FIELD: erection of large objects in space, mainly orbital complexes with industrial, laboratory and utility services and auxiliary rooms. SUBSTANCE: space station is made with fixed axial portion and movable cylindrical guard envelope composed of built-up modules of toroidal members where rooms and service are arranged; rooms are in communication with each other and with axial section. Mounted between envelope and axial section are circular linear electric motors and balancing devices for forming artificial gravitation in envelope. On the outside, station is coated with protective cover. Ends of fixed portion are provided with receiving points for arriving space vehicles. When envelope is revolving with the aid of above-mentioned electric motors, artificial gravity is created; adapter circular chambers are used for communication with fixed portion. Adapter circular chambers are provided with lifts secured to them in alternating order; lifts move in circular and transversal directions. EFFECT: reduced expenses; improved quality and enhanced safety of operation in erection of space stations from lightened unified built-up structures and materials. 5 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
LEAN-TO FOR SPACE STATION | 1995 |
|
RU2125526C1 |
SPACE COMPLEX WITH INTERNAL GRAVITATIONAL DRIVE | 1996 |
|
RU2115595C1 |
SPACE REPAIR AND ERECTION COMPLEX | 1997 |
|
RU2128605C1 |
SPACE COMPLEX WITH EXTERNAL GRAVITATIONAL DRIVE | 1996 |
|
RU2115596C1 |
SETTLEMENT IN SPACE | 2003 |
|
RU2264330C2 |
SETTLEMENT IN SPACE | 2002 |
|
RU2223204C2 |
SPACE LAUNCH AREA | 1998 |
|
RU2131830C1 |
ORBITAL SPACE COMPLEX | 1992 |
|
RU2026246C1 |
METHOD OF INTEGRATION OF ORBITAL SPACE COMPLEXES | 1995 |
|
RU2088490C1 |
METHOD FOR LAUNCHING OF OBJECT TO SPACE FROM COSMODROME IN SPACE | 2000 |
|
RU2241643C2 |
Authors
Dates
1998-08-10—Published
1995-12-19—Filed