Spacecraft are generally protected from a direct strike by launch the vehicle and ground structures, but protocols to evaluate the impact of nearby strikes are not consistent. Often spacecraft rely on the launch vehicle constraints to trigger a retest, but launch vehicles can typically evaluate the impact of a strike within minutes while spacecraft evaluation times can be on the order of hours or even days. For launches at the Kennedy Space Center where lightning activity is among the highest in the United States, this evaluation related delay could be costly with the possibility of missing the launch window altogether. This paper evaluated available data from local lightning measurements systems and computer simulations to predict the coupled effect from various nearby strikes onto a typical payload umbilical. Recommendations are provided to reduce the typical trigger criteria and costly delays.
Investigation on Improvements in Lightning Retest Criteria for Spacecraft
2016
6 pages
Report
Keine Angabe
Englisch
Retest of Refrigerant Container
SAE Technical Papers | 1998
Retest of Refrigerant Container
SAE Technical Papers | 2023
Retest of Refrigerant Container
SAE Technical Papers | 2012
RETEST OF REFRIGERANT CONTAINER
SAE Technical Papers | 1996