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• W4320485322 abstract "<strong class=journal-contentHeaderColor>Abstract.</strong> The instrumentation of the High Altitude and Long Range (HALO) research aircraft is extended by the new Broadband AirCrAft RaDiometer Instrumentation (BACARDI) to quantify the radiative energy budget. Two sets of pyranometers and pyrgeometers are mounted to measure upward and downward solar (0.3–3 <span class=inline-formula>µ</span>m) and thermal–infrared (3–100 <span class=inline-formula>µ</span>m) irradiances. The radiometers are installed in a passively ventilated fairing to reduce the effects of the dynamic environment, e.g., fast changes in altitude and temperature. The remaining thermal effects range up to 20 W m<span class=inline-formula>^−2</span> for the pyranometers and 10 W m<span class=inline-formula>^−2</span> for the pyrgeometers. Using data collected by BACARDI during a night flight, it is demonstrated that the dynamic components of the offsets can be parameterized by the rate of change of the radiometer sensor temperatures, providing a greatly simplifying correction of the dynamic thermal effects. The parameterization provides a linear correction function (200–500 W m<span class=inline-formula>^−2</span> K<span class=inline-formula>^−1</span> s) that depends on the radiometer type and the mounting position of the radiometer on HALO. Furthermore, BACARDI measurements from the EUREC<span class=inline-formula>⁴</span>A (Elucidating the Role of Clouds—Circulation Coupling in Climate) field campaign are analyzed to characterize the performance of the radiometers and to evaluate all corrections applied in the data processing. Vertical profiles of irradiance measurements up to 10 km altitude show that the thermal offset correction limits the bias due to temperature changes to values below 10 W m<span class=inline-formula>^−2</span>. Measurements with BACARDI during horizontal, circular flight patterns in cloud-free conditions demonstrate that the common geometric attitude correction of the solar downward irradiance provides reliable measurements in this typical flight section of EUREC<span class=inline-formula>⁴</span>A, even without active stabilization of the radiometer." @default.
• W4320485322 created "2023-02-14" @default.
• W4320485322 creator A5006746842 @default.
• W4320485322 date "2023-02-13" @default.
• W4320485322 modified "2023-10-18" @default.
• W4320485322 title "Reply on RC1" @default.
• W4320485322 doi "https://doi.org/10.5194/amt-2022-259-ac1" @default.
• W4320485322 hasPublicationYear "2023" @default.
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