxes Laser 1 ISS | Earth Science CATS Instrument 10

ISS | Earth Science Building the Transceiver 60 cm beryllium telescope, 110  rad field of view Laser 2 bench subassembly side Laser 1 bench subassembly side 11

ISS | Earth Science Integrated and DONE! The instrument shipped to SpaceX for integration on Sep 30, 2014 Integration to the SpaceX Dragon Trunk completed Oct 8, 2014 Expected launch date was Dec 16, 2014; actual was Jan 10,

The Cloud-Aerosol Transport System (CATS) is a lidar remote sensing payload utilizing ISS as an affordable Earth Science observing platform. CATS is designed to study clouds and aerosol properties in the Earth’s atmosphere to Monitor effects of climate change Monitor dynamic events Demonstrate pathfinder instrument for earth science CATS is not an operational science mission -- is an experiment. CATS provides in-space demonstration of technologies for future satellite missions (e.g., ACE) while demonstrating build-to-cost project development with streamlined management structure. ISS | Earth Science CATS Status TIMELINE Jan 10: CATS launched on SpaceX5 Jan 22: installed to JEM-EF Feb 5: “first light” with laser Feb 10: first “science quality” data Feb 10: first underflight with aircraft Feb 12: first continuous 24-hr operation Feb 17 & 20: additional aircraft underflights Feb 12- present: continuing operations, as continuously as possible, within operational constraints To-date on-orbit: Laser #1: 13 billion laser shots, 730+ hrs operation Laser #2: 3 ½ billion laser shots, 250+ hrs operation (that’s abut 65% availability to-date, which is not bad at all for just getting started and dealing with operational constraints of ISS) 13

ISS | Earth Science First Science Data! L1a data from Feb 11, UTC. Top image is 532 nm attenuated total backscatter, bottom image is 1064 nm attenuated total backscatter, and the ISS track corresponding to the data. 14

ISS | Earth Science Airborne Validation Data from Feb 11. Top image is 532 nm normalized relative backscatter (i.e., not yet calibrated) from CATS, bottom image is same for CPL on the ER-2 – the visual correspondence is spectacular. cirrus cloud heights agree mid-cloud heights agree surface return 15

ISS | Earth Science High Rep Rate Works! 16 This is raw, 350 m x 60 m profile data (1064 nm) – spectacular detail! CATS is the first on-orbit demonstration of high repetition-rate, photon-counting lidar. This raw data shows excellent detail and fine structure at raw resolution with a paltry 1-2 mJ pulse energy (at least at night).

ISS | Earth Science Spectacular Cirrus! 17 This is raw, 350 m x 60 m profile data (1064 nm) – spectacular detail! Exceptional cirrus, April 2, 2015 We just happened to be watching the real-time data feed and saw this wonderful cirrus structure.

ISS | Earth Science Spectacular Cirrus! 18 This is raw, 350 m x 60 m profile data (1064 nm) – spectacular detail! ISS nadir(-ish) video camera view at 13:30:42 UTC, spans ~700 km distance Exceptional cirrus, April 2, 2015

ISS | Earth Science Spectacular Cirrus! 19 This is raw, 350 m x 60 m profile data (1064 nm) – spectacular detail! ISS nadir(-ish) video camera view at 13:30:42 UTC, spans ~700 km distance Exceptional cirrus, April 2, 2015

ISS | Earth Science Excellent On-Orbit Demonstration! 20 This is 350 m x 60 m profile data (1064 nm) – spectacular detail! Again, excellent structure and detail in the cirrus cloud. Aerosol below is resolved. This is near-aircraft-quality resolution. Preliminary data indicates excellent detection sensitivity using the photon-counting detection.

ISS | Earth Science CATS Level-2 Data 21 This is raw, 350 m x 60 m profile data (1064 nm) – spectacular detail! Hot off press. First attempt at cramming data through Level-2 processing to retrieve vertical feature mask. For first attempt, not bad at all – now moving towards processing backlog of data and settling in to regular processing routine.

CATS is a spectacular opportunity, and the latitude given by the ISS Program to apply sound engineering and management judgment in the pursuit of generating good science has been demonstrated to work. ISS Program trusted the Payload Developer to derive our own science requirements instead of subjecting the project to externally-derived requirements and oversight Instrument design and requirements are consistent with the [self-generated] science requirements. CATS team has proven that a large attached payload can be built for ~$15M and ~2 years development time. On-time/on-cost completion Succesfully launched and operating The CATS experience and approach is directly applicable to Earth Venture Instrument (EVi) and Earth Venture Mission (EVm) competitive opportunities. The GSFC Class D Constitution has been an important outcome of the CATS effort. ISS | Earth Science Summary 22