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Spacecraft Environment
                                                                                    101
                      stations is affected by the atmosphere and ionosphere which also fluctu-
                      ate constantly.

                      Man in Space

                        All of the above situations must be considered when man is placed into
                      the space environment. In most cases, a suitable environment can be pro-
                      vided within a spacecraft or with the use of a space suit. However, humans
                      are particularly susceptible to high-energy particle radiations in the form
                      of cosmic rays (from distant stars and galaxies), the particles trapped in
                      the geomagnetic field, and those produced by solar flares. These particles
                      have the ability to pass through shielding and can produce cell damage to
                      astronauts, so exposure must be measured and limited. Fortunately, the
                      areas associated with commonly used nonpolar low-earth orbits have low
                      enough radiation levels to be relatively safe with simply a small amount
                      of protection.

                                     REFERENCEWADDITIONAL READING

                      National Aeronautics and Space Administration, Space  Physics Strate-
                        gy-  Implementation Study, 2nd ed. Washington: NASA, 199 1.
                      Interagency Group (Space), National Security Council, Report on Orbital
                        Debris. Washington: National Security Council, 1989.
                      T. Wilkerson, M. Lauriente, and G. Sharp (Eds.), Space Shuttle Environ-
                        ment. New York: Engineering Foundation, 1985.
                      C.  Cochran,  D.  Gorman,  and  J.  Dumoulin  (Eds.),  Space  Handbook.
                        Alabama: Air University Press, 1985.
                      Tascione, T., Introduction  to the Space Environment. Colorado Springs:
                        U.S. Air Force Academy, 1984.




                      1. Draw a graph showing the estimated temperature (T) and density (p)
                        variations of  the sun from 0 to 2 solar radii (R,) based on the informa-
                        tion given in the chapter. Use logarithmic scales for T and p and a lin-
                        ear scale for R,.

                      2. Starting with a value for the solar constant in the vicinity of the earth of
                        1,390 W/m2:
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