A Preliminary Research on a Two-Stage-To-Orbit Vehicle with Airbreathing Pre-cooled Hypersonic Engines
Author:
Affiliation:
1. Beijing Aerospace Technology Institute
2. Beijing Power Machinery Research Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2343
Reference34 articles.
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3. SKYLON USERS' MANUALR1.1[R]. Reaction Engine, 2010-01.
4. Hellman B M, Bradford J, Germain B S, etal Two Stage to Orbit Conceptual Vehicle Designs using the SABRE Engine [R].AIAA2016-5320.
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