Long life feasibility study for the shuttle infrared telescope facility

Physics – Optics

Scientific paper

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Space Infrared Telescope Facility, Spaceborne Experiments, Spaceborne Telescopes, Spacelab Payloads, Cryogenic Cooling, Cryogenic Equipment, Hydrogen, Long Duration Space Flight, Solid Cryogen Cooling, Spacelab

Scientific paper

A study was conducted to assess the feasibility of designing an Infrared Telescope of the 1 meter class which would operate effectively as a Shuttleborne, 14-day Spacelab payload and then be adapted with little modification to work as a 6 month Space station or free flyer payload. The optics configuration and requirements from a previous study were used without modification. In addition, an enhancement to 2 year mission lengths was studied. The cryogenic system selected was a hybrid design with an internal solid Hydrogen tank at 8 Kelvin and an internal superfluid tank at 2K. In addition to the cryogenic design, a detailed look at secondary mirror actuators for chopping, focus and decenter was conducted and analysis and cryo test reported.

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