Hot gas valve with fibrous monolith ceramic
作者： Don Mittendorf , Jason Gratton
DOI:
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摘要: A valve is disclosed for use in hot gas applications such as rocket or missile engine systems the like. The designed to withstand extreme temperatures encountered exhaust from propellants. seat of constructed fibrous monolith ceramic. This material does not degrade significantly when exhaust, resulting ammonium perchlorate propellant burned, ported through valve. generally includes a body, seat, which gases may pass, and poppet opens closes by pressing against moving away seat.
lens.org 参考文章(15)
Michael A. Wusterbarth, Thermal expansion reservoir ,(1986)
Howard G Cutforth, Method for making a rocket motor ,(1957)
Charles W. Dunmire, Short-length reduced-pressure backflow preventor ,(2001)
Manish P. Sutaria, Marlene Platero-AllRunner, Mark M. Opeka, Anthony C. Mulligan, Mark J. Rigali, E. Greg Hilmas, Composite components for use in high temperature applications ,(2001)
Vemulapalli Durga Nageswar Rao, Wallace Robert Wade, Filtration system for diesel engine exhaust-II ,(1984)
Michael L. Fulcher, Manish P. Sutaria, Anthony C. Mulligan, Mark J. Rigali, Randy C. Cook, Joseph P. Halloran, Dragan Popovich, Aligned composite structures for mitigation of impact damage and resistance to wear in dynamic environments ,(2002)
Schulz Helmut W, Hogsett John N, Albert Khuri, Adducts of metal borohydrides and organic polynitrogen compounds ,(1962)
Thomas O. Bales, Theodore C. Slack, Korey R. Kline, Kevin W. Smith, Propulsion system containing a mixed-phase propellant and a method for propelling an object with the same ,(1997)
N Bermender, Gas generator charge with decreased temperature sensitivity ,(1962)
Rolf K. Brodersen, Thrust vector control for large deflection angles ,(1981)