Rocket Powered Flight as a Perturbation to the Two-Body Problem.
The two body problem and the rocket equation r̈ + ∊ α ṙ + k/r3r = 0 have been expressed in numerous ways. However, the combination of the rocket equation with the two-body problem has not been studied to any degree of depth due to the intractability of the resulting non-linear, non-homogeneous equ...
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Digital Commons @ East Tennessee State University
2005
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| Online Access: | https://dc.etsu.edu/etd/1045 https://dc.etsu.edu/cgi/viewcontent.cgi?article=2202&context=etd |