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Explorer: HESSI (RHESSI, Reuven Ramaty, SMEX 6)

HESSI (SMEX 6) [Spectrum Astro]

HESSI (High Energy Solar Spectroscopic Imager), renamed to RHESSI (Reuven Ramaty High Energy Solar Spectroscopic Imager) is intended to image at high resolution solar flares in X-rays and gamma rays.

The X-rays and gamma rays covers an energy range of 3 keV.- 20 MeV with an energy resolution of about one keV.and a spatial resolution of just a few seconds of arc. The imaging is accomplished by a 45 cm × 1.7 m tube containing nine pairs (one behind the other, spaced 1.5 m apart) of tungsten or molybdenum wire grids of width nine cm mounted parallel to the rotation axis of the tube pointing at the Sun. The tube rotates about its axis as the spacecraft spins at a rate of 15 rpm. During a rotation, a photon from any point on the Sun can either pass through a grid-pair or be blocked by one or other of the grids. This causes a modulation of the intensity of photons emanating from that point. The depth of modulation is zero for the photons arriving exactly along the spin axis and gradually increases to the off-axis photons. Behind each grid-pair is a cryogenic (75 K) germanium detector of 7.1 cm diameter and 8.5 cm thickness. The output from each of the nine detectors, at any given energy, can be Fourier-analyzed to provide a full two-dimensional spatial spectrum of an extended source region on the Sun. The full spatial spectrum is possible because each wire grid pair has a different slit width, spacing and wire thickness.

Data accumulaton is about 16 Gb during a 10-min rotation. The telemetry data will be collected at Berkeley (CA), Wallops (VA), Santiago (Chile) and Weilheim (Germany). Science analysis of the data will involve close collaboration with many dedictated ground based and satellite based solar observatories.

A secondary goal of HESSI is to observe astronomical sources such as Crab Nebula.

Nation: USA
Type / Application: Solar observatory
Operator: NASA
Contractors: Spectrum Astro
Equipment: X-ray and gamma-ray imaging spectrometer
Configuration: SA-200B (modified), spin stabilized
Propulsion: ?
Power: 4 deployable fixed solar arrays, batteries
Lifetime:
Mass: 304 kg
Orbit: 587 km × 600 km, 38
Satellite COSPAR Date LS Launch Vehicle Remarks
HESSI (RHESSI, Reuven Ramaty, SMEX 6, Explorer 81) 2002-004A 05.02.2002 CC, L-1011, RW13/31 Pegasus-XL

References:

  • NSSDC Master Catalog: RHESSI
  • Orbital Sciences Corp.: RHESSI