Planetary quarantine analyses performed for recent unmanned Mars and Venus missions assumed that the probability of contamination by a spacecraft given accidental impact was equivalent to one. However, in the case of the gaseous outer planets, the heat generated during the inadvertent entry of a spacecraft into the planetary atmosphere might be sufficient to cause significant microbial burden reduction. This could affect navigation strategy by reducing the necessity for biasing the aim point away from the planets. An effort has been underway to develop the tools necessary to predict temperature histories for a typical spacecraft during inadvertent entry. In order that the results have general applicability, parametric analyses were performed. The thermal response of the spacecraft components and debris resulting from disintegration was determined. The temperature histories of small particles and composite materials, such as thermal blankets and an antenna, were given special attention. Guidelines are given to indicate the types of components and debris most likely to contain viable organisms, which could contaminate the lower layers of the Jovian atmosphere (approximately one atmosphere of pressure).
Spacecraft microbial burden reduction due to atmospheric entry heating: Jupiter
Joint Open Meeting of the Panel on Planetary Quarantine and Working Group 5 ; 1973 ; Konstanz, Germany
1973-06-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Atmospheric entry into Jupiter
AIAA | 1969
|Atmospheric entry into Jupiter
AIAA | 1968
|A Jupiter atmospheric entry mission
AIAA | 1971
|