FIELD: propellants.
SUBSTANCE: invention relates to manufacturing solid rocket fuels operated in a wide temperature range and used in engines with charged strongly attached to body. Fuel contains ammonium perchlorate, powdered aluminum, polydivinyl-isoprene-urethan rubber with terminal epoxide groups, aromatic amine (aniline), curing catalyst, iron-containing burning catalyst, plasticizers, and finely dispersed modified ammonium chlorate with, adsorbed on the surface thereof, methyltrichlorosilane-water reaction product. Rocket fuel is characterized by polymerization time not higher than 30 h at 80°C, burning rate up to 25 mm/s at pressure 100 kg/cm2 and 20°C.
EFFECT: improved elastic characteristics at positive temperatures.
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| Title | Year | Author | Number |
|---|---|---|---|
| HEAT-RESISTANT GAS-GENERATING COMPOUND FOR HIGH-STRENGTH WELL ELEMENTS | 2002 |
|
RU2233975C2 |
| SOLID ROCKET FUEL | 2000 |
|
RU2170722C1 |
| FUEL COMPOSITION (OPTIONS) | 2017 |
|
RU2649573C1 |
| ROCKET PROPELLANT | 2021 |
|
RU2761188C1 |
| HEAT-RESISTANT GAS-GENERATING SOLID FUEL | 2010 |
|
RU2451004C2 |
| GLUE COMPOSITION | 2004 |
|
RU2259381C1 |
| ICE-GENERATING PROPELLANT | 2005 |
|
RU2313936C2 |
| METHOD OF MAKING MIXED SOLID ROCKET FUEL CHARGE TIGHTLY BONDED TO ROCKET CASING | 2008 |
|
RU2374213C1 |
| METHOD FOR DECREASING VOLATILITY OF CARBOXYLATE RUBBER-BASE SOLID-PROPELLANT COMPOSITIONS OF LIQUID FERROCENE COMPOUNDS AND HIGH-MODULUS CARBOXYLATE RUBBER-BASE SOLID-PROPELLANT COMPOSITION AND LIQUID FERROCENE-CONTAINING CATALYTICALLY ACTIVE PLASTICIZER | 2003 |
|
RU2276162C2 |
| AMMONIUM PERCHLORATE HYDROPHOBIZATION METHOD | 2001 |
|
RU2211207C2 |
