FIELD: astronautics.
SUBSTANCE: invention relates to aerospace engineering and can be used for launching spacecraft. Space rocket comprises first and second stages in the form of packets of rocket blocks. Second stage has propulsion unit launched from Earth. First and second stages of the missile are assembled of several, for example, three, two-stage submissiles. Each subarray consists of three rocket blocks located in one plane and connected by means of lower and upper power belts. Two side rocket units are the first stage of the submissile, and the central rocket unit is the second stage of the submissile. Central rocket blocks of the submissile in the assembly of the space rocket are located in one plane and are connected by means of power belts forming the second stage of the missile. Side rocket blocks of subarray are the first stage of rocket.
EFFECT: higher energy efficiency.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-STAGE MODULE-TYPE LAUNCH VEHICLE | 2000 |
|
RU2238226C2 |
| MULTISTAGE LAUNCH VEHICLE | 1997 |
|
RU2116941C1 |
| METHOD FOR ORBIT INJECTION OF PAYLOAD BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINATION ARRANGEMENT WITH CRUISE LIQUID- PROPELLANT ROCKET ENGINE INSTALLATIONS (LREI), MULTIFUNCTIONAL LAUNCH VEHICLE WITH CRUISE LPEI AND METHOD FOR ITS DEVELOPMENT | 2000 |
|
RU2161108C1 |
| LAUNCH VEHICLE OF COMBINED CONFIGURATION | 2000 |
|
RU2166463C1 |
| METHOD FOR CONVERSION OF COMBAT SOLID-PROPELLANT ROCKETS INTO SOLID-PROPELLANT SPACE ROCKET AND SPACE ROCKET | 1998 |
|
RU2142898C1 |
| METHOD OF INJECTION OF PAYLOAD INTO NEAR-EARTH SPACE BY MEANS OF AIRCRAFT ROCKET SPACE COMPLEX AND AIRCRAFT ROCKET SPACE COMPLEX FOR REALIZATION OF THIS METHOD | 2005 |
|
RU2265558C1 |
| TWO-STAGE LAUNCH VEHICLE | 1995 |
|
RU2081036C1 |
| LAUNCH VEHICLE CONFIGURATION | 2009 |
|
RU2406660C1 |
| LAUNCH VEHICLE | 1999 |
|
RU2149125C1 |
| SPACE-MISSION ROCKET | 2008 |
|
RU2368542C1 |
