RU2012128750A - MISSILE FUEL - Google Patents
MISSILE FUEL Download PDFInfo
- Publication number
- RU2012128750A RU2012128750A RU2012128750/05A RU2012128750A RU2012128750A RU 2012128750 A RU2012128750 A RU 2012128750A RU 2012128750/05 A RU2012128750/05 A RU 2012128750/05A RU 2012128750 A RU2012128750 A RU 2012128750A RU 2012128750 A RU2012128750 A RU 2012128750A
- Authority
- RU
- Russia
- Prior art keywords
- fuel
- ratio
- beryllium
- components
- fuel according
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title claims abstract 37
- BRUFJXUJQKYQHA-UHFFFAOYSA-O ammonium dinitramide Chemical compound [NH4+].[O-][N+](=O)[N-][N+]([O-])=O BRUFJXUJQKYQHA-UHFFFAOYSA-O 0.000 claims abstract 10
- 229910052790 beryllium Inorganic materials 0.000 claims abstract 10
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract 10
- 229910052751 metal Inorganic materials 0.000 claims abstract 6
- 239000002184 metal Substances 0.000 claims abstract 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract 4
- RFVVBBUVWAIIBT-UHFFFAOYSA-N beryllium nitrate Chemical compound [Be+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O RFVVBBUVWAIIBT-UHFFFAOYSA-N 0.000 claims abstract 4
- 229910052796 boron Inorganic materials 0.000 claims abstract 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract 2
- XWROSHJVVFETLV-UHFFFAOYSA-N [B+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O Chemical compound [B+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O XWROSHJVVFETLV-UHFFFAOYSA-N 0.000 claims abstract 2
- 229910052782 aluminium Inorganic materials 0.000 claims abstract 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000011230 binding agent Substances 0.000 claims abstract 2
- ZWWCURLKEXEFQT-UHFFFAOYSA-N dinitrogen pentaoxide Chemical compound [O-][N+](=O)O[N+]([O-])=O ZWWCURLKEXEFQT-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000003822 epoxy resin Substances 0.000 claims abstract 2
- -1 for example Substances 0.000 claims abstract 2
- 229910052744 lithium Inorganic materials 0.000 claims abstract 2
- 150000002739 metals Chemical class 0.000 claims abstract 2
- 239000000178 monomer Substances 0.000 claims abstract 2
- 229920000647 polyepoxide Polymers 0.000 claims abstract 2
- 229920001225 polyester resin Polymers 0.000 claims abstract 2
- 239000004645 polyester resin Substances 0.000 claims abstract 2
- 229920002635 polyurethane Polymers 0.000 claims abstract 2
- 239000004814 polyurethane Substances 0.000 claims abstract 2
- 230000005855 radiation Effects 0.000 claims abstract 2
Landscapes
- Solid Fuels And Fuel-Associated Substances (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
1. Ракетное горючее, отличающееся тем, что содержит только металл (металлы) и/или бор.2. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: бериллия - 22,52%+-15%, динитрамида аммония - 77,48%+-15%.3. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: бериллия - 12,68%+-15%, динитрамида аммония - 87,32%+-15%.4. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: бериллия - 25,30%+-15%, нитрата бериллия - 74,70%+-15%.5. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: бериллия - 25,56%+-15%, нитрата бора - 74,44%+-15%6. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: бериллия - 29,44%+-15%, пятиокиси азота - 70,56%+-15%.7. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: лития - 30,92%+-15%, динитрамида аммония - 69,08%+-15%.8. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: бора - 18,85%+-15%, динитрамида аммония - 81,15%+-15%.9. Горючее по п.1, отличающееся тем, что соотношение компонентов топлива: алюминия - 35,83%+-15%, динитрамида аммония - 64,17,%+-15%.10. Горючее по п.1, отличающееся тем, что металл скреплен небольшим количеством связующего, например, полиэфирной или эпоксидной смолы, полиуретана и т.п., причем полимеризация мономера желательна радиационная.1. Missile fuel, characterized in that it contains only metal (metals) and / or boron. 