RU2012152500A - ONE-STAGE LIGHT-CLASS CARRIER - Google Patents
ONE-STAGE LIGHT-CLASS CARRIER Download PDFInfo
- Publication number
- RU2012152500A RU2012152500A RU2012152500/11A RU2012152500A RU2012152500A RU 2012152500 A RU2012152500 A RU 2012152500A RU 2012152500/11 A RU2012152500/11 A RU 2012152500/11A RU 2012152500 A RU2012152500 A RU 2012152500A RU 2012152500 A RU2012152500 A RU 2012152500A
- Authority
- RU
- Russia
- Prior art keywords
- fuel
- launch vehicle
- tanks
- fuel tank
- stage light
- Prior art date
Links
Landscapes
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
Одноступенчатая ракета-носитель легкого класса, состоящая из двигательной установки с одним или несколькими жидкостными ракетными двигателями и топливного бака, отличающаяся тем, что одноступенчатая ракета-носитель оснащена одним-двумя дополнительными топливными баками, которые по тандемной схеме последовательно расположены на топливном баке ракеты-носителя с помощью проставки, 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 отделения после выработки топлива.A single-stage light launch vehicle, consisting of a propulsion system with one or more 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 arranged in a tandem arrangement in series on the fuel tank of the launch vehicle with the help of a spacer, while the fuel and oxidizer tanks of the additional fuel tanks are connected by pipelines to the fuel and oxidizer tanks of the fuel tank in one step th launch vehicle and are installed with the possibility of separation after running out of fuel.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012152500/11A RU2532321C2 (en) | 2012-12-06 | 2012-12-06 | Light-class single-stage carrier rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012152500/11A RU2532321C2 (en) | 2012-12-06 | 2012-12-06 | Light-class single-stage carrier rocket |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2012152500A true RU2012152500A (en) | 2014-06-20 |
RU2532321C2 RU2532321C2 (en) | 2014-11-10 |
Family
ID=51213359
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2012152500/11A RU2532321C2 (en) | 2012-12-06 | 2012-12-06 | Light-class single-stage carrier rocket |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2532321C2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EA032110B1 (en) * | 2016-01-04 | 2019-04-30 | Ревик Артурович Степанян | Multi-stage rocket and method of operating the same |
EA030668B1 (en) * | 2016-01-27 | 2018-09-28 | Ревик Артурович Степанян | Multi-stage rocket and method for operating the same |
RU176695U1 (en) * | 2017-09-28 | 2018-01-25 | Ревик Артурович Степанян | Two-stage rocket |
RU2693093C2 (en) * | 2017-10-06 | 2019-07-01 | Ревик Артурович Степанян | Multi-stage rocket and head method of used parts separation |
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 RU2012152500/11A patent/RU2532321C2/en active
Also Published As
Publication number | Publication date |
---|---|
RU2532321C2 (en) | 2014-11-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PH12017502166B1 (en) | Ship | |
AR092686A1 (en) | NATURAL GAS DISTRIBUTOR FOR BICOMUS FUEL TRAILERS | |
AR091889A1 (en) | NATURAL GAS FUEL SYSTEM ADSORBED FOR VEHICLES WITH HYBRID ENGINES | |
RU2012152500A (en) | ONE-STAGE LIGHT-CLASS CARRIER | |
AR084555A1 (en) | MODIFIED ALQUILFENOL-ALDEHIDO RESINS, ITS USE AS ADDITIVES TO IMPROVE THE COLD PROPERTIES OF COLD FUEL AND LIQUID HYDROCARBON FUELS | |
PE20141273A1 (en) | ARRANGEMENT TO STORE AND REMOVE COMPRESSED GAS | |
AR084365A1 (en) | METHOD AND SYSTEM FOR THE DETERMINATION OF A STEERING ANGLE | |
AR090744A1 (en) | DIESEL FUEL SUPPLY CIRCUIT | |
WO2013003184A3 (en) | Hydraulic pressure generating system with buoyancy-adjusted subsystem connected to parabolic-shaped buoy, system further comprising rotatable panels | |
RU2012145047A (en) | ONE-STAGE CARRIER ROCKET | |
RU2012152502A (en) | ONE-STAGE HEAVY CLASS CARRIER | |
CO2020008993A2 (en) | Ecological system for the use of kinetic energy for vehicles | |
WO2014120526A3 (en) | Enhanced rocket engine fueling systems and methods | |
RU2012109250A (en) | AUTOMATICALLY COMBINED WHEEL-CHAIN MOTOR | |
UA88269U (en) | Method of pressurization of fuel tanks of power plant of launcher vehicle | |
RU2012147367A (en) | METHOD FOR REALIZING THE ROCKET ENGINE | |
UA108535C2 (en) | Method of boosting the fuel tanks of moving installation launcher | |
TR201203689U (en) | Fluid transport / storage system with membrane storage. | |
Xianghui | CCS: Pioneer for LNG Ship Standard | |
PE20150080A1 (en) | INTERCONNECTION SYSTEM FOR PANEL ASSEMBLIES | |
RU2014111002A (en) | FUEL AIRCRAFT SYSTEM | |
RU2012138056A (en) | ROCKET | |
RU2012140256A (en) | SCREEN PLAN | |
RU2011113849A (en) | ROCKET | |
JP2017005970A (en) | Vehicle using engine as battery |