摘要:
The invention is a solid double-base propellant composition comprising on a weight basis from about 5 to about 35 percent of a crystalline substantially non-solvated aluminum hydride, from about 20 to about 38 percent hydrazinium nitroformate and from about 30 to about 60 percent of a plasticized nitrocellulose binder.
摘要:
The present invention comprises a solid double-base propellant composition having on a weight basis from about 2 to about 23 percent of a light metal fuel, from about 14 to about 35 percent of a particulate solid oxidizer, from about 12 to about 35 percent triaminoguanidinium hydrazinium diazide and from about 30 to about 50 percent of a plasticized nitrocellulose binder.