Title:
打ち上げロケットと衛星を連結および分離する装置
Document Type and Number:
Japanese Patent JP4705172
Kind Code:
B2
Abstract:
A launcher and satellite connection-separation apparatus comprising a band (11) with an inner channel in which a plurality of clamps (13) are located in a sliding manner, which clamps are applied on the rings (15, 17) making up the joining interface between both vehicles, means (19) for radially tightening the band (11)-clamps (13) assembly and a union-separation device (41, 61, 71) of the ends (7, 9) thereof including, together with locking (47) and unlocking (48) means, a mechanism allowing a controlled opening of the band (11) in two phases: in the first phase its ends (7, 9) shift keeping in contact with the rings (15, 17), the elastic energy corresponding to the tightening of the band (11) being dissipated by friction; in the second phase the band (11) separates from the rings (15, 17) until reaching its parking position.
Inventors:
Rancho, Donsel, Miguel
Application Number:
JP2008534030A
Publication Date:
June 22, 2011
Filing Date:
October 06, 2005
Export Citation:
Assignee:
Airdos Casa Espacio Socieda Limitada
International Classes:
B64G1/64
Domestic Patent References:
| JP2005343311A | ||||
| JP2000006899A | ||||
| JP11152100A | ||||
| JP6099922A | ||||
| JP4252800A | ||||
| JP4189700A | ||||
| JP60081000A |
Foreign References:
| US5411349 | ||||
| US5157816 |
Attorney, Agent or Firm:
Hideto Asamura
Hajime Asamura
Yutaka Yoshida
Toru Mori
Hajime Asamura
Yutaka Yoshida
Toru Mori