RU2012152502A - ONE-STAGE HEAVY CLASS CARRIER - Google Patents
ONE-STAGE HEAVY CLASS CARRIER Download PDFInfo
- Publication number
- RU2012152502A RU2012152502A RU2012152502/11A RU2012152502A RU2012152502A RU 2012152502 A RU2012152502 A RU 2012152502A RU 2012152502/11 A RU2012152502/11 A RU 2012152502/11A RU 2012152502 A RU2012152502 A RU 2012152502A RU 2012152502 A RU2012152502 A RU 2012152502A
- Authority
- RU
- Russia
- Prior art keywords
- fuel
- launch vehicle
- tanks
- stage
- fuel tank
- Prior art date
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- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
Одноступенчатая ракета-носитель тяжелого класса, состоящая из двигательной установки с одним или несколькими кислородно-водородными жидкостными ракетными двигателями и топливного бака, отличающаяся тем, что одноступенчатая ракета-носитель оснащена одним-двумя дополнительными топливными баками, которые по тандемной (продольной) схеме последовательно расположены на топливном баке ракеты-носителя с помощью проставки, и, кроме этого, ракета-носитель оснащена по пакетной (параллельной) схеме одной или несколькими парами диаметрально противоположных друг относительно друга топливных баков, при этом баки горючего и окислителя дополнительных топливных баков соединены трубопроводами с баками горючего и окислителя топливного бака одноступенчатой ракеты-носителя и установлены с возможностью их отделения после выработки топлива.A heavy-duty single-stage launch vehicle consisting of a propulsion system with one or more oxygen-hydrogen liquid rocket engines and a fuel tank, characterized in that the single-stage launch vehicle is equipped with one or two additional fuel tanks, which are sequentially arranged in a tandem (longitudinal) layout on the fuel tank of the launch vehicle with a spacer, and, in addition, the launch vehicle is equipped with a packet (parallel) circuit with one or more diametrically pairs fuel tanks opposite to each other, while the fuel and oxidizer tanks of the additional fuel tanks are connected by pipelines to the fuel tanks and the oxidizer of the fuel tank of a single-stage launch vehicle and installed with the possibility of separation after the fuel is exhausted.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012152502/11A RU2532289C2 (en) | 2012-12-06 | 2012-12-06 | Light-class single-stage carrier rocket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012152502/11A RU2532289C2 (en) | 2012-12-06 | 2012-12-06 | Light-class single-stage carrier rocket |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2012152502A true RU2012152502A (en) | 2014-06-20 |
| RU2532289C2 RU2532289C2 (en) | 2014-11-10 |
Family
ID=51213360
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012152502/11A RU2532289C2 (en) | 2012-12-06 | 2012-12-06 | Light-class single-stage carrier rocket |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2532289C2 (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU94029156A (en) * | 1994-08-03 | 1996-06-20 | Конструкторское бюро Производственного объединения "Полет" | Multipurpose carrier rocket |
| US6612522B1 (en) * | 1998-03-17 | 2003-09-02 | Starcraft Boosters, Inc. | Flyback booster with removable rocket propulsion module |
| RU19519U1 (en) * | 2001-06-06 | 2001-09-10 | Федеральное государственное унитарное предприятие Государственное машиностроительное конструкторское бюро "Радуга" | WINGED ROCKET WITH ADDITIONAL DISCHARGEABLE MOUNTED FUEL TANKS |
-
2012
- 2012-12-06 RU RU2012152502/11A patent/RU2532289C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2532289C2 (en) | 2014-11-10 |
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