Catalyst, gas generator, and thruster with improved thermal capability and corrosion resistance
作者： Silvano R. Saretto , Junli Liu , Robert K. Masse
DOI:
关键词:
摘要: A catalyst includes a carrier of essentially hafnia, up to an equal part zirconia, and optionally additional stabilizers, upon the surface which is deposited active metal suitable promote reaction propellants be used in gas generators thrusters.
lens.org 参考文章(18)
Walter J. Sherwood, Qionghua Shen, Silicon carbide precursors and uses thereof ,(2006)
Paul L. Darby, Paul B. Weill, Liquid monopropellant compositions ,(1967)
Kurt F. Mueller, Manfred J. Cziesla, Monopropellant aqueous hydroxyl ammonium nitrate/fuel ,(1969)
David F. Gavin, Eckart W. Schmidt, Catalytic decomposition of hydroxylammonium nitrate-based monopropellants ,(1993)
James E. Torkelson, Mark D. Fokema, Thermally Stable Catalyst and Process for the Decomposition of Liquid Propellants ,(2006)
Ryo Minoguchi, Eiichiro Yoshikawa, Akihiko Tanaka, Eri Oishi, Makoto Iwasaki, Akihiko Kuroiwa, Yuji Ito, Eishi Sato, Kenjiro Ikeda, Airbag explosive composition and process for producing said composition ,(1996)
David R. Schryer, Bradley D. Leighty, Donald M. Oglesby, Anthony Neal Watkins, Jacqueline L. Schryer, Patricia P. Davis, Jeffrey D. Jordan, Methodology for the effective stabilization of tin-oxide-based oxidation/reduction catalysts ,(2002)
Hiroaki Nishio, Hot isostatic pressing method ,(1990)
Robert S. Scheffee, Norman H. Lundstrom, James D. Martin, Premixed liquid monopropellant solutions and mixtures ,(2000)