FIELD: rocket propellants.
SUBSTANCE: invention relates to the field of rocket propellants. Rocket propellant contains liquid nitrous oxide as an oxidizer, and liquid hydrogen as fuel, with a mass ratio of components: liquid nitrous oxide N2O - 95.6%, liquid hydrogen H2 - 4.4%.
EFFECT: increased calorific value of rocket propellant.
1 cl, 5 tbl
Title | Year | Author | Number |
---|---|---|---|
BALLISTITE PROPELLANT | 2001 |
|
RU2191765C1 |
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SOLID BALLISTITE-TYPE PROPELLANT | 2004 |
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BALLISTITE FUEL | 2003 |
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ECOLOGICAL FUEL | 2020 |
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RU2740948C1 |
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|
RU2090545C1 |
SOLID ROCKET FUEL | 2001 |
|
RU2207330C2 |
Authors
Dates
2021-12-06—Published
2021-04-12—Filed