Operability Benefits of Airbreathing Hypersonic Propulsion for Flexible Access to Space
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.43750
Reference25 articles.
1. Performance, Economic, and Operational Drivers of Reusable Launch Vehicles
2. Launch Vehicle Design Features for Minimum Cost
3. System robustness comparison of advanced space launch concepts
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