Hybrid Rocket Propulsion and In-Situ Propellant Production for Future Mars Missions-Reference-Cited by-同舟云学术

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Hybrid Rocket Propulsion and In-Situ Propellant Production for Future Mars Missions

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
Short-container-title:

Author:

Boiron Adrien J.¹,Cantwell Brian¹

Affiliation:

1. Stanford University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3899

Reference53 articles.

1. 1Hand,E."7minutesofterror.TheCuriosityroverpreparestoplungedowntoMars".1Aug.2012.Nature488,pp.16-17.

2. Feasibility of rocket propellant production on Mars

3. Development and testing of a vortex-driven, high-regression rate hybrid rocket engine

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1. Optimal battery selection for hybrid rocket engine;INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN SCIENCES AND ENGINEERING ICCMSE 2021;2022

2. Hybrid Propulsion System: Novel Propellant Design for Mars Ascent Vehicles;Propulsion - New Perspectives and Applications;2021-12-15

3. A Review of Metal Powder-CO₂ Propulsion Technology;2021 5th International Conference on Vision, Image and Signal Processing (ICVISP);2021-12

4. Propulsion System Design for Mars Ascent Vehicles by using the In-Situ CO2;AIAA Propulsion and Energy 2021 Forum;2021-07-28

5. Optimal Design of Electrically Fed Hybrid Mars Ascent Vehicle;Aerospace;2021-07-06

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