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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2021
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Article
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Tab 3
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Research Article
Design Optimization and Parameter Analysis of a Hybrid Rocket Motor-Powered Small LEO Launch Vehicle
Table 3
Approximation aerodynamic coefficients of the “Titan II” rocket.
Aerodynamic coefficients
Velocity range
Formula
0.29
2.8
3.55