FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used for descending space rocket stage separation parts (SRSSP) from orbits of payloads. SRSSP comprises propellant compartment and power compartment with bottoms. Upper bottom accommodates rotary chambers of rocket gas engine while lower bottom accommodates mid-fight engine (MFE) with elongated charge electrically connected via switchboard with power supply. SRSSP is oriented and stabilised by energy of liquid propellant gasified residues at application of velocity pulse defined by radii of SP MFE descending path apogee and perigee.
EFFECT: decreased area of SRSSP scatter.
3 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF DRIVING CARRIER ROCKET SEPARABLE UNIT FROM PAYLOAD ORBIT AND DEVICE TO THIS END | 2011 |
|
RU2482034C1 |
| 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 WITHDRAWING ROCKET CARRIER SEPARATED SECTION (RCSS) FROM PAY LOAD ORBIT AND POWER PLANT TO THIS END | 2008 |
|
RU2406856C2 |
| METHOD OF SPACECRAFT STAGE SEPARATION PART DESCENT | 2011 |
|
RU2475429C1 |
| METHOD OF SPACE REFUSE WITHDRAWAL FROM PAYLOAD ORBIT EXPLOITING CARRIER ROCKET SEPARATED PART AND ACCELERATING UNIT, AND DEVICE TO THIS END | 2010 |
|
RU2462399C2 |
| INCREASING EFFICIENCY OF SPACE ROCKET WITH MID-FLIGHT LIQUID-PROPELLANT ENGINE | 2014 |
|
RU2562826C1 |
| METHOD OF DESCENDING SEPARATED SPACE ROCKET STAGE AND DEVICE THEREFOR | 2015 |
|
RU2581894C1 |
| METHOD OF DESCENDING SPACE ROCKET STAGE SEPARATION PART AND DEVICE TO THIS END | 2009 |
|
RU2414391C1 |
| METHOD OF ROCKET ENGINE THRUST DEVELOPMENT | 2012 |
|
RU2517993C1 |
