RU2014119365A - METHOD FOR IMPROVING MISSILE FUELS AND MISSILE FUEL / OPTIONS / - Google Patents
METHOD FOR IMPROVING MISSILE FUELS AND MISSILE FUEL / OPTIONS / Download PDFInfo
- Publication number
- RU2014119365A RU2014119365A RU2014119365/05A RU2014119365A RU2014119365A RU 2014119365 A RU2014119365 A RU 2014119365A RU 2014119365/05 A RU2014119365/05 A RU 2014119365/05A RU 2014119365 A RU2014119365 A RU 2014119365A RU 2014119365 A RU2014119365 A RU 2014119365A
- Authority
- RU
- Russia
- Prior art keywords
- beryllium
- rocket fuel
- following ratio
- boron
- fuel
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title claims abstract 6
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 claims abstract 30
- 239000002760 rocket fuel Substances 0.000 claims abstract 30
- 229910052790 beryllium Inorganic materials 0.000 claims abstract 17
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract 17
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 claims abstract 10
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract 10
- 229910052796 boron Inorganic materials 0.000 claims abstract 10
- AYBCUKQQDUJLQN-UHFFFAOYSA-N hydridoberyllium Chemical compound [H][Be] AYBCUKQQDUJLQN-UHFFFAOYSA-N 0.000 claims abstract 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract 4
- UORVGPXVDQYIDP-UHFFFAOYSA-N borane Chemical class B UORVGPXVDQYIDP-UHFFFAOYSA-N 0.000 claims abstract 4
- 150000001875 compounds Chemical class 0.000 claims abstract 4
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract 4
- 229910052580 B4C Inorganic materials 0.000 claims abstract 2
- BRUFJXUJQKYQHA-UHFFFAOYSA-O ammonium dinitramide Chemical compound [NH4+].[O-][N+](=O)[N-][N+]([O-])=O BRUFJXUJQKYQHA-UHFFFAOYSA-O 0.000 claims abstract 2
- 229910000085 borane Inorganic materials 0.000 claims abstract 2
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000003245 coal Substances 0.000 claims abstract 2
- ZOCHARZZJNPSEU-UHFFFAOYSA-N diboron Chemical compound B#B ZOCHARZZJNPSEU-UHFFFAOYSA-N 0.000 claims abstract 2
- 229910021389 graphene Inorganic materials 0.000 claims abstract 2
- 229910002804 graphite Inorganic materials 0.000 claims abstract 2
- 239000010439 graphite Substances 0.000 claims abstract 2
- 239000004071 soot Substances 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 2
- RFVVBBUVWAIIBT-UHFFFAOYSA-N beryllium nitrate Chemical compound [Be+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O RFVVBBUVWAIIBT-UHFFFAOYSA-N 0.000 claims 2
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 claims 1
- ZWWCURLKEXEFQT-UHFFFAOYSA-N dinitrogen pentaoxide Chemical compound [O-][N+](=O)O[N+]([O-])=O ZWWCURLKEXEFQT-UHFFFAOYSA-N 0.000 claims 1
- 229910017604 nitric acid Inorganic materials 0.000 claims 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B47/00—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
- C06B47/02—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant
- C06B47/10—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant a component containing free boron, an organic borane or a binary compound of boron, except with oxygen
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B27/00—Compositions containing a metal, boron, silicon, selenium or tellurium or mixtures, intercompounds or hydrides thereof, and hydrocarbons or halogenated hydrocarbons
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
- C06B31/28—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
- C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
- C06D5/06—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by reaction of two or more solids
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Inorganic Chemistry (AREA)
- Solid Fuels And Fuel-Associated Substances (AREA)
- Catalysts (AREA)
Abstract
1. Способ улучшения ракетных топлив, содержащих хотя бы в одном из компонентов связанный азот, отличающийся тем, что к ракетному топливу добавляется мелкодисперсный бор или его горючие соединения.2. Способ по п. 1, отличающийся тем, что добавка бора составляет 1:1 к азоту по соотношению молекул, +-20%.3. Способ по п. 1, отличающийся тем, что упомянутыми соединениями являются бораны (гидриды бора), боргидриды, бориды, карбид бора.4. Способ по п. 1, отличающийся тем, что в топливо добавляется 0,0001-1% мелкодисперсного угля, графита, сажи, графена.5. Ракетное топливо, отличающееся от исходного тем, что выполнено по способу п. 1.6. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: нитрата аммония с тетрабораном в соотношении 69,25:30,75, все +-10%.7. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: нитрат аммония 59,40%, бериллий - 20,06%, диборан - 20,54%, все +-15%.8. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: нитрат аммония - 56,85%+-15%, гидрид бериллия - 23,50%+-15%, и диборан - 19,65%+-15%.9. