RU2012147367A - METHOD FOR REALIZING THE ROCKET ENGINE - Google Patents
METHOD FOR REALIZING THE ROCKET ENGINE Download PDFInfo
- Publication number
- RU2012147367A RU2012147367A RU2012147367/06A RU2012147367A RU2012147367A RU 2012147367 A RU2012147367 A RU 2012147367A RU 2012147367/06 A RU2012147367/06 A RU 2012147367/06A RU 2012147367 A RU2012147367 A RU 2012147367A RU 2012147367 A RU2012147367 A RU 2012147367A
- Authority
- RU
- Russia
- Prior art keywords
- rocket engine
- realizing
- krt
- gasification
- tanks
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract 3
- 238000002309 gasification Methods 0.000 claims abstract 4
- 239000007788 liquid Substances 0.000 claims abstract 4
- 238000002485 combustion reaction Methods 0.000 claims abstract 2
- 239000002826 coolant Substances 0.000 claims abstract 2
- 239000000446 fuel Substances 0.000 claims abstract 2
- 230000001590 oxidative effect Effects 0.000 claims abstract 2
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000002760 rocket fuel Substances 0.000 claims abstract 2
Landscapes
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
Способ реализации тяги ракетного двигателя, основанный на газификации жидких компонентов ракетного топлива (КРТ) и подаче их в камеру сгорания, отличающийся тем, что после останова маршевого жидкостного ракетного двигателя включают систему газификации КРТ, в шар-баллоны с дополнительными КРТ подают газ наддува и, посредством окислительного и восстановительного газогенераторов, в зависимости от конкретного топлива в баках, осуществляют подачу теплоносителей в баки с остатками КРТ.A method for realizing a thrust of a rocket engine based on gasification of liquid components of rocket fuel (KRT) and feeding them into the combustion chamber, characterized in that after stopping the marching liquid rocket engine, they include a gasification of KRT, pressurized gas is supplied to balloons with additional SRTs, and by means of oxidizing and reducing gas generators, depending on the specific fuel in the tanks, coolants are supplied to the tanks with the remains of SRT.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012147367/06A RU2517993C1 (en) | 2012-11-07 | 2012-11-07 | Method of rocket engine thrust development |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012147367/06A RU2517993C1 (en) | 2012-11-07 | 2012-11-07 | Method of rocket engine thrust development |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2012147367A true RU2012147367A (en) | 2014-05-20 |
| RU2517993C1 RU2517993C1 (en) | 2014-06-10 |
Family
ID=50695389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012147367/06A RU2517993C1 (en) | 2012-11-07 | 2012-11-07 | Method of rocket engine thrust development |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2517993C1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2614271C2 (en) * | 2015-09-15 | 2017-03-24 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Омский государственный технический университет" | Realization method of rocket power and device for its implementation |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3534686A (en) * | 1968-10-04 | 1970-10-20 | Nasa | Payload/burned-out motor case separation system |
| US6684624B2 (en) * | 1998-07-22 | 2004-02-03 | The Board Of Trustees Of The Leland Stanford Junior University | High regression rate hybrid rocket propellants |
| RU2406856C2 (en) * | 2008-06-11 | 2010-12-20 | Государственное Образовательное Учреждение Высшего Профессионального Образования "Омский Государственный Технический Университет" | Method of withdrawing rocket carrier separated section (rcss) from pay load orbit and power plant to this end |
-
2012
- 2012-11-07 RU RU2012147367/06A patent/RU2517993C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2517993C1 (en) | 2014-06-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20171108 |
|
| NF4A | Reinstatement of patent |
Effective date: 20180719 |
|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20191108 |