7 THE COMPASS NOTIONAL DESIGN, COMPRISED OF ELEMENTS FROM TRL 3 TO 5, IS A DUAL-CHANNEL PHOTOMETER THAT IMPLEMENTS PRIOR FLIGHT TECHNOLOGY DEVELOPMENTS IN THIN FILM REFLECTIVE COATINGS, COMPACT (CUBESAT-SCALE) ELECTRONICS PACKAGING, AND HIGH HERITAGE PHOTOMETRIC DETECTORS. SPECIFICALLY, COMPASS BENEFITS FROM PRIOR DESIGN AND FLIGHT OF THE USAF CUBESAT TINY IONOSPHERIC PHOTOMETER (I.E. HIGH SENSITIVITY CSI-BASED DETECTOR, CUBESAT-SCALE HIGH-VOLTAGE AND READOUT ELECTRONICS) AND OF NASA'S POLAR SATELLITE UV IMAGER (NARROWBAND VUV-COATED OPTICS). HEREIN, WE PROPOSE TO BUILD A COMPASS PROTOTYPE (ALONG WITH SEVERAL NARROW-BAND FILTERS SAMPLES) AND EXECUTE A TECHNOLOGY MATURATION PLAN VIA A SERIES OF RIGOROUS TESTS AND PHOTOMETRIC EVALUATIONS IN RELEVANT THERMAL/VACUUM, LAUNCH VIBRATION, AND PRELAUNCH HUMIDITY ENVIRONMENTS. IN DOING SO, WE WILL BRING THE INTEGRATED COMPASS PROTOTYPE TO A TRL 6 STATUS AT THE CONCLUSION OF 2 YEARS WITH SUFFICIENT SYSTEM ENGINEERING, SAFETY, AND MISSION ASSURANCE DOCUMENTATION TO SATISFY FULL READINESS FOR OPERATIONAL CUBESAT MISSION INTEGRATION. Funding Only Action ($409) 10/21/19 Not listed THE COMPASS NOTIONAL DESIGN COMPRISED OF ELEMENTS FROM TRL 3 TO 5 IS A DUAL-CHANNEL PHOTOMETER THAT IMPLEMENTS PRIOR FLIGHT TECHNOLOGY DEVELOPMENTS IN THIN FILM REFLECTIVE COATINGS COMPACT (CUBESAT-SCALE) ELECTRONICS PACKAGING AND HIGH HERITAGE PHOTOMETRIC DETECTORS. SPECIFICALLY COMPASS BENEFITS FROM PRIOR DESIGN AND FLIGHT OF THE USAF CUBESAT TINY IONOSPHERIC PHOTOMETER (I.E. HIGH SENSITIVITY CSI-BASED DETECTOR CUBESAT-SCALE HIGH-VOLTAGE AND READOUT ELECTRONICS) AND OF NASA'S POLAR SATELLITE UV IMAGER (NARROWBAND VUV-COATED OPTICS). HEREIN WE PROPOSE TO BUILD A COMPASS PROTOTYPE (ALONG WITH SEVERAL NARROW-BAND FILTERS SAMPLES) AND EXECUTE A TECHNOLOGY MATURATION PLAN VIA A SERIES OF RIGOROUS TESTS AND PHOTOMETRIC EVALUATIONS IN RELEVANT THERMAL/VACUUM LAUNCH VIBRATION AND PRELAUNCH HUMIDITY ENVIRONMENTS. IN DOING SO WE WILL BRING THE INTEGRATED COMPASS PROTOTYPE TO A TRL 6 STATUS AT THE CONCLUSION OF 2 YEARS WITH SUFFICIENT SYSTEM ENGINEERING SAFETY AND MISSION ASSURANCE DOCUMENTATION TO SATISFY FULL READINESS FOR OPERATIONAL CUBESAT MISSION INTEGRATION. ($409) 10/21/19 Not listed THE COMPASS NOTIONAL DESIGN COMPRISED OF ELEMENTS FROM TRL 3 TO 5 IS A DUAL-CHANNEL PHOTOMETER THAT IMPLEMENTS PRIOR FLIGHT TECHNOLOGY DEVELOPMENTS IN THIN FILM REFLECTIVE COATINGS COMPACT (CUBESAT-SCALE) ELECTRONICS PACKAGING AND HIGH HERITAGE PHOTOMETRIC DETECTORS. SPECIFICALLY COMPASS BENEFITS FROM PRIOR DESIGN AND FLIGHT OF THE USAF CUBESAT TINY IONOSPHERIC PHOTOMETER (I.E. HIGH SENSITIVITY CSI-BASED DETECTOR CUBESAT-SCALE HIGH-VOLTAGE AND READOUT ELECTRONICS) AND OF NASA'S POLAR SATELLITE UV IMAGER (NARROWBAND VUV-COATED