Imran Khan’s research while affiliated with University of California, Davis and other places

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Fig. 2 | Modified energy cascade model calculations. a MEC model total crop biomass per area, m ⌒ T (blue), and crop growth rate per area, _ m ⌒ B (orange), for (from top left) dry bean, lettuce, rice, soybean, tomato, wheat, peanut, sweet potato, and white potato with parameters Φ γ = 500 μmol γ m −2 s −1 , c CO2 = 1200 μmol CO2 mol À1 air .
Fig. 4 | Nitrogen Productivity Studies. a Measured areal biomass and MEC model curve calculated with Φ γ = 225 μmol γ m −2 s −1 and c CO2 = 525 ppm. b Measured fresh weight percentage of total nitrogen in plants over time. A single measurement was performed for each condition at 20 d AE . c Nitrogen productivity calculated from measured biomass and nitrogen content. Error bars represent propagated error. a-c Time range highlighted in gray is specified harvest time, t M , plus 5 d 11 . Error bars represent one SD. For each data point, 5 ≤ N ≤ 10. d-f Concentration and change in concentration of nitrogen measured in the NSS over time by experimental condition (deficient, normal, excess). Error bars represent 1 SD. N = 3 for each data point. g-i Photos of lettuce crops during main growth phase at 35 d AE grown in deficient, normal, and excess nitrogen conditions, respectively.
Fig. 5 | Lettuce model comparison. a Experimental data (circles) and NP model fits (lines) for lettuce biomass predicted by the MEC model and grown in 3 different nitrogen conditions. b Fitting of m N by values of r, K, and α to experimental mass of N in plant. c Fitting of _ Y N by functions for η N and μ N to nitrogen productivity calculated from experimental data. d Sensitivity analysis result based on the ranges defined by the fitting procedure. The y − axis denotes the variable of interest wile the x − axis represents the corresponding variable's index value. e Fitted NP parameter values for MEC baseline and experimental N conditions. r: governing rate in [d −1 ]; K: limiting value of m N in [g N ]; α: dimensionless scaling factor; η N : nitrogen use efficiency in [g DW g À1 N ]; μ N relative nitrogen accumulation rate in [d −1 ].
Fig. 6 | MEC and NP Model Projection Comparison. a NP model fits to MEC growth curves (Φ γ = 225 mol γ m −2 s −1 , c CO2 = 525 ppm) for dry bean, peanut, rice, soybean, sweet potato, tomato, wheat, white potato. b Sensitivity analysis result based on the ranges defined by the fitting procedure. The y − axis denotes the variable of interest wile the x − axis represents the corresponding variable's index value.
Nitrogen accountancy in space agriculture
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  • Full-text available

September 2024

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159 Reads

npj Microgravity

Kevin Yates

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Food production and pharmaceutical synthesis are posited as essential biotechnologies for facilitating human exploration beyond Earth. These technologies not only offer critical green space and food agency to astronauts but also promise to minimize mass and volume requirements through scalable, modular agriculture within closed-loop systems, offering an advantage over traditional bring-along strategies. Despite these benefits, the prevalent model for evaluating such systems exhibits significant limitations. It lacks comprehensive inventory and mass balance analyses for crop cultivation and life support, and fails to consider the complexities introduced by cultivating multiple crop varieties, which is crucial for enhancing food diversity and nutritional value. Here we expand space agriculture modeling to account for nitrogen dependence across an array of crops and demonstrate our model with experimental fitting of parameters. By adding nitrogen limitations, an extended model can account for potential interruptions in feedstock supply. Furthermore, sensitivity analysis was used to distill key consequential parameters that may be the focus of future experimental efforts.

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Nitrogen Accountancy in Space Agriculture

March 2024

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190 Reads

Food production and pharmaceutical synthesis are posited as essential biotechnologies for facilitating human exploration beyond Earth. These technologies not only offer critical green space and food agency to astronauts but also promise to minimize mass and volume requirements through scalable, modular agriculture within closed-loop systems, offering an advantage over traditional bring-along strategies. Despite these benefits, the prevalent model for evaluating such systems exhibits significant limitations. It lacks comprehensive inventory and mass balance analyses for crop cultivation and life support, and fails to consider the complexities introduced by cultivating multiple crop varieties, which is crucial for enhancing food diversity and nutritional value. Here we expand space agriculture modeling to account for nitrogen dependence across an array of crops and demonstrate our model with experimental fitting of parameters. By adding nitrogen limitations, an extended model can account for potential interruptions in feedstock supply. Furthermore, sensitivity analysis was used to distill key consequential parameters that may be the focus of future experimental efforts.