FIELD: aviation.
SUBSTANCE: interplanetary spacecraft consists of the main and auxiliary modules. The auxiliary module is fixed to the main module case with the possibility of rotation around the center of the main module weight. The main module is made with accommodation inside residential and office premises, life support systems, outside its housing has solar panels, heat sink radiators, anti-radiation shields. The auxiliary module consists of a rotary frame and a propulsion unit attached to its end, containing propulsion engines and a fuel tank.
EFFECT: increasing the safety, providing traffic with a fixed orientation of the main module to the sun.
5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MANNED SPACE AIRCRAFT | 2020 |
|
RU2774896C2 |
| SPACE RADIATION SHELTER | 2015 |
|
RU2595067C1 |
| REUSABLE SPACECRAFT FOR DELIVERING TOURISTS FROM THE LUNAR FUELING STATION TO THE FLIGHT PATH OF MARS AND SUBSEQUENT RETURN TO THAT STATION | 2020 |
|
RU2741143C1 |
| SPACE VEHICLE | 1992 |
|
RU2072951C1 |
| VEHICLE FOR INTERPLANETARY COMMUNICATION (VERSIONS) | 2015 |
|
RU2621805C2 |
| SPACE PLATFORM | 2016 |
|
RU2688630C2 |
| UNIFIED SPACE PLATFORM MODULAR PRINCIPLE OF BUILDING | 2018 |
|
RU2684877C1 |
| REUSABLE SPACE TRANSPORTATION SYSTEM FOR MASS DELIVERY FROM NEAR-EARTH ORBIT TO CIRCUMLUNAR ORBIT OF TOURISTS OR PAYLOADS AND SUBSEQUENT RETURN TO EARTH | 2019 |
|
RU2736657C1 |
| METHOD OF POWER SUPPLY OF SPACECRAFT WITH ELECTROCHEMICAL GENERATORS DURING FLIGHT | 2007 |
|
RU2360332C2 |
| REUSABLE SPACE TRANSPORTATION SYSTEM FOR ONE-WAY CARGO DELIVERY AND MASS DELIVERY OF TOURISTS FROM LONG ORBIT TO THE LUNAR SURFACE AND FOLLOWING RETURN TO EARTH | 2020 |
|
RU2744844C1 |
