Vehicle-Level Oxygen/Methane Propulsion System Hotfire Demonstration at Thermal Vacuum Conditions
Author:
Affiliation:
1. NASA Johnson Space Center
2. NASA Kennedy Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4748
Reference16 articles.
1. Integrated Pressure-Fed Liquid Oxygen / Methane Propulsion Systems - Morpheus Experience, MARE, and Future Applications
2. Propulsion Risk Reduction Activities for Non-Toxic Cryogenic Propulsion
3. Nontoxic Orbital Maneuvering and Reaction Control Systems for Reusable Spacecraft
4. International Space Exploration Coordination Group Assessment of Technology Gaps for LOx/Methane Propulsion Systems for the Global Exploration Roadmap
5. Project Morpheus: Lander Technology Development
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