NSSDCA ID: 1975-096A-02
Mission Name: AE-DThe Miniature Electrostatic Analyzer (MESA) obtained data on the neutral density of the atmosphere in the altitude range of 120 to 400 km by the measurements of satellite deceleration due to aerodynamic drag. The instrument consisted of three single-axis accelerometers, mounted mutually at right angles, two in the spacecraft X-Y plane and the other in the Z-axis. The instrument determined the applied acceleration from the electrostatic force required to recenter a proof mass. The output of the device was a digital pulse rate proportional to the applied acceleration. The sample time of each measurement was 0.25 s. The measurements allowed determination of the density of the neutral atmosphere, monitored the thrust of the orbit-adjust propulsion system (OAPS), determined the satellite minimum altitude, measured spacecraft roll, and provided some attitude-sensing information. Spacecraft nutations of less than 0.01 deg were monitored. The instrument had three sensitivity ranges: 8.E-3 earth's gravity (G) in OAPS monitor mode; 4.E-4 G between 120 km (plus or minus 2%) and 280 km (plus or minus 10%); and 2.E-5 G between 180 km (plus or minus 2%) and 400 km (plus or minus 10%). Numbers in parentheses represent errors. A systematic error of up to plus or minus 5% due to drag coefficient uncertainty was also possible. The highest measurement altitude was determined assuming the instrument could sense to 0.2% of full scale. More details can be found in K. S. W. Champion et al., Radio Sci., v. 8, n. 4, p. 297, 1973. NSSDC has all the data that exist from this investigation.
Mass: 3.5 kg
Power (avg): 5 W
Questions and comments about this experiment can be directed to: Dr. Dieter K. Bilitza
Name | Role | Original Affiliation | |
---|---|---|---|
Mr. Frank A. Marcos | Other Investigator | Phillips Laboratory (nee USAF Geophysics Lab, nee Cambridge Labs) | |
Dr. Kenneth S. W. Champion | Principal Investigator | Phillips Laboratory (nee USAF Geophysics Lab, nee Cambridge Labs) |