Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Todd Neill"'
Autor:
Christophe Bonhomme, Robert Starke, Walter Zinner, Scott Forde, Patrick Alliot, Todd Neill, Christophe Rothmund, Alain Souchier, Masahiro Atsumi, Randy Parsley, Mamoru Takahashi, Dominique Valentian, Philippe Caisso, William W. Wang
Publikováno v:
Acta Astronautica. 65:1723-1737
Liquid-propellant rocket engines are widely used all over the world, thanks to their high performances, in particular high thrust-to-weight ratio. The present paper presents a general panorama of liquid propulsion as a contribution of the IAF Advance
Publikováno v:
Acta Astronautica. 65:696-705
Liquid methane has been considered an attractive rocket propellant for several decades. However, most rocket engine development efforts in the last 30 years have focused on using more traditional fuels such as hydrogen, kerosene, and earth storables,
Publikováno v:
Acta Astronautica. 59:271-277
Aerojet used the patented thrust augmented nozzle (TAN) concept to validate a unique means of increasing sea-level thrust in a liquid rocket booster engine. We have used knowledge gained from hypersonic Scramjet research to inject propellants into th
Publikováno v:
56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law.
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Autor:
Melvin J. Bulman, Todd Neill
Publikováno v:
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Autor:
Todd Neill, Jeffrey D. Gladstone
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
The development of low cost, highly reusable rocket thrusters is essential for fulfilling NASA's commitment of providing economical space access. Results obtained from a recent sub-scale, high performance rocket thruster development and test program