49.140 Space systems and operations

Space systems Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages

Formula to obtain Ec by the product of the probability of impact on a specific latitude band, and the population within the band, which is integrated over the latitude range covered by the orbital inclination

Space systems — Re-entry risk management for uncrewed spacecraft and launch vehicle orbital stages

Space product assurance - Wire-wrapping of high-reliability electrical connections