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TRACE
TRACE
TRACE
Credit: Manufacturer Image
American solar satellite. TRACE, carried a 30-cm extreme ultraviolet imaging telescope for studies of the sun. Lockheed was the lead contractor while the Smithsonian Astrophysical Observatory made the telescope mirrors. Solar observatory satellite built by NASA Goddard Space Flight Center for NASA, USA. Launched 1998.

Status: Operational 1998. First Launch: 1998-04-02. Last Launch: 1998-04-02. Number: 1 . Gross mass: 213 kg (469 lb).

TRACE had a field of view of 8.5 arcmin and a resolution of 1 arcsecond. TRACE was placed in a sun-synchronous orbit, enabling it to make continuous observation of the sun.

NASA NSSDC Master Catalog Description

The Transition Region and Coronal Explorer (TRACE) is a NASA small explorer mission designed to examine the three-dimensional magnetic structures which emerge through the Sun's photosphere (the visible surface of the Sun) and define both the geometry and dynamics of the upper solar atmosphere (the transition region and corona). Its primary science objectives are to: (1) follow the evolution of magnetic field structures from the solar interior to the corona; (2) investigate the mechanisms of the heating of the outer solar atmosphere; and, (3) determine the triggers and onset of solar flares and mass ejections. TRACE is a single-instrument, three-axis stabilized spacecraft. The spacecraft attitude control system (ACS) utilizes three magnetic-torquer coils, a digital sun sensor, six coarse sun sensors, a three-axis magnetometer, four reaction wheels, and three two-axis inertial gyros to maintain pointing. In science mode the spacecraft uses an instrument-provided guide telescope as a fine guidance sensor to provide a pointing accuracy of less than 5 arc-seconds. Power is provided to the spacecraft through the use of four panels of Ga-As solar cells with a total area of 2.0 square-meters. The solar array actually produces power of around 220 W, 85 W of which is used each orbit by the spacecraft and 35 W of which is used by the instrument each orbit. The remaining power is used for operational and decontamination heating of the spacecraft and telescope. A 9 A-hour Ni-Cd battery provides energy during time when the spacecraft is in the Earth's shadow. Communications are provided via a 5 W S-band transponder, providing up to 2.25 Mbps downlink data transmission and 2 kbps uplink. Data are transmitted up to six times daily. Data are stored on-board using a solid-state recorder capable of holding up to 300 MB. The command and data handling system uses a 32-bit 80386/80387 processor.


More at: TRACE.

Family: Astronomy, Solar, Sun synchronous orbit. Country: USA. Launch Vehicles: Pegasus, Pegasus XL. Projects: Small Explorer. Launch Sites: Point Arguello WADZ. Agency: NASA Greenbelt, Lockheed. Bibliography: 2, 4183, 6992, 13288.

1998 April 2 - . 02:42 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Vandenberg.. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL.
  • TRACE - . Nation: USA. Agency: NASA Greenbelt. Program: Small Explorer. Class: Astronomy. Type: Solar satellite. Spacecraft: TRACE. USAF Sat Cat: 25280 . COSPAR: 1998-020A. Apogee: 652 km (405 mi). Perigee: 602 km (374 mi). Inclination: 97.8000 deg. Period: 97.10 min.

    NASA's third Small Explorer, the Transition Region and Coronal Explorer (TRACE), was successfully launched by an Orbital Pegasus XL. The L-1011 carrier aircraft took off from Vandenberg and dropped the Pegasus over the Pacific Ocean. TRACE, a project led by Lockheed's solar physics group, carried a 30-cm extreme ultraviolet imaging telescope which will study the Sun. The telescope mirrors were made by the Smithsonian Astrophysical Observatory. TRACE had an 8.5 arcmin field of view and 1 arcsecond resolution. Air dropped in Point Arguello WADZ.



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