Zobrazeno 1 - 8
of 8
pro vyhledávání: '"John J. Rusek"'
Autor:
David J. Brodrecht, John J. Rusek
Publikováno v:
Applied Energy. 74:113-124
Swift has developed an Al–H2O2 semi fuel-cell (SFC) that uses a novel approach to increase the maximum power output of the cell. Pure, high surface area aluminum flakes, courtesy of Transmet Corporation of Columbus, Ohio, are compressed to form the
Autor:
Daniel N. Prater, John J. Rusek
Publikováno v:
Applied Energy. 74:135-140
At present, the use of hydrogen and oxygen gases is necessary to achieve a reasonable power density in fuel-cell systems. However, the overall energy density of a hydrogen/oxygen fuel cell system is low in comparison with many present, or alternate,
Autor:
John J. Rusek
Publikováno v:
Journal of Propulsion and Power. 18:810-813
A need has surfaced over the past several years for low-cost access to space. The two primary avenues for cost reduction are to lower propellant raw material costs and to lower processing costs. Thermoplastics and thermoplastic elastomers will help a
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Autor:
Stephen D. Heister, John J. Rusek
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Traditional education in rocket propulsion has largely relied on lecture presentations. This generally leads to a restricted background in the issues related to fabrication and testing for propulsion engineers produced by academia. These factors have
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A new type of catalyst system for use in decomposing hydrogen peroxide was studied. The catalyst system was composed of sodium permanganate loaded onto a cordierite-based ceramic material that had not previously been used in this manner. Both immersi
Autor:
John J. Rusek, Matthew R. Long
Publikováno v:
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Interest in Rocket Grade Hydrogen Peroxide (RGHP) has been renewed in recent years by the search for a non-toxic alternative to rocket propellents currently in use. Innovations have increased the efficiency of the utilization of energy obtained from
Publikováno v:
International Journal of Alternative Propulsion. 1:154
Combustion characteristics and fuel regression behaviour have been studied for two fuels utilising 98% rocket-grade hydrogen peroxide (RGHP) as oxidiser. Two test series (A and C) involved a total of 13 firings of dicyclopentadiene (DCPD) fuel grains