| http://www.w3.org/ns/prov#value | - In the drawing: FIGS. 1 and 2 are longitudinal sections of the improved rocket according to this invention, FIG. 1 showing the missile ready for the launching operation, and FIG. 2 the same missile at the end of the propellant combustion phase; and FIG. 3 is a section taken along the line III-III of FIG. 1.
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