Direct transfer trajectory design options for...

Advances in Space Research 2017 / 04 Vol. 59; Iss. 7

Direct transfer trajectory design options for interplanetary orbiter missions using an iterative patched conic method

Parvathi, S.P., Ramanan, R.V.
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Volume:
59
Language:
english
Journal:
Advances in Space Research
DOI:
10.1016/j.asr.2017.01.023
Date:
April, 2017
File:
PDF, 723 KB
english, 2017
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