| Autor: |
Charles R. McClinton, Sharon S. Welch, Charles E. Cockrell, R. Wayne Guy, Aaron H. Auslender |
| Rok vydání: |
2002 |
| Předmět: |
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| Zdroj: |
AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference. |
| DOI: |
10.2514/6.2002-5188 |
| Popis: |
Third-generation reusable launch vehicle (RLV) systems are envisioned that utilize airbreathing and combined-cycle propulsion to take advantage of potential performance benefits over conventional rocket propulsion and address goals of reducing the cost and enhancing the safety of systems to reach earth orbit. The dual-mode scramjet (DMSJ) forms the core of combined-cycle or combination-cycle propulsion systems for single-stage-to-orbit (SSTO) vehicles and provides most of the orbital ascent energy. These concepts are also relevant to two-stage-to-orbit (TSTO) systems with an airbreathing first or second stage. Foundation technology investments in scramjet propulsion are driven by the goal to develop efficient Mach 3-15 concepts with sufficient performance and operability to meet operational system goals. A brief historical review of NASA scramjet development is presented along with a summary of current technology efforts and a proposed roadmap. The technology addresses hydrogen-fueled combustor development, hypervelocity scramjets, multi-speed flowpath performance and operability, propulsion-airframe integration, and analysis and diagnostic tools. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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