hardware improvements that have taken place through the years. For samples approaching 100 or so, it seriously over-weights the old data and under-weights the more recent events. Although equal weighting does not seem suitable for this application, it could be appropriate in other large-sample situations, for example, predicting the failure probability of devices that are all manufactured at the same time by the same process, and tested to the same standards. Table 4. Comparison of Weicllting Percentages Sample Last+ Last5 Last 10 Last 25 !Last 50 Last Size Filter* Point Points Points Points Points Half 4 Expon. 25.8 - - - - 51.0 Index 40.0 - - - - 70.0 Equal 25.0 - - - - 50.0 10 Expon. 10.9 52.5 100.0 - - 52.5 Index 18.2 72.7 100.0 - - 72.5 Equal 10.0 50.0 100.0 - - 50.0 20 Expon. 6.0 28.9 55.0 - - 55.0 Index 9.5 42.9 73.8 - - 73.8 Equal 5.0 25.0 50.0 - - 50.0 100 Expon. · 2.3 11.1 21.1 45.7 73.3 73.3 Index 2.0 9.7 18.9 43.6 74.8 74.8 Equal 1.0 5.0 10.0 25.0 50.0 50.0 200 Expon. 2.0 9.8 18.6 40.4 64.7 88.3 Index 1.0 4.9 9.7 23.4 43.7 74.9 Equal 0.5 2.5 5.0 12.5 25.0 50.0 500 Expon. 2.0 9.6 18.3 39.7 63.6 99.4 Index 0.4 2.0 4.0 9.7 19.0 75.0 Equal 0.2 1.0 2.0 5.0 10.0 50.0 1000 Expon. 2.0 9.6 18.3 39.7 63.6 99.996 Index 0.1 1.0 2.0 4.9 9.7 75.0 Equal 0.1 0.5 1.0 2.5 5.0 50.0 * F = 0.98 for exponential filter + "Last" refers to the most recent data point The index-count filter has serious deficiencies when applied to either small or large samples of missiles and space vehicles. For small samples, too much emphasis is placed on recent data. For a sample of four, 40% of the total weight is given to the last test, and 70% to the last two tests. For a sample of ten, 18.2% of the total weight is given to the last test and 72.7% to the last five tests. The reliability improvement rate implied by these weightings seems too optimistic unless there were serious design flaws in the early configurations that were discovered and corrected. Since many types of failures surely exist that occur only once in 50 or once in 100 or more launches, the tenth launch may be no better than the first for predicting the probability of occurrence of such failures. For large samples, the index-count filter under-weights current data 9/10/96 19 RTI
Vision Description (EN)
Page 25 contains four statistical tables presenting failure data for multiple missile/launch vehicle systems: Atlas (532 flights), Delta (232 flights), Titan (337 flights), and Eastern-Range Ther (85 flights). Each table is organized by flight phase (rows 0 through 0-5) and failure-response mode (columns 1-5, N/A, and Tumble). Tables present numerical counts of failures in each category. No classification markings, redactions, signatures, or illustrative elements are visible. Document footer shows date 9/10/96 and report identifier RTI.
Descrição Vision (PT-BR)
A página 25 contém quatro tabelas estatísticas apresentando dados de falhas para múltiplos sistemas de mísseis/veículos lançadores: Atlas (532 voos), Delta (232 voos), Titan (337 voos) e Eastern-Range Ther (85 voos). Cada tabela é organizada por fase de voo (linhas 0 a 0-5) e modo de resposta a falhas (colunas 1-5, N/A e Tumble). As tabelas apresentam contagens numéricas de falhas em cada categoria. Nenhuma marcação de classificação, redações, assinaturas ou elementos ilustrativos são visíveis. O rodapé do documento mostra a data 9/10/96 e o identificador de relatório RTI.