Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation-Reference-Cited by-同舟云学术

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Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation

Published:2024-03 Issue: Volume:216 Page:488-503
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Yue^ORCID,Wang Yunpeng

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference56 articles.

1. SAENGER - the reference concept of the German hypersonics technology program;Weingertner,1993

2. Promising solutions for fully reusable two-stage-to-orbit configurations;Deneu;Acta Astronaut.,2005

3. Investigation of TSTO propulsion system options;McKinney,2006

4. Abort separation of launch escape system using aerodynamic interference;Wang;AIAA J.,2012

5. Numerical study on aerodynamic performance of Mars parachute models with geometric porosities;Jiang;Space: Sci. Technol.,2022

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