Feasibility and Performance of Atmospheric-Breathing Propulsion for Mars Descent
| Autor: | Aaron H. Auslender, Robert D. Braun, Keir C. Gonyea |
|---|---|
| Rok vydání: | 2018 |
| Předmět: |
020301 aerospace & aeronautics
business.industry Aerospace Engineering 02 engineering and technology Thrust-to-weight ratio Mars Exploration Program Propulsion 01 natural sciences 010305 fluids & plasmas Propellant mass fraction 0203 mechanical engineering Payload fraction Space and Planetary Science 0103 physical sciences Environmental science Rocket engine Descent (aeronautics) Aerospace engineering business Propulsive efficiency |
| Zdroj: | Journal of Spacecraft and Rockets. 55:346-355 |
| ISSN: | 1533-6794 0022-4650 |
| DOI: | 10.2514/1.a33959 |
| Popis: | Analysis was performed to assess the impact of atmospheric-breathing supersonic retropropulsion as a technology solution for Mars descent. Vehicle models were developed for three architectures, emp... |
| Databáze: | OpenAIRE |
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