FIELD: rocket and space technology.
SUBSTANCE: invention relates to aerospace engineering and can be used for acceleration of carrier rocket (CR) with parallel arrangement of tanks for various components of rocket fuel. When starting CR, method includes turning on all liquid propellant rocket engines (LPE) of first stage, supplying power to components of rocket fuel of all LPE stage from central tank containing one of components, and from one side of tank, containing a second component, shutting off fuel lines after complete exhaustion in side tank of all rocket fuel components, releasing side tank together with LPE mounted on it, switching power supply to all remaining rocket engines of second component from other side tank with rocket fuel components, repeating operations of shuting off fuel lines, releasing side tank and switching fuel lines until complete exhaustion all rocket fuel components in all tanks of CR of corresponding stage.
EFFECT: invention increases payload weight and speed of CR with same payload weight.
1 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF IMPLEMENTATION OF RUNNING OF BOOSTER ROCKET | 2015 |
|
RU2628836C2 |
| METHOD OF CARRYING OUT ACCELERATION OF CARRIER-ROCKETS | 2014 |
|
RU2561154C2 |
| METHOD OF DRIVING CARRIER ROCKET SEPARABLE UNIT FROM PAYLOAD ORBIT AND DEVICE TO THIS END | 2011 |
|
RU2482034C1 |
| MULTISTAGE CARRIER ROCKET CONFIGURATION | 2013 |
|
RU2532445C1 |
| MODULE-TYPE LAUNCH VEHICLE (VERSIONS) | 2002 |
|
RU2291817C2 |
| LAUNCH VEHICLE | 2006 |
|
RU2306242C1 |
| CARRIER ROCKET | 2007 |
|
RU2331550C1 |
| METHOD OF ROCKET IN-TANK LIQUID-PROPELLANT GASIFICATION AND DEVICE TO THIS END | 2012 |
|
RU2522536C1 |
| WITHDRAWAL OF CARRIER ROCKET STAGE SEPARATED PART FROM PAYLOAD ORBIT AND DEVICE TO THIS END | 2012 |
|
RU2518918C2 |
| METHOD OF ROCKET ENGINE THRUST DEVELOPMENT | 2012 |
|
RU2517993C1 |
