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EP0334485
European procedure
Extract from the Register of European Patents
EP About this file: EP0334485
| EP0334485 - Spacecraft attitude control using coupled thrusters [Right-click to bookmark this link] | Status | No opposition filed within time limit Status updated on 18.05.1995 Database last updated on 21.03.2026 | Most recent event Tooltip | 18.05.1995 | No opposition filed within time limit | published on 05.07.1995 [1995/27] | Applicant(s) | For all designated states Space Systems / Loral, Inc. 3825 Fabian Way Palo Alto California 94303 / US | [N/P] |
| Former [1991/27] | For all designated states SPACE SYSTEMS / LORAL INC. 3825 Fabian Way Palo Alto, California 94303-4697 / US | ||
| Former [1991/12] | For all designated states FORD AEROSPACE CORPORATION 3501 Jamboree Boulevard Suite 500 Newport Beach, CA 92660 / US | ||
| Former [1989/39] | For all designated states FORD AEROSPACE CORPORATION 300 Renaissance Centre Detroit Michigan 48243 / US | Inventor(s) | 01 /
Garg, Subhash C. 1789 Trudean Way San Hose California 95132 / US | 02 /
Bhat, Mahabaleshwar K. P. 1196 Lynbrook Way San Jose California 95129 / US | [1989/39] | Representative(s) | Crawford, Andrew Birkby, et al A.A. Thornton & Co. 235 High Holborn London WC1V 7LE / GB | [N/P] |
| Former [1989/39] | Crawford, Andrew Birkby, et al A.A. THORNTON & CO. Northumberland House 303-306 High Holborn London WC1V 7LE / GB | Application number, filing date | 89301621.2 | 20.02.1989 | [1989/39] | Priority number, date | US19880161931 | 29.02.1988 Original published format: US 161931 | [1989/39] | Filing language | EN | Procedural language | EN | Publication | Type: | A2 Application without search report | No.: | EP0334485 | Date: | 27.09.1989 | Language: | EN | [1989/39] | Type: | A3 Search report | No.: | EP0334485 | Date: | 04.10.1989 | Language: | EN | [1989/40] | Type: | B1 Patent specification | No.: | EP0334485 | Date: | 13.07.1994 | Language: | EN | [1994/28] | Search report(s) | (Supplementary) European search report - dispatched on: | EP | 18.08.1989 | Classification | IPC: | G05D1/08, B64G1/26 | [1989/39] | CPC: |
G09B9/52 (EP,US);
B64G1/244 (EP,US);
B64G1/26 (EP,US)
| Designated contracting states | DE, FR, GB [1989/39] | Title | German: | Lageregelung eines Raumfahrzeuges mit gekoppelten Schubdüsen | [1989/39] | English: | Spacecraft attitude control using coupled thrusters | [1989/39] | French: | Dispositif de commande d'altitude de véhicule spatial avec des tuyères accouplées | [1989/39] | Examination procedure | 21.03.1990 | Examination requested [1990/20] | 27.10.1992 | Despatch of a communication from the examining division (Time limit: M04) | 17.02.1993 | Reply to a communication from the examining division | 16.11.1993 | Despatch of communication of intention to grant (Approval: Yes) | 17.01.1994 | Communication of intention to grant the patent | 07.04.1994 | Fee for grant paid | 07.04.1994 | Fee for publishing/printing paid | Opposition(s) | 14.04.1995 | No opposition filed within time limit [1995/27] | Fees paid | Renewal fee | 21.01.1991 | Renewal fee patent year 03 | 20.01.1992 | Renewal fee patent year 04 | 29.01.1993 | Renewal fee patent year 05 | 08.02.1994 | Renewal fee patent year 06 |
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| Responsibility for the accuracy, completeness or quality of the data displayed under the link provided lies entirely with the Unified Patent Court. | Documents cited: | Search | [Y] JOURNAL OF GUIDANCE AND CONTROL, vol. 3, no. 3, May-June 1980, pages 195-202, NY, US, K.L. Lebsock: 'High pointing accuracy with a momentum bias atitude control system' [Y] |