Table 13. Percentage Weighting for Sample of 1186 Launches ter Last Last 100 Last200 Last 300 I i:st 500 Point Ra nstant Point Points Points Points Points Last:Fir 0.999 0.14 13.7 26.1 37.3 56.7 3.3 0.996 0.40 33.3 55.6 70.6 87.3 1.2 X 1()2 0.995 0.50 39.5 63.5 78.0 92.1 3.8x 1()2 0.994 0.60 45.3 70.0 83.6 95.1 1.3x Hf 0.993 0.70 50.5 75.5 87.9 97.0 4.2 X l(f 0.992 0.80 55.2 79.9 91.0 98.2 1.4 X 104 0.991 0.90 59.5 83.6 93.4 98.9 4.5 X 104 0.990 1.00 63.4 86.6 95.1 99.3 1.5x Hf 0.980 2.00 86.7 · 98.2 99.8 99.996 3.9 X 1011 The value of F = 0.999 is considered inappropriate because, as seen in Table 13, the weighting factor applied to the most recent datum is only 3.3 times that applied to the oldest test result from 39 years ago. The most recent 200 and 300 points in the sample comprising 16.8% and 25.2% of the data receive only 26.1% and 37.3% of the total weight. This is not too different from equal weighting of data, which is appropriate only if the relative frequency of occurrence of each response mode has not changed significantly through the years. On the other hand, use of F = 0.99 effectively throws out the oldest 600 to 700 launches that are sorely needed for an adequate sample size. The results of the filtering process are given in Table 14 for failures during flight phases 0 - 2. Table 14. Response-Mode Occurrence Percentages Filter Respcnse Mode Factor 1 2 3 4 5 0.999 7.39 2.27 1.70 73.30 15.34 0.996 2.24 4.35 0.37 80.37 12.67 0.995 1.32 4.92 0.19 82.59 10.98 0.994 0.73 5.26 0.09 84.57 9.35 0.993 0.39 5.37 0.04 86.25 7.95 0.992 0.20 5.31 0.02 87.68 6.78 0.991 0.11 5.13 0.01 88.92 5.84 0.990 0.05 4.87 0.00 90.02 5.06 0.980 0.00 1.86 0.00 96.81 1.33 The results in Table 14 show that the percentages of occurrence for response-modes 2 and 4 are relatively insensitive to filter-factor values, while the percentages for Modes 1, 3, and 5 decrease as filter memory (filter factor) decreases. This suggests that occurrences of Modes 1, 3, and 5 have been decreasing over the years, while Modes 2 and 4 occurrences have not changed much. Although it cannot be argued convincingly 9/10/96 27 RTI
Vision Description (EN)
This is a page of technical text from a report, specifically section 6.1.4 regarding 'Malfunction-Turn Results for Atlas IIAS'. The text discusses atmospheric effects, vacuum calculations, and impact distributions for simulated random-attitude turns. There are no redactions or obscured areas on this page, which is fully legible.
Descrição Vision (PT-BR)
Esta é uma página de texto técnico de um relatório, especificamente a seção 6.1.4 referente a 'Malfunction-Turn Results for Atlas IIAS'. O texto discute efeitos atmosféricos, cálculos de vácuo e distribuições de impacto para curvas de atitude aleatória simuladas. Não há rasuras ou áreas obscurecidas nesta página, que está totalmente legível.