2. The fuel according to claim 1, characterized in that the ratio of fuel components: beryllium is 22.52% + - 15%, ammonium dinitramide - 77.48% + - 15% .3. The fuel according to claim 1, characterized in that the ratio of fuel components: beryllium is 12.68% + - 15%, ammonium dinitramide - 87.32% + - 15% .4. Fuel according to claim 1, characterized in that the ratio of fuel components: beryllium is 25.30% + - 15%, beryllium nitrate - 74.70% + - 15% .5. The fuel according to claim 1, characterized in that the ratio of fuel components: beryllium is 25.56% + - 15%, boron nitrate - 74.44% + - 15% 6. Fuel according to claim 1, characterized in that the ratio of fuel components: beryllium is 29.44% + - 15%, nitrogen pentoxide - 70.56% + - 15% .7. The fuel according to claim 1, characterized in that the ratio of fuel components: lithium is 30.92% + - 15%, ammonium dinitramide - 69.08% + - 15% .8. Fuel according to claim 1, characterized in that the ratio of fuel: boron components is 18.85% + - 15%, ammonium dinitramide - 81.15% + - 15% .9. The fuel according to claim 1, characterized in that the ratio of fuel components: aluminum is 35.83% + - 15%, ammonium dinitramide - 64.17,% + - 15% .10. The fuel according to claim 1, characterized in that the metal is bonded with a small amount of a binder, for example, polyester or epoxy resin, polyurethane, etc., moreover, the polymerisation of the monomer is desirable radiation.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012128750/05A RU2523367C2 (en) | 2012-07-09 | 2012-07-09 | Rocket fuel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012128750/05A RU2523367C2 (en) | 2012-07-09 | 2012-07-09 | Rocket fuel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2012128750A true RU2012128750A (en) | 2014-01-20 |
| RU2523367C2 RU2523367C2 (en) | 2014-07-20 |
Family
ID=49944780
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012128750/05A RU2523367C2 (en) | 2012-07-09 | 2012-07-09 | Rocket fuel |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2523367C2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2688510C2 (en) * | 2017-07-04 | 2019-05-21 | Николай Евгеньевич Староверов | Fuel for wakeless torpedo (versions) |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2205863C2 (en) * | 1994-03-02 | 2003-06-10 | Уильям С. ОРР | Fuel composition and a method for creation of precombustion vapors |
| RU2182163C2 (en) * | 1995-06-07 | 2002-05-10 | Уильям К. Орр | Fuel composition |
| US6254705B1 (en) * | 1999-02-26 | 2001-07-03 | Svenska Rymdaktiebolaget | Liquid propellant |
| RU2309140C2 (en) * | 2005-02-24 | 2007-10-27 | Общество с ограниченной ответственностью"Композит" | Method for preparing gel-like rocket monofuel |
-
2012
- 2012-07-09 RU RU2012128750/05A patent/RU2523367C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2523367C2 (en) | 2014-07-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| MX2018006138A (en) | Structural adhesive with improved failure mode. | |
| Siddiqui et al. | Capacity switching options under rivalry and uncertainty | |
| RU2016120582A (en) | EVAPORABLE HETTER ALLOYS, SPECIALLY SUITABLE FOR SORPTION OF HYDROGEN AND CARBON MONOXIDE | |
| JP2013172518A5 (en) | ||
| IN2014KN01773A (en) | ||
| CO7280469A2 (en) | Safe mixtures of ammonium nitrate (an) with urea or a product comprising an with a product comprising urea | |
| Hardin et al. | Quasi-uniformity of minimal weighted energy points on compact metric spaces | |
| RU2012128750A (en) | MISSILE FUEL | |
| BR112015028273A2 (en) | method for producing an epoxy isocyanate hybrid resin, epoxy isocyanate hybrid resin and use of such a resin | |
| RU2013103958A (en) | FIRE PROTECTION COMPOSITION | |
| RU2014132123A (en) | New rocket fuels based on metal perchlorates | |
| WO2013101740A3 (en) | Low temperature curable epoxy system | |
| RU2014124622A (en) | Explosive Staroverov - 4 / options / | |
| Jiang et al. | Stochastic wave equation of pure jumps: Existence, uniqueness and invariant measures | |
| RU2014119364A (en) | CHARGING TO LIGHT-GAS WEAPONS (OPTIONS) | |
| RU2014124618A (en) | Light Gas Charge - 13 / options / | |
| RU2012128251A (en) | MISSILE FUEL OXIDIZER | |
| CN204884575U (en) | Casing of corrosion resistant, high rigidity | |
| RU2014119367A (en) | Cumulative charge Stararov-10 | |
| RU2014124620A (en) | MISSILE FUEL STAROVEROVA-18 / OPTIONS / | |
| RU2014124619A (en) | EXPLOSIVES STAROVEROVA - 2 / OPTIONS / | |
| TH157382A (en) | Resin composition, prepreg, resin panels and metal foil-covered laminates | |
| RU2014124621A (en) | Light Gas Charge - 12 / options / | |
| RU2012142882A (en) | ROCKET ENGINE STAROVEROVA - 14 (OPTIONS) | |
| Nabok | PROBLEMS OF ECONOMIC SECURITY OF UKRAINE AS A COMPONENT OF STATE SECURITY |