An improved power and temperature control system for a rocket-borne space processing mirror furnace

Details An improved power and temperature control system for a rocket-borne space processing mirror furnace An improved power and temperature control system for a rocket-borne space processing mirror furnace

Jun 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980esasp.152..363g&link_type=abstract

In ESA European Rocket and Balloon Programs and Related Res. p 363-366 (SEE N81-10914 01-99)

Computer Science

Sound

Furnaces, Radiant Heating, Reduced Gravity, Space Processing, Temperature Control, Convective Heat Transfer, Mirrors, Sounding Rockets, Space Commercialization, Temperature Profiles

Scientific paper

Operational experience with the mirror furnaces flown in the Texus 1 and 2 rockets led to the development of an improved mirror furnace system for thermal analysis of small samples. The furnace operates in two basic modes: constant optical power and sample temperature profile mode. In the constant power mode the control system maintains the same light output from the halogen lamps in convective cooling of the filament in microgravity. In the temperature profile mode the temperature at the edge of the sample is used to control the furnace power.

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