Recent Advances in Gossamer Spacecraft

Chapter 6: Thermal Measurement Techniques

Joseph R. Blandino [*] and Jonathan J. Miles [ ]
James Madison University, Harrisonburg, Virginia

Copyright 2005 by the authors. Published by American Institute of Aeronautics and Astronautics, Inc., with permission.

Nomenclature

  • A element = area of a sail element

  • C = heat capacity

  • c = specific heat

  • E b = blackbody radiation per unit area

  • G = irradiance per unit area

  • K = thermal conductance

  • P = photon flux

  • Q = total heat

  • = radiant heat flux per unit area

  • = radiosity

  • R sun = solar radius

  • r = distance from Sun

  • T = temperature of object or membrane

  • T ? = temperature of background space

  • z element = thickness of the sail membrane for an element

  • ? = density

  • ? = absorptance

  • ? = emittance

  • ? 1 = sail Sun-facing side emittance

  • ? 2 = sail shadowed side emittance

  • ? ? = membrane emittance at a specific angle

  • ? ? = total membrane emissivity at a specific angle

  • ? = percent of radiant energy absorbed by detector

  • ? = incident angle for radiation

  • ? = wavelength

  • ? = reflectance

  • ? = Stefan Boltzman constant

  • ? = transmittance

  • = pitch angle of sail element with respect to solar vector

  • ? = roll angle of sail element with respect to solar vector

[*]Associate Professor, Integrated Science and Technology.

[ ]Professor, Integrated Science and Technology.

I.

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