Explosive and thermic compositions or charges – Structure or arrangement of component or product
Reexamination Certificate
2006-04-04
2006-04-04
Felton, Aileen (Department: 3641)
Explosive and thermic compositions or charges
Structure or arrangement of component or product
C149S017000, C149S045000
Reexamination Certificate
active
07022196
ABSTRACT:
An oxidizer package for use in a solid fuel propellant system. The oxidizer package comprises a solid oxidizer in the form of discrete pellets of predetermined geometric shape. The pellets are arranged in an array with spaces amongst the pellets. A holder is provided for maintaining the pellets in the array for receipt of a binder introduced to spaces amongst the array of pellets. Preferred propellants include hydrazinium nitroformate and nitronium perchlorate. This arrangement for the pellets can achieve loadings as high as 85% by weight for the pellets.
REFERENCES:
patent: 3183665 (1965-05-01), Webb
patent: 3316718 (1967-05-01), Webb
patent: 3429265 (1969-02-01), Longwell et al.
patent: 3522334 (1970-07-01), Bieber et al.
patent: 3527168 (1970-09-01), McCurdy et al.
patent: 3811380 (1974-05-01), Glass
patent: 3812671 (1974-05-01), Burr et al.
patent: 3995559 (1976-12-01), Bice et al.
patent: 4781117 (1988-11-01), Garnett et al.
patent: 4950341 (1990-08-01), Schoyer et al.
patent: 5010728 (1991-04-01), Joy
patent: 5351619 (1994-10-01), Chan et al.
patent: 5579635 (1996-12-01), Miskelly, Jr. et al.
patent: 5714711 (1998-02-01), Schumacher et al.
patent: 5847311 (1998-12-01), Ryder
patent: 6354218 (2002-03-01), Weise et al.
patent: 6647888 (2003-11-01), Cesaroni et al.
Cesaroni Anthony J.
Dennett Michael J.
Louwers Jeroen
Alston & Bird LLP
Cesaroni Technology Incorporated
Felton Aileen
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