NO119830B - - Google Patents
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- Publication number
- NO119830B NO119830B NO301169A NO301169A NO119830B NO 119830 B NO119830 B NO 119830B NO 301169 A NO301169 A NO 301169A NO 301169 A NO301169 A NO 301169A NO 119830 B NO119830 B NO 119830B
- Authority
- NO
- Norway
- Prior art keywords
- plastic
- combustion catalyst
- fuel
- weight
- mixture
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims description 8
- 239000004033 plastic Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 7
- 239000003054 catalyst Substances 0.000 claims description 6
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 claims description 5
- 239000002760 rocket fuel Substances 0.000 claims description 5
- 229920002367 Polyisobutene Polymers 0.000 claims description 3
- VLTRZXGMWDSKGL-UHFFFAOYSA-M perchlorate Inorganic materials [O-]Cl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-M 0.000 claims description 3
- VLTRZXGMWDSKGL-UHFFFAOYSA-N perchloric acid Chemical compound OCl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-N 0.000 claims description 3
- 239000000080 wetting agent Substances 0.000 claims description 3
- 229910044991 metal oxide Inorganic materials 0.000 claims description 2
- 150000004706 metal oxides Chemical class 0.000 claims description 2
- 239000000446 fuel Substances 0.000 description 6
- 235000015842 Hesperis Nutrition 0.000 description 4
- 235000012633 Iberis amara Nutrition 0.000 description 4
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- 239000007800 oxidant agent Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- IIZPXYDJLKNOIY-JXPKJXOSSA-N 1-palmitoyl-2-arachidonoyl-sn-glycero-3-phosphocholine Chemical compound CCCCCCCCCCCCCCCC(=O)OC[C@H](COP([O-])(=O)OCC[N+](C)(C)C)OC(=O)CCC\C=C/C\C=C/C\C=C/C\C=C/CCCCC IIZPXYDJLKNOIY-JXPKJXOSSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- PADMMUFPGNGRGI-UHFFFAOYSA-N dunnite Chemical compound [NH4+].[O-]C1=C([N+]([O-])=O)C=C([N+]([O-])=O)C=C1[N+]([O-])=O PADMMUFPGNGRGI-UHFFFAOYSA-N 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 229940067606 lecithin Drugs 0.000 description 1
- 235000010445 lecithin Nutrition 0.000 description 1
- 239000000787 lecithin Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- 238000009489 vacuum treatment Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/007—Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Solid Fuels And Fuel-Associated Substances (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Medicinal Preparation (AREA)
Description
Plastisk rakettdrivstoff. Plastic rocket fuel.
Denne oppfinnelse vedrorer et plastisk rakettdrivstoff spesielt for anvendelse i raålraketter, redningsraketter, fyrverkeri-raketter og lignende. This invention relates to a plastic rocket fuel especially for use in crude rockets, rescue rockets, firework rockets and the like.
Plastisk drivstoff for raketter er tidligere kjent bestående av en blanding av et oksydasjonsmiddel såsom et perklorat,et organisk brensel som ammoniumpikrat, en forbrenningskatalysator såsom titan-dioksyd, et bindemiddel for de faste bestanddeler, f.eks.' polyisobu-len som også virker som brensel, og et fuktemiddel eller overflate-aktivt stoff, f.eks. lecitin. Ovennevnte blanding ble blandet i en blandemaskin og måtte deretter valses på differensialvalser for å meddele blandingen plastisk konsistens. Plastic fuel for rockets is previously known consisting of a mixture of an oxidizing agent such as a perchlorate, an organic fuel such as ammonium picrate, a combustion catalyst such as titanium dioxide, a binder for the solid components, e.g. polyisobutylene, which also acts as fuel, and a wetting agent or surface-active substance, e.g. lecithin. The above mixture was mixed in a mixing machine and then had to be rolled on differential rollers to give the mixture a plastic consistency.
