Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Shelly M. Ferlemann"'
Publikováno v:
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.
The successful Mach 7 flight test of the Hyper-X (X-43) research vehicle has provided the major, essential demonstration of the capability of the airframe integrated scramjet engine. This flight was a crucial first step toward realizing the potential
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c870ac76ae7786cce4d121dcd45c2759
https://doi.org/10.2514/6.2005-3322
https://doi.org/10.2514/6.2005-3322
Publikováno v:
40th AIAA Aerospace Sciences Meeting & Exhibit.
Hypersonic airbreathing engine (scramjet) powered vehicles are being considered to replace conventional rocket-powered launch systems. Effective utilization of scramjet engines requires careful integration with the air vehicle. This integration syner
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d4c0548fbbc65ec8ebf3516b345e2c7
https://doi.org/10.2514/6.2002-543
https://doi.org/10.2514/6.2002-543
Autor:
Lawrence W. Taylor, Shelly M. Ferlemann, Jeffrey S. Robinson, Charles P. Leonard, John G. Martin, Hilmi Kamhawi
Publikováno v:
21st Aerodynamic Measurement Technology and Ground Testing Conference.
Designing a hypersonic vehicle is a complicated process due to the multi-disciplinary synergy that is required. The greatest challenge involves propulsion-airframe integration. In the past, a two-dimensional flowpath was generated based on the engine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::030f474bd606eef05f807a5d27b1ab25
https://doi.org/10.2514/6.2000-2694
https://doi.org/10.2514/6.2000-2694
Autor:
Dennis H. Petley, R F Vause, Jeffrey S. Robinson, P L Moses, J L Hunt, Shelly M. Ferlemann, K A Bouchard, Iii L. W. Taylor, S Z Pinckney, Charles P. Leonard, John G. Martin
Publikováno v:
9th International Space Planes and Hypersonic Systems and Technologies Conference.
Airbreathing launch vehicles continue to be a subject of great interest in the space access community. In particular, horizontal takeoff and horizontal landing vehicles are attractive with their airplane-like benefits and flexibility for future space
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e8816808f0669df5ecae0d93b3a62e2
https://doi.org/10.2514/6.1999-4948
https://doi.org/10.2514/6.1999-4948