Power plants – Reaction motor – Solid and fluid propellant
Reexamination Certificate
2011-06-28
2011-06-28
Kim, Ted (Department: 3741)
Power plants
Reaction motor
Solid and fluid propellant
C060S253000, C102S287000
Reexamination Certificate
active
07966809
ABSTRACT:
A hybrid rocket motor is formed from a single piece of material, such as, for example, by extrusion or injection molding. The rocket motor includes various components, such as casing, structure, oxidizer tank, combustion chamber, fuel, port and nozzle that are all formed from a single piece of material. The material can be, for example, a material that can be used as solid rocket fuel.
REFERENCES:
patent: 3032970 (1962-05-01), Fox
patent: 3280566 (1966-10-01), Larue
patent: 3298182 (1967-01-01), Webb
patent: 3354647 (1967-11-01), Aycock
patent: 3434426 (1969-03-01), De Dapper
patent: 3447326 (1969-06-01), Fuller
patent: 3507296 (1970-04-01), Fix et al.
patent: 3555824 (1971-01-01), Buse et al.
patent: 3715888 (1973-02-01), Massie
patent: 3812671 (1974-05-01), Burr et al.
patent: 4023355 (1977-05-01), McDonald
patent: 4424679 (1984-01-01), Holzman
patent: 4787202 (1988-11-01), Crapiz
patent: 4802333 (1989-02-01), Smith
patent: 4880185 (1989-11-01), Apfel
patent: 5026259 (1991-06-01), Whitehead et al.
patent: 5119627 (1992-06-01), Bradford et al.
patent: 5579636 (1996-12-01), Rosenfield
patent: 5582001 (1996-12-01), Bradford et al.
patent: 5694769 (1997-12-01), Akiba et al.
patent: 6016652 (2000-01-01), Smith et al.
patent: 6092366 (2000-07-01), Smith et al.
patent: 6354074 (2002-03-01), Jones et al.
patent: 6393830 (2002-05-01), Hamke et al.
patent: 6679047 (2004-01-01), Uematsu et al.
patent: 6880326 (2005-04-01), Karabeyoglu et al.
patent: 7069717 (2006-07-01), Macklin et al.
patent: 2002/0121081 (2002-09-01), Cesaroni et al.
patent: 2006/0064963 (2006-03-01), Macklin et al.
patent: 2006/0213181 (2006-09-01), Sarigul-Klijn et al.
Space Daily “Surrey fires micro electric thruster” Oct. 25, 1999 http://www.spacedaily.com
ews/microsat-99j.html.
Williams et al. “Almost There: Responsive Space” AIAA 2nd Responsive Space Conference 2004 RS2-2004-8000; Apr. 19-22, 2004; Los Angeles, CA.
Hernandez Fred C.
Kim Ted
Mintz Levin Cohn Ferris Glovsky and Popeo P.C.
Spacedev, Inc.
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