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Table I. Maximum deceleration, stabilization, and recovery opening loads allowable on aircrewmember |
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|  MIL-S-18471G(AS)
Maximum deceleration, stabilization, and recovery opening loads
TABLE I.
allowable on aircrewmember.
1/ Resultant loads shall be obtained as the vector sum of time-variant loads
measured along each of the three axes defined in figure 5. Maximum
resultant loadings shall be calculated as specified in the appendix.
2/ Maximum allowable loading applies to the aircrewmember population range
specified in 3.2.1.1 and wearing full personal flight gear.
30
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