High solids ratio solid rocket motor propellant grains and metho

Plastic and nonmetallic article shaping or treating: processes – Explosive or propellant article shaping or treating – Forming or treating particulate material

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264 31, 102289, 102291, C06B 2100

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047643196

ABSTRACT:
A high acceleration high performance solid rocket motor grain such as for a ballistic defense missile or rocket assisted projectile comprises a propellant material which includes a highly plasticized binder so that the grain has a solids ratio equal to at least about 95 percent. In order that the grain with such a solids ratio may have adequate strength and withstand high acceleration forces, a reticulated structure is embedded therein. A method of constructing a rocket motor having such a grain is also disclosed.

REFERENCES:
patent: 2961710 (1960-11-01), Stark
patent: 2977885 (1961-04-01), Perry, Jr. et al.
patent: 3109374 (1963-11-01), Rumbel et al.
patent: 3109375 (1963-11-01), Rumbel et al.
patent: 3125542 (1964-03-01), Haines
patent: 3140663 (1964-07-01), Rumbel et al.
patent: 3163113 (1964-12-01), Davis et al.
patent: 3165483 (1965-01-01), Gemeinhardt et al.
patent: 3171820 (1965-03-01), Volz
patent: 3175025 (1965-03-01), Geen et al.
patent: 3175030 (1965-03-01), Geen
patent: 3191535 (1965-06-01), Mulloy
patent: 3230281 (1966-01-01), Carrez
patent: 3308210 (1967-03-01), Ross
patent: 3367268 (1968-02-01), Spenadel et al.
patent: 3389025 (1968-06-01), Nix et al.
patent: 3390210 (1968-06-01), Guenter
patent: 3499283 (1970-03-01), Simpkins
patent: 3616841 (1971-11-01), Walz
patent: 3664133 (1972-05-01), Iwanciow et al.
patent: 3678854 (1972-07-01), Davidson
patent: 3711115 (1973-01-01), Lohr
patent: 3756025 (1973-09-01), McCullogh
patent: 3764420 (1973-10-01), Sayles
patent: 3807171 (1974-04-01), Anderson
patent: 3811380 (1974-05-01), Glass
patent: 3822645 (1974-07-01), Alexander
patent: 3827715 (1974-08-01), Lynch
patent: 3829537 (1974-08-01), Rosenthal
patent: 3860678 (1975-01-01), Martin et al.
patent: 3897221 (1975-07-01), Salyer et al.
patent: 3925122 (1975-12-01), Berthmann et al.
patent: 3946039 (1976-03-01), Walz
patent: 3972545 (1976-08-01), Kirchoff et al.
patent: 4072546 (1978-02-01), Winer
patent: 4083905 (1978-04-01), Insley et al.
patent: 4085173 (1978-04-01), Lomax, Jr. et al.
patent: 4102953 (1978-07-01), Johnson et al.
patent: 4116466 (1978-09-01), Gehrig
patent: 4321220 (1982-03-01), Camp
patent: 4370181 (1983-01-01), Lundstrom et al.
patent: 4393014 (1983-07-01), Ziegler
patent: 4409155 (1983-10-01), Bonnycastle et al.
patent: 4418622 (1983-12-01), Foster et al.
patent: 4458595 (1984-07-01), Gerrish, Jr. et al.
patent: 4547342 (1985-10-01), Adams et al.
patent: 4660475 (1987-04-01), Rogowski et al.
Brochure, "Duocel, a New Basic Design Material", by Energy Research and Generation, Inc.
Technical Report AFRPL-TR-68-232, Dec., 1968, "Foamed Aluminum Propellant Study."
Brochure, "Duocel Foam Metal, a New Basic Design Material for Energy Absorption and Structural Applications", by Energy Research and Generation, Inc.
Brochure, "Duocel Foam Metal, a New Basic Design Material, Passive Omnidirectional Borehold Deformation Gauge", by Energy Research and Generation, Inc.
Brochure, "ERG Evolutionary Basic Design Materials", by Energy Research and Generation, Inc.
Brochure, "Reticulated Vitreous Carbon", by Energy Research and Generation, Inc.
"Scott, Chemotronics Get Reticulation Patents", C&EN, Jun. 7, 1965, p. 42.

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