FIELD: transport.
SUBSTANCE: invention relates to rocketry. Multistage carrier rocket of cluster configuration consists of first stage shuttle equipped with wing and vertical empennage, single-shot second stage, nose and tail bearing structures with locks to integrate said stages into single unit. Tail bearing structure is composed of vertical empennage formed by two keels for second stage to be mechanically locked there between at their free ends. Mating parts of said locks are arranged at second stage outer surface and spaced apart through distance equal to maximum length of second stage cross-section chord.
EFFECT: increased payload, higher reliability.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
| NON-EXPANDABLE AERO-SPACE SYSTEM | 1999 |
|
RU2164882C1 |
| METHOD OF INJECTION OF OBJECTS INTO NEAR-EARTH ORBIT AND RECOVERABLE AERO-SPACE ROCKET AIRCRAFT-CARRIER FOR REALIZATION OF THIS METHOD (AERO-SPACE SYSTEM NUR-SAID SYSTEM) | 2001 |
|
RU2232700C2 |
| CARRIER ROCKET FIRST STAGE FLY-BACK BOOSTER BUILT AROUND UNIFIED ROCKET UNIT | 2012 |
|
RU2492123C1 |
| DEVICE FOR ATTACHMENT AND SEPARATION OF CLUSTER-CONFIGURATION CARRIER ROCKET | 2012 |
|
RU2521888C1 |
| CARRIER ROCKET | 2011 |
|
RU2482030C2 |
| AIRCRAFT MIXED-MODE AERORODYNAMIC AND SPACE FLIGHT AND METHOD FOR ITS PILOTING | 2007 |
|
RU2441815C2 |
| LAUNCH VEHICLE RECOVERABLE BOOSTER | 2006 |
|
RU2321526C1 |
| AIRCRAFT AIRFRAME | 2012 |
|
RU2521936C2 |
| SIMPLIFIED SHUTTLE MODULE FOR CARRIER ROCKET | 2011 |
|
RU2566597C2 |
