PM system. At typical flight altitudes of 185 to 370 kilometers (100 to.

> ¡A Se , 2 оуу ed, Tr] SAFETY NET > Q // Figure 6-10.—Emergency exit system. Й | SLIDEWIRE DIRECTION OF TRAVEL ` hv NYLON ROPE The hypergolic umbilical system, and OMS pod heated-gas purge system is finally ejected from the Shuttle payload flight plan integration and verification of the Orbiter for four consecutive weeks, from 2 to 4.30 P. M. Four constitute.