Power plants – Reaction motor – Liquid oxidizer
Reexamination Certificate
2005-06-07
2005-06-07
Tyler, Cheryl (Department: 3746)
Power plants
Reaction motor
Liquid oxidizer
C060S770000, C060S200100, C239S265130
Reexamination Certificate
active
06901740
ABSTRACT:
The pointed end of a central spike, used in an engine of a space launcher, may have a deformable structure that can adopt either a folded position or a deployed position.
REFERENCES:
patent: 2828603 (1958-04-01), Laucher
patent: 3346186 (1967-10-01), Fulton et al.
patent: 3482783 (1969-12-01), Nebiker et al.
patent: 3596465 (1971-08-01), Paine et al.
patent: 3711027 (1973-01-01), Carey
patent: 4109867 (1978-08-01), Ebeling, Jr.
patent: 4162040 (1979-07-01), Carey
patent: 4213566 (1980-07-01), Miltenberger
patent: 4349155 (1982-09-01), Donguy
patent: 4383407 (1983-05-01), Inman
patent: 4387564 (1983-06-01), Carey
patent: 4480437 (1984-11-01), Gauge
patent: 4489889 (1984-12-01), Inman
patent: 5048289 (1991-09-01), Brown
patent: 5282576 (1994-02-01), Chatenet et al.
patent: 5640844 (1997-06-01), Pahl
patent: 6205772 (2001-03-01), Perrier et al.
patent: 6418710 (2002-07-01), Perrier et al.
patent: 6691505 (2004-02-01), Harvey et al.
patent: 2003/0136128 (2003-07-01), Groeber et al.
patent: 0018300 (1980-10-01), None
patent: 1460610 (1966-03-01), None
patent: 2422831 (1979-11-01), None
patent: 2013787 (1979-08-01), None
M. Calabro J.B. Perie, M.T. Prodhomme, EADS Launch Vehicles, Les Mureaux, France, AIAA 2001-3692. “Innovative Upper Stage Propulsion Concepts For Future Launchers,” 37thAIAA/ASME/SAE/ASEE JPC Conference & Exhibit, Jul. 8-11, 2001—Salt Lake City, Utah, pp. 1-9.
G. Hagemann, et al.; “Advanced Rocket Nozzles,” Journal of Propulsion and Power, American Institute of Aeronautics and Astronautics, New York, US, vol. 14, No. 5, Sep. 1, 1998, pp. 620-634, XP000778443, ISBN: 0748-4658.
Eads Launch Vehicles
Rodriguez William H.
Stevens Davis Miller & Mosher LLP
Tyler Cheryl
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