Spacecraft launch system and method
US6186039A · kind A · utility
4Cited by
20References
34Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Feb 25, 1998 |
| Grant date | Feb 13, 2001 |
| Priority date | — |
| Expiry date | Feb 25, 2018 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64G5/00
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A spacecraft launch system includes a support assembly and a seat coupled to a hinge having a hinge axis. In operation, the support assembly and the seat rotate about the hinge axis to move the spacecraft from a horizontal position to a vertical position for launching. The launch system may incorporate an alignment technique that includes alignment members and actuators.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.