FIELD: rocket fuels.
SUBSTANCE: invention proposes composition for liquid single-base propellant including solution of (i) an oxidant of general formula X-D, wherein X represents cation selected from group consisting of (H2NOH)
EFFECT: reduced toxicity and improved safety in handling.
8 cl, 4 dwg, 2 tbl
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Authors
Dates
2005-01-20—Published
2000-02-23—Filed