The Viking Mars landers to be launched in 1975 will carry experiments in biology, planetology, and atmospheric physics. A terminal dry-heat sterilization process using an inert gas was chosen to meet planetary quarantine requirements and preclude contamination of the biology experiment by terrestrial organisms. Deep sterilization is performed at the component level and terminal surface sterilization at the system level. Solutions to certain component problems relating to sterilization are discussed, involving the gyroscope, tape recorder, battery, electronic circuitry, and outgassing. Heat treatment placed special requirements on electronic packaging, including fastener preload monitoring and solder joints. Chemical and physical testing of nonmetallic materials was performed to establish data on their behavior in heat-treatment and vacuum environments. A Thermal Effects Test Model and a Proof Test Capsule were used. It is concluded that a space vehicle can be designed and fabricated to withstand heat sterilization requirements.
Viking heat sterilization - Progress and problems
International Astronautical Federation, International Astronautical Congress ; 1974 ; Amsterdam, Netherlands
1974-09-01
Conference paper
No indication
English
Viking. viking flying boat V-2
Engineering Index Backfile | 1929
NTRS | 1975
NTIS | 1979
|NTRS | 1979
|Online Contents | 2006