Page 100 - Intro to Space Sciences Spacecraft Applications
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                                                              Spacecraft Environment
                        Sunspots  seem  to  occur  only  around  mid-solar  latitudes,  between
                      around 60” north and south of the equator, forming closer to the equator
                      as the cycle approaches minimum. A reversal of the magnetic polarity of
                      the sun, from positive to negative lines of magnetic flux emanating from
                      the geographical poles, occurs over each solar cycle. This variability in
                      intensity, location, and magnetic polarity over time manifests itself in a
                      changing and difficult-to-predict environment in the vicinity of the earth.

                                                 THE EARTH

                        The environment on and around the earth is affected in many ways by
                      the electromagnetic and particulate radiations from the  sun. Spacecraft
                      must operate in and through the resulting environment, which includes the
                      earth itself and its atmosphere as well as the space around it. Consequent-
                      ly, the following sections describe some of the properties of the earth as
                      well as the interaction of the earth with the solar radiations.


                      Electromagnetic Interaction

                        We  previously  determined the amount of  electromagnetic energy that
                      reaches the vicinity of the earth when we calculated the solar constant. This
                      energy retains the blackbody spectral characteristics it had when it left the
                      sun, the  only difference being  that  the  energy levels over the range of
                      wavelengths has decreased. As this energy encounters the earth, the inter-
                      actions affect both the earth and the energy itself. In some cases, these
                      interactions are useful to the space systems user. For example, remote sens-
                      ing techniques measure the absorption or transmission of solar radiation
                      through the atmosphere to infer some of the characteristics of the atmos-
                      phere from space, and most spacecraft use solar panels to convert some of
                      this radiation to electricity to power the spacecraft systems. In other cases,
                      solar radiations produce undesired effects. For instance, spacecraft may
                      absorb excess infrared frequencies, necessitating the use of thermal control
                      devices, and the ionosphere, described next, may introduce errors in trans-
                      mitted signals. Spacecraft systems, including power generation and ther-
                      mal control, and spacecraft applications, such as remote sensing and com-
                      munications, are described more thoroughly later in the text.


                      The Ionosphere. The short wavelength (X-ray, UV) radiations from the sun
                      have enough energy to “knock” electrons out of some of the constituents of
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