|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||102/290 ; 102/272 ; 149/2 ; 149/57|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 0|
Propellant formulations are provided which include non-toxic burn rate modifiers. In order to produce a usable propellant formulation, it is necessary to control the burn rate of the propellant. Failure to adequately control the propellant burn rate often results in unacceptable performance of the propellant. For example, during the operation of a rocket motor, or similar device which contains a propellant, the propellant may produce operating pressures which are too high or too low for the intended purpose of the device. It has often been the practice t...
A solid propellant matrix having a non-toxic burn rate modifier, said burn rate modifier comprising bismuth trioxide.