Official name IRIS (ESRO 2B)
Alternative name Iris (ESRO 2)
Cospar ID 1968-041A
Norad ID 3233
Launch date 1968-05-17
Launch site AFWTR
Launch vehicle Scout-B
Country/Organization Europe
Type application Research, cosmic radiation and solar astronomy
Operator ESRO
RCS size UNKNOWN
Decay date 1971-05-08
Shape Cyl
Mass (kg) 74
Diameter (m) 0.76
Height (m) 0.85
Span (m^2) 0.85
Contractors Hawker Siddely Dynamics, Matra
Equipment see above
Propulsion ?
Power Solar cells, batteries

ESRO 2 (European Space Research Organisation), Iris (International Radiation Investigation Satellite) was a 75 kg spin-stabilized spacecraft On the launch of ESRO 2A, the third stage vehicle failed and the spacecraft did not achieve orbit. ESRO 2B was launched on 16 May 1968, into a near polar orbit. The main objective of ESRO 2 was to conduct a study of solar astronomy and cosmic rays. The ESRO 2 experiments had their counterparts in the NASA-OSO series. The purpose of the spacecraft was to provide continuity to the solar radiation observations carried out by OSO D launched 18 October 1967. The particle experiments were designed to continue similar measurements carried out by the Ariel 1 (UK 1) satellite.

Experiments on board were:

  • Monitor of Energetic Particle Flux
  • Solar and Van Allen Belt Protons
  • Solar and Galactic Alpha Particles and Protons
  • Primary Cosmic Ray Electrons
  • Hard Solar X-rays
  • Soft Solar X-rays
  • Flux and Energy Spectra of Solar and Galactic Cosmic Ray Particles

The satellite had a spin rate of about 40 rpm and had completed 16,282 orbits of the earth before reentry on 8 May 1971, shortly after 0300 UT. No playback data has been available since 10 December 1968, following a mechanical failure of the onboard tape recorder. The failure reduced the data flow by about 80 percent, although a combination of Estrack (ESRO) and STADAN (NASA) tracking stations were used.

Satellite COSPAR Date LS Launch Vehicle Remarks
IRIS (ESRO 2B) 1968-041A 1968-05-17 AFWTR Scout-B