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• LoadTest2
  ...d of the spacecraft, the [[telescope baffle]] operates at 42.3 K and the [[telescope primary mirror]] operates at 35.9 K. The temperatures of key parts of the i
  42 KB (7,697 words) - 16:43, 4 October 2012
• The satellite
  ...rmal and radiative insulation between the warm service module and the cold telescope and instruments. |'''Angle between spin axis and telescope boresight'''
  14 KB (2,170 words) - 09:29, 21 May 2014
• Beams LFI
  where B = baffle', P = primary reflector, S = secondary reflector, F = focal plane unit box, ...eans that we considered in the calculation the reflection on the telescope baffle system.
  24 KB (3,748 words) - 10:02, 26 September 2016
• The satellite WiP
  ...rmal and radiative insulation between the warm service module and the cold telescope and instruments. |'''Angle between spin axis and telescope boresight'''
  14 KB (2,136 words) - 09:37, 3 February 2015