Lake Michigan Launchers Black Brant II
DOI:
https://doi.org/10.17307/wsc.v1i1.190Abstract
The objective of the 2015-2016 Collegiate Rocket Launch aimed to model and scale a historical rocket no longer in use. The Lake Michigan Launchers chose to model the Black Brant II and used a J class motor in order for the rocket to propel between 2500’ and 3500’. The construction of the rocket itself and the prediction of apogee depending on wind speed and temperature were the two most vital parts of the research. We aimed to have a successful flight along with an accurate prediction on the day of the launch using precise construction techniques and accurate predictions of the highest altitude the Black Brant II will fly.
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Published
2017-01-17
How to Cite
Kasper, M., Abbott, A., Lee, N., Haag, J., & Krueger, B. (2017). Lake Michigan Launchers Black Brant II. Proceedings of the Wisconsin Space Conference, 1(1). https://doi.org/10.17307/wsc.v1i1.190
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Team Projects
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This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.