Radiation protection of astronauts in LEO.
Radiological protection for space flights is often perceived as a technico-scientific problem. All this is the result of the effects of radiation encountered in space and manned flight conditions. The main characteristics of this radiation come from its complex composition and its large energy spectrum which must be taken into account as well as flux variations by both solar activity and the vehicle position on orbit. Inside a vehicle, structures constitute irregularly distributed shields and lead to a specific dose at each location. To be able to protect the crew, it is first necessary to understand the threat and therefore to identify the radiation environment: extraterrestrial and orbital. As the environment varies with both the orbit position and time, the dose received in each critical organ during missions must be determined and compared with acceptable limits. To counter the threat, which may exceed acceptable limits, a strategy is required, including the complementary aspects of prevention, detection, protection and possibly treatment.
Melkonian
G
G
Avions Marcel Dassault-Breguet Aviation, Saint-Cloud, France.
Bourrieau
J
J
D001267:Atlantic Ocean; D003359:Cosmic Radiation; D004307:Dose-Response Relationship, Radiation; D004583:Electrons; D018478:Extravehicular Activity; D006801:Humans; D008280:Magnetics; D011522:Protons; D011829:Radiation Dosage; D011834:Radiation Monitoring; D011835:Radiation Protection; D012062:Relative Biological Effectiveness; D019445:Solar Activity; D013020:South America; D013026:Space Flight / Q000295:instrumentation*; D018531:Spacecraft / Q000295:instrumentation
D011522:Protons