|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 7 인용 특허 : 3|
This invention relates to novel nitramine propellant compositions for gunsnd rockets.
1. A propellant composition, which comprises a particulate organic nitramine propellant and an effective amount for burn rate acceleration of a metal tetrahydridoborohydride of the following formula: Me(BH 4 ) x, wherein Me represents an alkali metal or an alkaline earth metal and x is 1 when Me is an alkali metal and x is 2 when Me is an alkaline earth metal. 2. A propellant composition according to claim 1, wherein the metal tetrahydridoborohydride is present in amount up to about 20% by weight of the nitramine compound. 3. A propellant composition acc...