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Dynamics Explorer 1

NSSDCA/COSPAR ID: 1981-070A

Description

The Dynamics Explorer (DE) mission's general objective is to investigate the strong interactive processes coupling the hot, tenuous, convecting plasmas of the magnetosphere and the cooler, denser plasmas and gases corotating in the earth's ionosphere, upper atmosphere, and plasmasphere. Two satellites, DE 1 and DE 2, were launched together and were placed in polar coplanar orbits, permitting simultaneous measurements at high and low altitudes in the same field-line region. The DE 1 spacecraft (high-altitude mission) uses an elliptical orbit selected to allow (1) measurements extending from the hot magnetospheric plasma through the plasmasphere to the cool ionosphere; (2) global auroral imaging, wave measurements in the heart of the magnetosphere, and crossing of auroral field lines at several earth radii; and (3) measurements for significant periods along a magnetic field flux tube. The spacecraft approximated a short polygon 137 cm in diameter and 115 cm high. The antennas in the X-Y plane measured 200-m tip-to-tip, and on the Z-axis are 9 meters tip-to-tip. Two six-meter booms are provided for remote measurements. Power is supplied by a solar cell array, mounted on the side and end panels. The spacecraft is spin stabilized, with the spin axis normal to the orbital plane, and the spin rate at ten plus or minus 0.1 rpm. A pulse code modulation (PCM) telemetry data system is used that operates in real time or in a tape-recorder mode. Data have been acquired on a science-problem-oriented basis, with closely coordinated operations of the various instruments, both satellites, and supportive experiments. Data acquired from the instruments are temporarily stored on tape recorders before transmission at an 8:1 playback-to-record ratio. Additional operational flexibility allows a playback-to-record ratio of 4:1. The primary data rate is 16,384 bits per second. Since commands are stored in a command memory unit, spacecraft operations are not real time, except for the transmission of the wideband analog data from the Plasma Wave Instrument (81-070A-02). On October 22, 1990 science operations were terminated. On February 28, 1991 Dynamics Explorer 1 operations were offically terminated. Additional details may be found in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981.

Alternate Names

  • DE-A
  • DE 1
  • Dynamics Explorer-A
  • Explorer 62
  • 12624

Facts in Brief

Launch Date: 1981-08-03
Launch Vehicle: Delta
Launch Site: Vandenberg AFB, United States
Mass: 424.0 kg
Nominal Power: 86.0 W

Funding Agency

  • NASA-Office of Space Science Applications (United States)

Discipline

  • Space Physics

Additional Information

Questions or comments about this spacecraft can be directed to: Dr. Dieter K. Bilitza.

 

Personnel

NameRoleOriginal AffiliationE-mail
Dr. Michael A. CalabreseProgram ManagerNASA Headquartersmcalabre@pop100.gsfc.nasa.gov
Dr. Robert A. HoffmanProject ScientistNASA Goddard Space Flight Centerrhoffman@pop600.gsfc.nasa.gov
Dr. Mary M. MellottProgram ScientistNASA Headquartersmary.m.mellott@nasa.gov
Mr. Paul J. PashbyProject ManagerNASA Goddard Space Flight Center 

Other DE 1 Data/Information at NSSDCA

CDAWeb (Browse and retrieve DE in CDAW)

Related Data/Information at NSSDCA

Dynamics Explorer 2

Other Sources of DE 1 Data/Information

General DE page (Los Alamos)

PWI page (U. Iowa) Access to data
SAI page (U. Iowa) Access to data
RIMS page (NASA/MSFC) Access to data
EICS page (Lockheed-Martin) Access to data

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