FIELD: chemistry.
SUBSTANCE: invention relates to applied chemistry, specifically to solid fuel for ramjet engines of rocket projectiles. Solid fuel contains organic combustible binder, ultrafine powder of high-energy metal and carborane and/or phenyl carborane. Combustible binder in solid fuel is a mixture of epoxy resin, dibutylphthalate, curing agent and diamine diaoleate in certain ratio of components.
EFFECT: composition of solid fuel ensures preservation of integrity of gas-generating elements made therefrom under conditions of high overloads of rocket projectiles during shooting from gun and its operation by improving mechanical properties of solid fuel with simultaneous high power and other characteristics.
4 cl, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
COMPOSITION FOR SOLID FUEL | 2005 |
|
RU2288207C1 |
NANO-COMPONENT ENERGY SUPPLEMENT AND LIQUID HYDROCARBON FUEL | 2013 |
|
RU2529035C1 |
PASTE-LIKE FUEL COMPOSITION FOR RAMJET ENGINE | 2019 |
|
RU2732870C1 |
SOLID-PROPELLANT COMPOSITION BASED ON AMMONIA NITRATE | 2007 |
|
RU2363691C1 |
METHOD OF PRODUCING MIXED SOLID FUEL | 2008 |
|
RU2429282C2 |
AEROSOL-FORMING AND FLAME-ARRESTING COMPOSITION | 2006 |
|
RU2325204C1 |
METHOD FOR PRODUCING MIXED FIRM ROCKET FUEL | 2016 |
|
RU2621789C1 |
EPOXIDE COMPOSITION | 1999 |
|
RU2160291C1 |
METHOD OF CONTROLLING RATE OF COMBUSTION OF MIXED SOLID FUEL | 2008 |
|
RU2423338C2 |
ROCKET PROPELLANT | 2021 |
|
RU2761188C1 |
Authors
Dates
2016-11-10—Published
2015-07-07—Filed