Det er nu funnet at ved å benytte et forholdsvis hbyt inn-hold av ZnO, f.eks. ca. 25 vektprosent, virker dette dels som forbrenningskatalysator og dels som fyllstoff og oksydasjonsmiddel, og videre vil dot ved blandingen av komponentene ved en temperatur av ca. 70° C bevirke at det allerede i blandcmaskinen fås en plastisk masse som direkte kan formes til egnede ladninger ved stamping uten valsing og vakuumbehandling for at luftinneslutninger skal unn-gås. It has now been found that by using a relatively high content of ZnO, e.g. about. 25 percent by weight, this acts partly as a combustion catalyst and partly as a filler and oxidizing agent, and further will dot when the components are mixed at a temperature of approx. 70° C means that already in the mixing machine a plastic mass is obtained which can be directly formed into suitable charges by stamping without rolling and vacuum treatment in order to avoid air inclusions.
Oppfinnelsen vedrorer således et plastisk rakettdrivstoff omfattende en blanding av et perklorat, polyisobutylen, et fuktningsmiddel og en forbrenningskatalysator i form av et metalloksyd, og oppfinnelsen utmerker seg ved at det sem forbrenningskatalysator inneholder ZnO i en mengde av 15 - 30 vektprosent. The invention thus relates to a plastic rocket fuel comprising a mixture of a perchlorate, polyisobutylene, a wetting agent and a combustion catalyst in the form of a metal oxide, and the invention is distinguished by the fact that the combustion catalyst contains ZnO in an amount of 15 - 30 percent by weight.
Et foretrukket eksempel på en sammensetning ifolge oppfinnelsen er folgende bestanddeler regnet i vektprosent: A preferred example of a composition according to the invention is the following components calculated in percentage by weight:
Faste rakettdrivstoffer er karakterisert ved en nedre Solid rocket fuels are characterized by a lower
grense for forbrenningstrykket når de brenner i en rakettmotor, men under denne grense brenner disse drivstoffer ujevnt hvilket bevirker en nedsatt motorytelse eller at rakettmotoren eventuelt slukner. Et drivstoff ifolge oppfinnelsen brenner også stabilt ved trykk under 5 kp/cm 2, og dette muliggjor et skyvkraftforhold pa over 1 : 30 for brenntrykk i startfasen på f.eks. 150 kp/cm 2 i en enkammermotor. limit for the combustion pressure when they burn in a rocket engine, but below this limit these fuels burn unevenly, which causes a reduced engine performance or that the rocket engine eventually shuts down. A fuel according to the invention also burns stably at pressures below 5 kp/cm 2 , and this enables a thrust ratio of over 1:30 for combustion pressures in the initial phase of e.g. 150 kp/cm 2 in a single-chamber engine.
Claims (2)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO301169A NO119830B (en) | 1969-07-19 | 1969-07-19 | |
| DE19702006229 DE2006229A1 (en) | 1969-07-19 | 1970-02-12 | Plastic rocket fuel |
| GB2943370A GB1307239A (en) | 1969-07-19 | 1970-06-17 | Plastic rocket propellants |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO301169A NO119830B (en) | 1969-07-19 | 1969-07-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NO119830B true NO119830B (en) | 1970-07-06 |
Family
ID=19879310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO301169A NO119830B (en) | 1969-07-19 | 1969-07-19 |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2006229A1 (en) |
| GB (1) | GB1307239A (en) |
| NO (1) | NO119830B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2193491B (en) * | 1978-07-21 | 1988-09-14 | Imi Kynoch Limited Kynoch Work | Improvements in propellants |
| GB2246348B (en) * | 1986-07-15 | 1993-03-03 | Ici Plc | Nitrocellulose propellant composition |
-
1969
- 1969-07-19 NO NO301169A patent/NO119830B/no unknown
-
1970
- 1970-02-12 DE DE19702006229 patent/DE2006229A1/en active Pending
- 1970-06-17 GB GB2943370A patent/GB1307239A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1307239A (en) | 1973-02-14 |
| DE2006229A1 (en) | 1971-01-28 |
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