Feasibility Study of Aerocapture at Mars with an Innovative Deployable Heat Shield-Reference-Cited by-同舟云学术

Feasibility Study of Aerocapture at Mars with an Innovative Deployable Heat Shield

Published:2021-11 Issue:6 Volume:58 Page:1752-1761
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Isoletta Giorgio¹^ORCID,Grassi Michele¹,Fantino Elena²,de la Torre Sangrà David³,Peláez Jesús⁴

Affiliation:

1. University of Naples “Federico II,” 80125 Naples, Italy

2. Khalifa University of Science and Technology, P.O. Box 127788, Abu Dhabi, United Arab Emirates

3. Polytechnic University of Catalonia (UPC), 08222 Terrassa, Spain

4. Technical University of Madrid (UPM), 28040 Madrid, Spain

Funder

Khalifa University of Science, Technology and Research

Università degli Studi di Napoli Federico II

Ministerio de Economía, Industria y Competitividad, Gobierno de España

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A35016

Reference29 articles.

1. Qualitative Assessment of Aerocapture and Applications to Future Missions

2. WrightH. S.OhD. Y.WesthelleC. H.FisherJ. L.DykeR. E.EdquistK. T.BrownJ. L.JusthH. L.MunkM. M. “Mars Aerocapture Systems Study,” NASA TM-2006-214522, 2006.

3. Survey of Ballute Technology for Aerocapture

4. A survey of aeroassisted orbit transfer

5. Cost-Benefit Analysis of the Aerocapture Mission Set

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