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Table 5 . Normal tolerance limit of amplification factor in logarithm of the dummy satellite in the range: 300-1000Hz (real values are shown in bracket). Amplification factor Perpendicular to the axial(x) Perpendicular to the axial(y) Axial direction (z) Average 0.39(2.4) 0.49(3.1) 0.14(1.4) Standard deviation 0.20(1.6) 0.28(3.1) 0.11(1.3) NTL (Min) 0.06(1.15) 0.02 (1.05) -0.04(0.91) NTL (Max) 0.72(5.25) 0.96 (9.12) 0.32(2.09)

transactions of the japan society for aeronautical and space sciences, aerospace technology japan

Erratum for “Laboratory Tests to Standardize Environment Test Conditions of Micro/Nano Satellite Units” [Trans. JSASS Aerospace Tech. Japan Vol. 12, No. ists29, pp. Pf_1-Pf_10, 2014]