Trisha Shetty

Dynamics Explorer

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Operator  NASA
SATCAT no.  12624
Rocket  Delta 3913 642/D155
Period  6.8 hours
Apogee  23.2463 million m
Manufacturer  RCA
COSPAR ID  1981-070A
Power  68 W
Inclination  89.959°
Launch mass  424 kg
Launch date  3 August 1981
Dynamics Explorer httpsuploadwikimediaorgwikipediacommons66
Mission type  Magnetospheric research
Similar  Fast Auroral Snapshot, IMAGE, ISEE‑1, Magsat, Student nitric oxide explorer

Dynamics Explorer was a NASA mission, launched on August 3, 1981 and terminated on February 28, 1991. It consisted of two unmanned satellites, DE-1 and DE-2, whose purpose was to investigate the interractions between plasmas in the magnetosphere and those in the ionosphere. The two satellites were launched together into polar coplanar orbits, which allowed them to simultaneously observe the upper and lower parts of the atmosphere.

Contents

Design

Both spacecraft had a polygonal shape, and were approximately 137 cm in diameter and 115 cm high. Each also had a 200-cm radio antenna and two 6-meter booms which were needed to distance some of the equipment from the main body of the spacecraft. They were stacked on top of each other and launched aboard a Delta 3000 booster rocket. Upon reaching orbit, the two spacecraft departed from the booster and entered separate orbits. Dynamics Explorer 1 was placed into a high altitude elliptical orbit, while DE-2 was put into a lower orbit that was also more circular.

Dynamics Explorer 1 Instrumentation

The main instrument aboard Dynamics Explorer 1 was the Plasma Wave Instrument (PWI). This instrument, designed and built by the Plasma Wave Group, measured auroral kilometric radiation, auroral hiss, Z-mode radiation, and narrow band electromagnetic emissions. Additional Instruments aboard the spacecraft included:

  • The Spin-scan Auroral Imager (SAI)
  • The Retarding Ion Mass Spectrometer (RIMS)
  • The Energetic Ion Mass Spectrometer (EIMS)
  • Dynamics Explorer 2 Instrumentation

    The Dynamics Explorer 2 carried the following instruments for data collection:

  • A Retarding Potential Analyzer, which measured the ion flux along the velocity vector of the spacecraft. This data was then used to determine the ion temperature and drift velocity in the spacecraft's area.
  • An Ion drift meter, which measured the ambient ion drift.
  • A Magnetometer
  • A Vector Electric Field Instrument
  • A Neutral Atmosphere Composition Spectrometer
  • A Wind and Temperature Spectrometer (WATS), which measured the zonal and vertical components of the neutral winds, as well as the kinetic temperature. (The zonal wind component is the component in the direction of lines of latitude - i.e., east-west.) The WATS instrument on DE-2 is one of the few satellite instruments which has measured thermosphere vertical wind speeds, with the Neutral Atmosphere Temperature Instrument (NATE) on Atmospheric Explorer C (AE-C) being one other.
  • A Fabry–Pérot interferometer (FPI), which measured the meridional component of the neutral winds. (The meridional wind component is the component in the direction of lines of longitude - i.e., north-south.)
  • A Low-Altitude Plasma Instrument
  • A Langmuir probe
  • Mission Results

    As a result of a malfunction in the Delta 3000 booster rocket in which its main engine shut off slightly early, DE-2 was placed into a slightly lower orbit than was anticipated. This was not a serious problem, however, and the spacecraft had lasted its expected lifespan when it re-entered the Earth's atmosphere on February 19, 1983. DE-1, being in a higher orbit, continued to collect data until 1991, when the mission was officially terminated.

    References

    Dynamics Explorer Wikipedia


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