diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
index a71243f4..d13ff0dd 100755
--- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
+++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
@@ -1,10 +1,10 @@
 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale)
 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
-2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
-3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
-4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
-5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
+2,RT,BATT_V,12,V,cubesatsim_ina219_voltage | FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
+4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
+5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_racceleration | FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current
 7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature
 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X Panel
@@ -19,7 +19,7 @@
 17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel
 18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel
 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel
-20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage
+20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage | FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage
 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude