Spacecraft to Launch Vehicle Interfaces Sample Clauses

Spacecraft to Launch Vehicle Interfaces. The SC to LV interfaces are as specified in the herein-referenced sections of the Sea Launch User’s Guide and the Inmarsat -4 IRD, reference document number 4. Once signed, the INXXXXXX 0 xo Sea Launch System ICD shall supersede the interfaces defined here.
Sample 1
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Spacecraft to Launch Vehicle Interfaces. The SC to LV interfaces are as specified in the herein-referenced sections of the Sea Launch User's Guide. Once signed, the XM-4 SC to Sea Launch System ICD shall supercede the interfaces defined here.
Sample 1
Spacecraft to Launch Vehicle Interfaces. The SC to LV interfaces shall be as specified in the herein-referenced sections of the Atlas Launch System Mission Planner’s Guide (ref. A-4). Once signed, the SC to LV ICD shall supersede the interfaces defined within this SOW, and the Atlas Launch System Mission Planner’s Guide (ref. A-4).
Sample 1

Related to Spacecraft to Launch Vehicle Interfaces

  • Launch Customer shall use commercially reasonable efforts to begin distribution of the Google Desktop Applications promptly following the launch of the Desktop Portal.

  • Interfaces 1 2 wire i/f (towards PSTN) -------------------------------------------------------------------------------------------------------- 2 2 wire i/f (towards standard handset) -------------------------------------------------------------------------------------------------------- 2.2 FUNCTIONS -------------------------------------------------------------------------------------------------------- 1 Selective Call -------------------------------------------------------------------------------------------------------- 2 Conference Call (up to four participants) ----------------------------------------------------------------------------------------------------------------------------------- ----------------------------------------------------------------------------------------------------------------------------------- 3 MANAGEMENT COMMUNICATION -------------------------------------------------------------------------------------------------------- 3.1 COMMUNICATION INTERFACES see OPTera Product Description SEC. 5.2.3 - Standard Communications Interfaces and SEC.7.3 - Management Communication -------------------------------------------------------------------------------------------------------- 1 F- Interface (RS 232) -------------------------------------------------------------------------------------------------------- 2 Q- interface as gateway to the EMS -------------------------------------------------------------------------------------------------------- 3 Qecc Routing (2 level IS-IS) -------------------------------------------------------------------------------------------------------- 4 Q I/F (Ethernet) -------------------------------------------------------------------------------------------------------- 5 Optical Supervisory Channel ----------------------------------------------------------------------------------------------------------------------------------- 6 OSC - wavelength IR IR IR see OPTera Product - bitrate Description SEC. 5.2.2 - optical span limit - Per Wavelength - transmission protocol Optical Service Channel and SEC.7.3 - Management Communication ----------------------------------------------------------------------------------------------------------------------------------- ----------------------------------------------------------------------------------------------------------------------------------- 3.2 O & M INTERFACES ----------------------------------------------------------------------------------------------------------------------------------- 1 8 x Remote Control Inputs ----------------------------------------------------------------------------------------------------------------------------------- 2 Remote Control Outputs ----------------------------------------------------------------------------------------------------------------------------------- 3 Card LED support ----------------------------------------------------------------------------------------------------------------------------------- 4 Subrack LED support ----------------------------------------------------------------------------------------------------------------------------------- 5 Rack Alarm support ----------------------------------------------------------------------------------------------------------------------------------- -----------------------------------------------------------------------------------------------------------------------------------

  • Hardware and Software Requirements In order to access and retain Disclosures electronically, you must satisfy the following computer hardware and software requirements: access to the Internet; an email account and related software capable of receiving email through the Internet; a web browser which is SSL-compliant and supports secure sessions, and hardware capable of running this software.

  • Technical Specifications Each Bloom System is an integrated system comprised of a fuel cell stack assembly and associated balance of plant components that converts a fuel into electricity using electrochemical means that (i) has a Nameplate Capacity of at least 0.5 kilowatts of electricity using an electrochemical process and (ii) has an electricity-only generation efficiency greater than thirty percent (30%).

  • TECHNICAL SUPPORT SERVICES 2.1 The technical support services (the "Services"): Party A agrees to provide to Party B the relevant services requested by Party B, which are specified in Exhibit 1 attached hereto ("Exhibit 1").

  • Technical Support State Street will provide technical support to assist the Fund in using the System and the Data Access Services. The total amount of technical support provided by State Street shall not exceed 10 resource days per year. State Street shall provide such additional technical support as is expressly set forth in the fee schedule in effect from time to time between the parties (the “Fee Schedule”). Technical support, including during installation and testing, is subject to the fees and other terms set forth in the Fee Schedule.

  • Compatibility The Spacecraft Bus shall be compatible with standard GPS interfaces as defined in [**Redacted**].

  • Configuration The configuration for the Purchase Right Aircraft will be the Detail Specification for Model 767-3S2F aircraft at the revision level in effect at the time of the Supplemental Agreement. Such Detail Specification will be revised to include (i) changes required to obtain required regulatory certificates and (ii) other changes as mutually agreed upon by Boeing and Customer.

  • Measurement and Monitoring Tools As of the Effective date, Vendor and Prudential will mutually agree on the measurements and service level management procedures, pursuant to the governance procedures set forth in Attachment G and performance standards set forth in Attachment E-1 and E-2, to measure Vendor's performance of the Services against the applicable Service Levels. Such measurement and monitoring tools and procedures will (a) for Attachment E-1, be implemented upon the Effective Date; (b) for Attachment E-2, be implemented after successful completion of all testing and written acceptance by Prudential of the Transition Services set forth in Attachment B-1; (c) permit reporting at a level of detail sufficient to verify compliance with the Service Levels; and (d) be subject to audit by Prudential or its designee in accordance with the Agreement, except such audit will not include the installation of any audit software on Vendor's network.

  • Upgrades The Software includes all updates or supplements to the Software and this Section 19 applies to all such updates or supplements, unless the BNPP Entities provide other terms along with the update or supplement.

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