FIELD: space engineering; launching manned and unmanned spacecraft from Earth.
SUBSTANCE: proposed system includes linear electric drive with stator in form of circular windings with core located inside them. Core is made in form of magnetic envelope of launch vehicle. Launch vehicle with spacecraft is located inside this envelope. Stator windings are mounted on trestle assembled from separate members with supports. Charge mounted in envelope operates at the end of trestle ejecting the launch vehicle from envelope at simultaneous deceleration of envelope. Supports are provided with seismic protective units and follow-up system for elimination of shift of windings. Launch vehicle may be installed along mountain slope.
EFFECT: enhanced economical efficiency of launching spacecraft.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| REUSABLE TRANSPORT APPARATUS | 2020 |
|
RU2759060C1 |
| MOTOR-GENERATOR | 2003 |
|
RU2256995C2 |
| MULTI-PURPOSE SYSTEM OF ELECTRIC DRIVES ON BASIS OF PLANETARY CYCLOIDAL REDUCTION GEAR - MKE PCSR | 2008 |
|
RU2452883C2 |
| MULTISTAGE AXIAL AND RADIAL INGUGSTROM TURBOMACHINE WITHOUT OUTPUT SHAFT | 2002 |
|
RU2253737C2 |
| AEROSPACE LAUNCHING COMPLEX MARS | 2001 |
|
RU2215673C2 |
| ELECTRICAL AIR START SYSTEM OF THE SPACE ROCKET | 2017 |
|
RU2658236C1 |
| VEHICLE | 1999 |
|
RU2158683C1 |
| ELECTRIC DRIVE WITH CYCLOID PLANETARY REDUCTION GEAR | 2000 |
|
RU2206805C2 |
| VEHICLE FOR INTERPLANETARY COMMUNICATION (VERSIONS) | 2015 |
|
RU2621805C2 |
| SPACE MISSILE AIR-BREATHING LAUNCH SYSTEM WITH THE ELECTRIC START | 2016 |
|
RU2620172C1 |
