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URL: https://daac.ornl.gov/ATOM/guides/ATom_MMS_Instrument_Data_Fig1.png
MMS instrumentation on the DC-8 aircraft during the fourth field campaign in the NASA Convection and Moisture Experiment (CAMEX) series. The MMS Air Motion Sensor System consists of sensors that measure airflow angles such as angle of attack (AOA) and yaw angle, total and static pressure (P_total, Ps), and slow and fast temperature responses (T_fast, T_slow). The fast temperature probe location has been modified recently. The inset picture shows the rear rack with the Data Acquisition System (DAS) and Inertial Navigation System (INS).
Source: ATom: Measurements from Meteorological Measurement System (MMS), 2016-2018
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