Temporal Variation of Earth Thermal Environmental Parameters for Spacecraft at Low Inclination Orbits

932196

07/01/1993

Event
International Conference On Environmental Systems
Authors Abstract
Content
The temporal variation of Earth emitted infrared radiation (IR) and albedo are examined for the case of a spacecraft operating in a Space Station Freedom (SSF)-like orbit with a period of 94 minutes and an inclination 28.75°. Seventy three randomly selected days of daily average Earth IR and albedo measurements from the Earth Radiation Budget Experiment were used to calculate the effective IR and albedo constants for the Earth during representative orbits. The time average effective IR and albedo extreme values, including a correction for diurnal effects, are presented for multiple periods of up to 4 hours. The statistical variation of IR and albedo over various time intervals is also presented, as are the results of a study of the correlation between IR and albedo. The results of the present study are used to recommend the design environments that should be used for future spacecraft in orbits with inclination and altitude similar to SSF.
Meta TagsDetails
DOI
https://doi.org/10.4271/932196
Pages
13
Citation
Farner, D., Ungar, E., and Elzey, C., "Temporal Variation of Earth Thermal Environmental Parameters for Spacecraft at Low Inclination Orbits," SAE Technical Paper 932196, 1993, https://doi.org/10.4271/932196.
Additional Details
Publisher
Published
Jul 1, 1993
Product Code
932196
Content Type
Technical Paper
Language
English