Title:
複数のペイロードを同一ランチャ上に担持するための傾斜アダプタ
Document Type and Number:
Japanese Patent JP3801640
Kind Code:
B2
Abstract:
PCT No. PCT/FR96/00847 Sec. 371 Date Feb. 6, 1997 Sec. 102(e) Date Feb. 6, 1997 PCT Filed Jun. 5, 1996 PCT Pub. No. WO96/39328 PCT Pub. Date Dec. 12, 1996In order to be able to install in juxtaposed manner several satellites beneath the nose cone of the same launcher without any collision risk at the time of their separation, between each satellite and the support plate is positioned an adaptor. During launch, the adaptors occupy a size-limiting carriage position. When it is wished to control the separation of a satellite, its adaptor passes into a separation position, in which the satellite is tilted or swung away from the neighbouring satellite or satellites.
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Inventors:
Obry, daniel
Pimon, lemon
Sievalier, gui
Pimon, lemon
Sievalier, gui
Application Number:
JP50019297A
Publication Date:
July 26, 2006
Filing Date:
June 05, 1996
Export Citation:
Assignee:
Aerospatial Societe Nacional Andeustriel
International Classes:
B64G1/64; F42B12/60; B64G1/00; B64G1/10
Domestic Patent References:
| JP5116699A | ||||
| JP3121393U | ||||
| JP5112300A |
Foreign References:
| DE4243562A1 | ||||
| US3903803 | ||||
| US4632339 | ||||
| US4679752 | ||||
| EP0381869A1 |
Attorney, Agent or Firm:
Yoshio Kawaguchi
Toru Nakamura
Takeshi Funayama
Naoya Fushimi
Toru Nakamura
Takeshi Funayama
Naoya Fushimi