IN the design of long range aircraft, the high percentage weight of fuel carried lias always tended to necessitate the provision of a system by means of which this fuel could be rapidly jettisoned, in the event of forced landing or continued flight on partial power. The provision of such a jettison system is now an important problem in ancillary design.
Brennan, M.J. (1941), "Performance of a Jettison System: An Investigation of the Hydraulic Performance, in which the Importance of Adequate Venting is Stressed", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 9, pp. 247-250. https://doi.org/10.1108/eb030819Download as .RIS
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