TL;DR: In this article, the effects of the space radiation environment on spacecraft systems and instruments are significant design considerations for space missions Astronaut exposure is a serious concern for manned missions and the radiation environment must be understood and accurately modeled.
Abstract: The effects of the space radiation environment on spacecraft systems and instruments are significant design considerations for space missions Astronaut exposure is a serious concern for manned missions In order to meet these challenges and have reliable, cost-effective designs, the radiation environment must be understood and accurately modeled The nature of the environment varies greatly between low earth orbits and higher earth orbits There are both short-term and long-term variations with the phase of the solar cycle In this paper we concentrate mainly on charged particle radiations in the near-Earth region Descriptions of the radiation belts and particles of solar and cosmic origin are reviewed An overview of the traditional models is presented accompanied by their application areas and limitations This is followed by discussion of some recent model developments
TL;DR: In this paper, the authors present a concise and up-to-date study of the mathematical formulation needed to understand and quantify the motion of a satellite in the atmosphere and its effect on its motion.
Abstract: Nearly all of the satellites now in orbit
feel the effects of atmosphere drag. This
book, written by a highly respected
author with a lifetime's experience in
space research, presents a concise and
up-to-date study of the mathematical
formulation needed to understand and
specify their motion. The early
chapters develop the theory, first for a
spherical atmosphere, then for various
more realistic models, e.g. an oblate
atmosphere or one with density varying
between day and night. Two later
chapters show how to apply the theory
in analysing the orbits of real satellites
to determine air density, winds and
other atmospheric parameters. Practical
methods are presented for predicting
the lifetimes of satellites, and the theory
is also applied to orbits about Mars and
Venus.
This book will be of special interest to
lecturers, postgraduates and researchers
in applied mathematics, applied
physics, space research, geophysics and
aerospace.
Contents
Introduction. The atmosphere and its
action on a satellite. Basic theory.
Orbital theory for a spherically
symmetrical, exponential atmosphere.
Orbital theory for an oblate, exponential
atmosphere. Orbital theory when
atmospheric scale height varies with
altitude. Orbital theory for an
atmosphere with day-to-night density
variation. Effect of atmospheric rotation
on the orientation of the orbital plane.
Extensions and alternatives. Adaptation
of the theory for use in atmospheric
research. The theory in action.
Predicting satellite lifetimes. Orbits
about Mars and Venus. Appendix: The
Earth's gravitational field. References.
Further reading. Index.