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Dispersion development programThe requirement for the predictable dispersion of small munitions over large areas from ground support missile systems has resulted in the development of a fin stabilized submissile and sling ejection system for the Little John warhead. The progressive development of this system is traced including a comparison of simulator, sled test, and flight test results. The results indicate that it is not only necessary but also possible to eject long slender bodies, from a missile warhead at Mach 1, in a stable, uniform and predictable manner.
Document ID
19760012097
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlson, D. J.
(Chrysler Corp. Detroit, MI, United States)
Lusardi, R. J.
(Chrysler Corp. Detroit, MI, United States)
Phillips, W. H.
(Chrysler Corp. Detroit, MI, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Kennedy Space Center 9th Aerospace Mech. Symp.
Subject Category
General
Accession Number
76N19185
Funding Number(s)
CONTRACT_GRANT: DAAA21-72-C-0030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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