96. Weight and Balance Problems of “”Zero Length”” Launching
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Paper
Abstract
The introduction, in 1947, of the idea of ‘zero length’ launching in connection with the Matador missile presented some novel engineering problems-and the Weight Group received its full share. The solutions to these problems represent a first attempt on our part, and do not attempt to constitute final answers.
It is hoped, nevertheless, that this discussion may prove informative to those who already face these problems-and serve to alert those who have yet to encounter them. Certainly, these problems will arise again and again as surface-launched missiles become more common. Designers of conventional aircraft too, will be encouraged to consider zero length launching-as a means for eliminating the need for take-off runways
