Electrical Interfaces Sample Clauses

Electrical Interfaces. Sea Launch provided electrical interfaces shall include umbilical wiring, SC telemetry and command links including RF re-radiation system and hardwire links and in flight interfaces. Inmarsat shall provide separation connectors for the mission. Electrical interfaces shall be as specified in the Sea Launch User’s Guide, Section 7.2 and Sea Launch Facilities Accommodations Handbook, Section 6 and the Inmarsat -4 IRD, reference document number 4. The launch vehicle adapter standard configuration accommodates two SAE=AS81703-style connectors (37 pins or 61 pins). Inmarsat through Astrium shall supply both halves and provide the mating half to Sea Launch for installation on the adapter. Sea Launch shall provide spacecraft umbilical charging capability of 70A maximum total (35A per connector) up until L-8 hours and 20A maximum total after L-8 hours. Sea Launch shall provide an interface skirt umbilical path during transit to the launch site. The T-0 umbilical path is not available during transit to the launch site. Sea Launch shall provide a re-radiation system for SC telemetry and command that supports a frequency range of 3-18 GHz. Frequencies required outside this range may be negotiated.
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Electrical Interfaces. The Sea Launch provided electrical interfaces shall include separation connectors, umbilical wiring, SC telemetry and command links including RF reradiation system, and in flight interfaces. Electrical interfaces shall be as specified in the Sea Launch User's Guide, section 7.2 and Sea Launch Facilities Accommodations Handbook, section 6. SEA LAUNCH PROPRIETARY ***** Certain information on this page has been omitted and filed separately with the Securities and Exchange Commission. Confidential treatment has been requested with respect to the omitted portions.
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Electrical Interfaces. The Launch Provider provided electrical interfaces shall include, umbilical wiring, SC telemetry and command links including RF re-radiation system, and in flight interfaces. Electrical interfaces shall be as specified in the Atlas Launch System Mission Planner’s Guide (ref. A-4), and the SC to LV ICD. Mission unique configurations shall supersede the Atlas Launch System Mission Planner’s Guide (ref. A-4), and shall be specified in the SC to LV ICD. [*] CONFIDENTIAL TREATMENT REQUESTED BY ICO GLOBAL COMMUNICATIONS (HOLDINGS) LIMITED. [*]
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  • Licensed Software Section 3.17(f).......................................27

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