Engineering:TE-416 Tomahawk
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Revision as of 01:14, 1 June 2021 by imported>CodeMe (over-write)
The TE-416 Tomahawk is a rocket developed by the American company Thiokol at the beginning of the 1960s for Sandia National Laboratories. Although the TE-416 Tomahawk can be launched alone, it was started predominantly as upper stage in connection with other rockets, for example with a Nike rocket as first stage (Nike Tomahawk). The TE-416 Tomahawk has a thrust of 9,500 lbf (42 kN) and a burn time of 9.5 seconds.[1] The diameter of the TE-416 tomahawk is 9 inches (23 cm) and the fin span is 36 in (91 cm).
References
- ↑ "Tomahawk Sandia". Archived from the original on 2011-03-03. https://web.archive.org/web/20110303144252/http://www.astronautix.com/lvs/tomandia.htm.
External links
es:Misil Tomahawk
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