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The definition and specification of the near earth environmental criteria for spacecraft thermal design (1974)

Gary, G. A. ; Craven, P. D.

In: CASI

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Publication Date: 2019-06-27

Description: The variation of the earth's thermal and albedo radiation received by a near-earth orbiting space vehicle or space payload as a result of temporal variation of the earth atmosphere is discussed. A statistical study of current satellite data for determining probability distributions is proposed. With these distributions the thermal designer can define confidence levels on predicted temperature ranges which are compatible with engineering models for use in design, failure probabilities, and spacecraft cost estimates. Use of the distributions in environmental criteria guidelines is also considered.

Keywords: SPACE VEHICLES

Type: NASA-TM-X-64870

Format: application/pdf

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