In October 1994 a breadboard model of MicroMAPS was flown on the NASA Ames DC-8 research aircraft in a underflight of the MAPS which flew on STS68. Approximately 40,000 line km of CO and N2O measurements were made over a 10 day period over the US and southern Canada.
Data was both observed in real time and recorded digitally on the notebook computer data terminal hard disk during most of the MicroMAPS breadboard flight. The shell program that recorded the data also partially reduced the data so that cell ratio's could be observed. These ratios were recorded in a flight journal as a backup to the digitally recorded data. This "real time" feature made it was possible to evaluate the performance of the instrument in flight.
The flight observations of the changes in CO and N2O to clear cell ratios during ascent and descent validated the operation of the sensor and simulated the on-orbit detection of CO and N2O. In general, in-flight observations confirmed that the instrument was fully functional for 40,000 line km.
N2O channel CO channel
Signal ratio gas/clear Ref BB 0.82 0.685
Signal ratio gas/clear Atmospheric 1.00 0.815
Noise in ratio 0.012 0.012
DeltaS/S 0.22 0.187
Average at absn coef. used in model 2.1 atm/cm 2.5 atm/cm
Modulation Efficiency (estimated) 0.6 0.85
Column amount (atm-cm) 0.174 0.088
Column thickness 9.6 km 9.6 km
Average column density 0.65 std atm 0.65 std atm
Mixing Ratio from zero order model 280 ppb average 140 ppb average
Noise equivalent amount (NEA) 18 ppb 9 ppb
©Resonance Ltd. Aug '99