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: нитрат аммония, гидрид бериллия, боргидрид бериллия - 56,85:15,67:27,48, все +-15%.10. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: нитрат аммония 62,20%, бериллий - 21,00%, и бор - 16,80%, все +-15%.11. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: динитрамида аммония (далее ДНА) ДНА - 63,26+-15%, бор - 36,74+-15%.12. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: ДНА - 69,94+-15%, тетраборан - 30,06+-15%.13. Ракетное топливо, отличающееся тем, что имеет следующее соотношение: ДНА - 62,84+-15%, бериллий - 9,13+-9%, диборан - 28,03+-15%14. Ракетное топливо, отлич�1. A method for improving rocket fuels containing bound nitrogen in at least one of the components, characterized in that finely dispersed boron or its combustible compounds are added to the rocket fuel. A method according to claim 1, characterized in that the addition of boron is 1: 1 to nitrogen by the ratio of molecules, + -20%. 3. A method according to claim 1, characterized in that the said compounds are boranes (boron hydrides), borohydrides, borides, boron carbide. The method according to claim 1, characterized in that 0.0001-1% of finely dispersed coal, graphite, soot, graphene is added to the fuel. Rocket fuel, different from the original one in that it is made according to the method of clause 1.6. Rocket fuel, characterized in that it has the following ratio: ammonium nitrate with tetraborane in a ratio of 69.25: 30.75, all + -10% .7. Rocket fuel, characterized in that it has the following ratio: ammonium nitrate 59.40%, beryllium - 20.06%, diborane - 20.54%, all + -15% .8. Rocket fuel, characterized in that it has the following ratio: ammonium nitrate - 56.85% + - 15%, beryllium hydride - 23.50% + - 15%, and diborane - 19.65% + - 15% .9. Rocket fuel, characterized in that it has the following ratio: ammonium nitrate, beryllium hydride, beryllium borohydride - 56.85: 15.67: 27.48, all + -15% .10. Rocket fuel, characterized in that it has the following ratio: ammonium nitrate 62.20%, beryllium - 21.00%, and boron - 16.80%, all + -15% .11. Rocket fuel, characterized in that it has the following ratio: ammonium dinitramide (hereinafter DND) DND - 63.26 + -15%, boron - 36.74 + -15% .12. Rocket fuel, characterized in that it has the following ratio: DND - 69.94 + -15%, tetraboran - 30.06 + -15% .13. Rocket fuel, characterized in that it has the following ratio: DND - 62.84 + -15%, beryllium - 9.13 + -9%, diboran - 28.03 + -15% 14. Rocket fuel, excellent
Claims (22)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2014119365/05A RU2582712C2 (en) | 2014-05-13 | 2014-05-13 | Rocket propellant /versions/ |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2014119365/05A RU2582712C2 (en) | 2014-05-13 | 2014-05-13 | Rocket propellant /versions/ |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2014119365A true RU2014119365A (en) | 2015-11-20 |
| RU2582712C2 RU2582712C2 (en) | 2016-04-27 |
Family
ID=54553014
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2014119365/05A RU2582712C2 (en) | 2014-05-13 | 2014-05-13 | Rocket propellant /versions/ |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2582712C2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102020118962A1 (en) | 2020-07-17 | 2022-01-20 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung eingetragener Verein | Fast-burning solid propellant with an oxidizer, an energetic binder and a metallic burn-up modifier and method for its production |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3309248A (en) * | 1962-01-24 | 1967-03-14 | Dow Chemical Co | Solid propellants containing hydrazonium azide and boron compounds |
| US3551224A (en) * | 1962-09-10 | 1970-12-29 | Us Army | Nitrated cellulose rocket propellants with amino fluorine containing plasticizer |
| US3247034A (en) * | 1964-04-06 | 1966-04-19 | Dal Mon Research Co | Polymeric high energy boron fuel compositions |
| US3552127A (en) * | 1964-08-25 | 1971-01-05 | Jacque C Morrell | Composite high energy rocket propellants and process for same |
| US3577289A (en) * | 1968-02-12 | 1971-05-04 | Jacque C Morrell | Composite high energy solid rocket propellants and process for same |
| RU2182163C2 (en) * | 1995-06-07 | 2002-05-10 | Уильям К. Орр | Fuel composition |
| RU2486230C1 (en) * | 2012-07-04 | 2013-06-27 | Николай Евгеньевич Староверов | Combustible rocket propellant (versions) and method for preparation thereof |
-
2014
- 2014-05-13 RU RU2014119365/05A patent/RU2582712C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2582712C2 (en) | 2016-04-27 |
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