The various analyses described here were aimed at obtaining a more comprehensive understanding and definition of the environments in the vicinity of the Radioisotope Thermal Generator (RTG) during certain Space Transportation System (STS) and Titan IV launch abort accidents. Addressed here are a number of issues covering explosion environments and General Purpose Heat Source Radioisotope Thermoelectric Generator (GPHS-RTG) responses to those environments.
Summary of miscellaneous hazard environments for hypothetical Space Shuttle and Titan IV launch abort accidents
1989-12-01
Report
No indication
English
NTIS | 2011
|AIAA | 2011
|British Library Conference Proceedings | 2011
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