## Spacecraft temperature control by thermostatic fins-analysis, Part 2 |

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70 Solar 90 Solar Polar A F _ a/b ratio adjacent thermostatic analysis angle of inclination assumed average value Ax^l Ax2r base material base surface Btu/hr-ft Calculation of Effective characteristics cos0 effective reflectance curve Effective Reflectance Ratio emittance energy which leaves equation fin length fin material fin top fraction is designated fraction of energy groove heat flux inch finned incoming radiation infinitely long Invar Length of base low expansion side monochromatic effective reflectance NASA Pairs of fins radiosity reaches the opening reflected from Ax0 shown in Figures slit angles slit formed solar absorptance solar irradiation Solar Polar Angle specular wall static material surface area surface base section surface element surface temperature thermo thermostat elements Thermostat Surface Thermostatic Fin Surface thermostatic strip thickness uniform temperature variation vertical position view factor virtual image wavelength white base white paint x x xT y y