Manned and robotic missions to the Earth's moon and Mars are exposed to a continuous flux of Galactic Cosmic Rays (GCR) and occasional, but intense, fluxes of Solar Energetic Particles (SEP). These natural radiations impose hazards to manned exploration, but also present some constraints to the design of robotic missions. The hazards to interplanetary flight crews and their uncertainties have been studied recently by a National Research Council Committee (Space Studies Board 1996). Considering the present uncertainty estimates, thick spacecraft shielding would be needed for manned missions, some of which could be accomplished with onboard equipment and expendables. For manned and robotic missions, the effects of radiation on electronics, sensors, and controls require special consideration in spacecraft design. This paper describes the GCR and SEP particle fluxes, secondary particles behind shielding, uncertainties in radiobiological effects and their impact on manned spacecraft design, as well as the major effects on spacecraft equipment. The principal calculational tools and considerations to mitigate the radiation effects are discussed, and work in progress to reduce uncertainties is included.
Radiation effects and protection for moon and Mars missions
1998
13 Seiten, 43 Quellen
Conference paper
English
Optimal Free-Return Trajectories for Moon Missions and Mars Missions
Springer Verlag | 2000
|Optimal Free-Return Trajectories for Moon Missions and Mars Missions
Online Contents | 2000
|Optimal Free-Return Trajectories for Moon Missions and Mars Missions
British Library Conference Proceedings | 2000
|