Rocket containing lead oxidizer salt-high density propellant

Details Rocket containing lead oxidizer salt-high density propellant Rocket containing lead oxidizer salt-high density propellant

1973-11-05

1976-03-23

Padgett, Benjamin R.

Power plants

Reaction motor

Solid propellant

60 3947, 149 191, 149 193, 149 196, 149 199, 149 45, 149 83, C06D 506

Patent

active

039452026

ABSTRACT:
A propellant including a binder, a curative for the binder (whenever necessary), an oxidizer and a fuel additive are provided. The oxidizer has a relatively high value of specific gravity or density and is stable even at relatively high temperatures and is capable of supplying relatively high amounts of oxygen to the fuel additives or the reducing agents in the propulsion material. The propellant provides density-impulses greater than the density-impulses provided by the propellants of the prior art.

REFERENCES:
patent: 2970898 (1961-02-01), Fox
patent: 3046168 (1962-07-01), Burkardt et al.
patent: 3152027 (1964-10-01), Godsey
patent: 3257801 (1966-06-01), Martinez et al.
patent: 3418184 (1968-12-01), Vetter
patent: 3601053 (1971-08-01), Grall et al.
patent: 3617403 (1971-11-01), Johnson
patent: 3625155 (1971-12-01), Douda et al.
patent: 3673287 (1972-06-01), Thies et al.
patent: 3677840 (1972-07-01), Shaw et al.
patent: 3765177 (1973-10-01), Ritchey et al.

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