Effects of the rotational vehicle dynamics on the ascent flight trajectory of the SpaceLiner concept
Crossref DOI link: https://doi.org/10.1007/s12567-018-0223-7
Published Online: 2018-11-13
Published Print: 2019-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Krummen, Sven http://orcid.org/0000-0002-4126-688X
Sippel, Martin http://orcid.org/0000-0001-7356-7575
Text and Data Mining valid from 2018-11-13
Article History
Received: 28 February 2018
Revised: 13 August 2018
Accepted: 8 November 2018
First Online: 13 November 2018