Initial particle ejection behaviours due to a hypersonic jet impingement at different high-nozzle pressure ratios in rarefied atmospheric conditions-Reference-Cited by-同舟云学术

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Initial particle ejection behaviours due to a hypersonic jet impingement at different high-nozzle pressure ratios in rarefied atmospheric conditions

Published:2024-09 Issue: Volume:222 Page:126-135
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ukai Takahiro^ORCID,Subramanian Senthilkumar^ORCID,Wilson Andrew^ORCID,Craig Bradley^ORCID,Kontis Konstantinos

Funder

Japan Society for the Promotion of Science

Publisher

Elsevier BV

Reference41 articles.

1. Apollo Lunar Descent and Ascent Trajectory;Bennett,1970

2. Mars InSight entry, descent, and landing trajectory and atmosphere reconstruction;Karlgaard;J. Spacecraft Rockets,2021

3. "Mars Science Laboratory: Entry, Descent, and Landing System Performance," 2007 IEEE Aerospace Conference, Big Sky, MT, USA;Way,2007

4. Cratering and blowing soil by rocket engines during Lunar landings;Metzger;Conf. Proc 18th Int. Conf Case Histories Geotech. Eng,2008

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