At the end of this module the student should understand the key physical parameters of the near-earth space environment and how these affect spacecraft design and operation. Topics will include: properties of the near-Earth space environment and interplanetary medium (i.e. solar wind, geomagnetic field, magnetosphere, ionosphere, thermosphere); basic plasma physics relevant to radio propagation; basic solar-terrestrial physics relevant to spacecraft charging and drag.
Learning Outcomes
By the end of the module students should be able to:
Demonstrate a comprehensive knowledge of the mathematical and scientific study of the space environment as applied to complex aspects of spacecraft design, critiquing current work and future developments (M1, R10).
Apply space environment standards to authentic mission element designs by formulation and problem analysis, accounting for available data and using judgement to address and discuss uncertain or incomplete information (M2).
Choose appropriate computational and analytical methods for simulating space environment effects, discussing technique limitations (M3).