OPTICS). HEREIN WE PROPOSE TO BUILD A COMPASS PROTOTYPE (ALONG WITH SEVERAL NARROW-BAND FILTERS SAMPLES) AND EXECUTE A TECHNOLOGY MATURATION PLAN VIA A SERIES OF RIGOROUS TESTS AND PHOTOMETRIC EVALUATIONS IN RELEVANT THERMAL/VACUUM LAUNCH VIBRATION AND PRELAUNCH HUMIDITY ENVIRONMENTS. IN DOING SO WE WILL BRING THE INTEGRATED COMPASS PROTOTYPE TO A TRL 6 STATUS AT THE CONCLUSION OF 2 YEARS WITH SUFFICIENT SYSTEM ENGINEERING SAFETY AND MISSION ASSURANCE DOCUMENTATION TO SATISFY FULL READINESS FOR OPERATIONAL CUBESAT MISSION INTEGRATION. $0 6/29/18 6 THE COMPASS NOTIONAL DESIGN, COMPRISED OF ELEMENTS FROM TRL 3 TO 5, IS A DUAL-CHANNEL PHOTOMETER THAT IMPLEMENTS PRIOR FLIGHT TECHNOLOGY DEVELOPMENTS IN THIN FILM REFLECTIVE COATINGS, COMPACT (CUBESAT-SCALE) ELECTRONICS PACKAGING, AND HIGH HERITAGE PHOTOMETRIC DETECTORS. SPECIFICALLY, COMPASS BENEFITS FROM PRIOR DESIGN AND FLIGHT OF THE USAF CUBESAT TINY IONOSPHERIC PHOTOMETER (I.E. HIGH SENSITIVITY CSI-BASED DETECTOR, CUBESAT-SCALE HIGH-VOLTAGE AND READOUT ELECTRONICS) AND OF NASA'S POLAR SATELLITE UV IMAGER (NARROWBAND VUV-COATED OPTICS). HEREIN, WE PROPOSE TO BUILD A COMPASS PROTOTYPE (ALONG WITH SEVERAL NARROW-BAND FILTERS SAMPLES) AND EXECUTE A TECHNOLOGY MATURATION PLAN VIA A SERIES OF RIGOROUS TESTS AND PHOTOMETRIC EVALUATIONS IN RELEVANT THERMAL/VACUUM, LAUNCH VIBRATION, AND PRELAUNCH HUMIDITY ENVIRONMENTS. IN DOING SO, WE WILL BRING THE INTEGRATED COMPASS PROTOTYPE TO A TRL 6 STATUS AT THE CONCLUSION OF 2 YEARS WITH SUFFICIENT SYSTEM ENGINEERING, SAFETY, AND MISSION ASSURANCE DOCUMENTATION TO SATISFY FULL READINESS FOR OPERATIONAL CUBESAT MISSION INTEGRATION. Other Administrative Action $0 6/29/18 Not listed THE COMPASS NOTIONAL DESIGN COMPRISED OF ELEMENTS FROM TRL 3 TO 5 IS A DUAL-CHANNEL PHOTOMETER THAT IMPLEMENTS PRIOR FLIGHT TECHNOLOGY DEVELOPMENTS IN THIN FILM REFLECTIVE COATINGS COMPACT (CUBESAT-SCALE) ELECTRONICS PACKAGING AND HIGH HERITAGE PHOTOMETRIC DETECTORS. SPECIFICALLY COMPASS BENEFITS FROM PRIOR DESIGN AND FLIGHT OF THE USAF CUBESAT TINY IONOSPHERIC PHOTOMETER (I.E. HIGH SENSITIVITY CSI-BASED DETECTOR CUBESAT-SCALE HIGH-VOLTAGE AND READOUT ELECTRONICS) AND OF NASA'S POLAR SATELLITE UV IMAGER (NARROWBAND VUV-COATED OPTICS). HEREIN WE PROPOSE TO BUILD A COMPASS PROTOTYPE (ALONG WITH SEVERAL NARROW-BAND FILTERS SAMPLES) AND EXECUTE A TECHNOLOGY MATURATION PLAN VIA A SERIES OF RIGOROUS TESTS AND PHOTOMETRIC EVALUATIONS IN RELEVANT THERMAL/VACUUM LAUNCH VIBRATION AND PRELAUNCH HUMIDITY ENVIRONMENTS. IN DOING SO WE WILL BRING THE INTEGRATED COMPASS PROTOTYPE TO A TRL 6 STATUS AT THE CONCLUSION OF 2 YEARS WITH SUFFICIENT SYSTEM ENGINEERING SAFETY AND MISSION ASSURANCE DOCUMENTATION TO SATISFY FULL READINESS FOR OPERATIONAL CUBESAT MISSION INTEGRATION. $70.8k 9/12/17