2020 IEEE 7th International Workshop on Metrology for AeroSpace (MetroAeroSpace) 2020
DOI: 10.1109/metroaerospace48742.2020.9160063
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GreenCube: microgreens cultivation and growth monitoring on-board a 3U CubeSat

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Cited by 10 publications
(6 citation statements)
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“…The agricultural and horticultural microgreen plant requires specific temperatures and humidity for production in closed and open systems. Temperature and humidity of 30–33 °C, 75–80% for rice grass, 15–32 °C, 80–85% for barley grass, 16–27 °C, 75–80% for oat grass, 23–28 °C, 60–70% for wheat grass, 29–32 °C, 30% for jowar grass, 25–34 °C, 52–88% for maize grass, 10–21 °C, 8–80% for buckwheat, 21–26 °C, 14–16% for chickpea, 18–21 °C, 50–60% for mint, 17–27 °C, 60–70% for coriander, 21 °C, 50–60% for basil, 24–29 °C, 75% for rosemary, 32 °C, 95–100% for parsley, 9.2–23.8 °C, 50–100% for saltwort, 21 °C, 50–70% for shisho, −1.11 °C, 50–75% for sorrel, 18–23 °C, 60–70% for sage, 18–23 °C, 40–60% for beet, 15–24 °C, 50–70% for chard, 24–26 °C, 11–96% for quinoa, 22–26 °C, 100% for spinach, 33–36 °C, 80% for chives, 32–50 °C, 65–75% for garlic, 18–23 °C, 95–100% for leek, 55–75 °C, 40–50% for onion, 15–21 °C, 60–70% for carrot, 14–26 °C, 90–95% for celery, 16–18 °C, 58–63% for dill, 60–70 °C, 50–65% for fennel, 10–29 °C, 50–60% for radish, 15–17 °C, 50–60% for aster cress, 15–21 °C, 76% for mustard, 7.2–29.4 °C, 55–65% for kale, 25–30 °C, 40–70% for kohlrabi, 7.2–18 °C, 90–95% for arugula, 25 °C day/23 °C night, 60% for sunflower, 25–34 °C, 50–60% for linseed, 23–25 °C, 90–95% for chicory, 15–18 °C, 95–98% for endive, 20 °C, 80% for lettuce, 15–21 °C, 40–50% for beans, 12–25 °C, 40–50% for welsh onion, 12–25 °C, 40–50% for long green onion, and 23–32 °C, 90–95% for red swiss chard are required for microgreen plant production.…”
Section: Factors Affecting In Microgreen Plant Production In Soilless...mentioning
confidence: 99%
“…The agricultural and horticultural microgreen plant requires specific temperatures and humidity for production in closed and open systems. Temperature and humidity of 30–33 °C, 75–80% for rice grass, 15–32 °C, 80–85% for barley grass, 16–27 °C, 75–80% for oat grass, 23–28 °C, 60–70% for wheat grass, 29–32 °C, 30% for jowar grass, 25–34 °C, 52–88% for maize grass, 10–21 °C, 8–80% for buckwheat, 21–26 °C, 14–16% for chickpea, 18–21 °C, 50–60% for mint, 17–27 °C, 60–70% for coriander, 21 °C, 50–60% for basil, 24–29 °C, 75% for rosemary, 32 °C, 95–100% for parsley, 9.2–23.8 °C, 50–100% for saltwort, 21 °C, 50–70% for shisho, −1.11 °C, 50–75% for sorrel, 18–23 °C, 60–70% for sage, 18–23 °C, 40–60% for beet, 15–24 °C, 50–70% for chard, 24–26 °C, 11–96% for quinoa, 22–26 °C, 100% for spinach, 33–36 °C, 80% for chives, 32–50 °C, 65–75% for garlic, 18–23 °C, 95–100% for leek, 55–75 °C, 40–50% for onion, 15–21 °C, 60–70% for carrot, 14–26 °C, 90–95% for celery, 16–18 °C, 58–63% for dill, 60–70 °C, 50–65% for fennel, 10–29 °C, 50–60% for radish, 15–17 °C, 50–60% for aster cress, 15–21 °C, 76% for mustard, 7.2–29.4 °C, 55–65% for kale, 25–30 °C, 40–70% for kohlrabi, 7.2–18 °C, 90–95% for arugula, 25 °C day/23 °C night, 60% for sunflower, 25–34 °C, 50–60% for linseed, 23–25 °C, 90–95% for chicory, 15–18 °C, 95–98% for endive, 20 °C, 80% for lettuce, 15–21 °C, 40–50% for beans, 12–25 °C, 40–50% for welsh onion, 12–25 °C, 40–50% for long green onion, and 23–32 °C, 90–95% for red swiss chard are required for microgreen plant production.…”
Section: Factors Affecting In Microgreen Plant Production In Soilless...mentioning
confidence: 99%
“…Here we note the trade-offs with the tight volume and power stores on board. Smaller satellite modules can get technologies off the ground to advance TRL [52][53][54] , but feature even greater size handicaps, and may prevent testing at the integrated, factory level in the DBTL cycle 55,56 . Scientific instruments and modules on rovers have been geared primarily for exploration and observation, not technology validation.…”
Section: Development Of Means For Sbe Flightmentioning
confidence: 99%
“…As a result, many university CubeSat teams opt to implement a protoflight model (PFM) philosophy whereby a single model is produced and flown after it has been subjected to protoflight qualification and acceptance test campaigns. Typically these projects rely on significant flight heritage or a robust CubeSat bus so that the associated risk is accepted [43,48,49]. In the case of EIRSAT-1, the increased risk of the PFM approach was not deemed acceptable due to the lack of experience among the team.…”
Section: Assembly Integration and Verification Of Eirsat-1mentioning
confidence: 99%