PROPULSION SUBSYSTEM Sample Clauses

PROPULSION SUBSYSTEM. [***] [The remaining 3 pages (pages 8-1 through 8-3) of this section have been omitted and filed separately with the Commission.]
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PROPULSION SUBSYSTEM. 4-10 4.6.1 Qualification..........................................4-10 4.6.2 Acceptance Testing.....................................4-10 4.7 SOLAR ARRAY.....................................................4-10 4.7.1 Solar Panel Coupon Qualification.......................4-10 4.7.1 Solar Panel Coupon Qualification.......................4-11 4.7.2 Acceptance Testing.....................................4-11 4.7.2 Acceptance Testing.....................................4-12 4.8 ELECTRICAL POWER SUBSYSTEM......................................4-13 4.8.1 Qualification..........................................4-13 4.8.2 Protoflight and Acceptance.............................4-13 4.9 SPACECRAFT CONTROL ELECTRONICS SUBSYSTEM........................4-14 4.10 THERMAL CONTROL SUBSYSTEM.......................................4-14 4.11 STRUCTURE SUBSYSTEM.............................................4-14 4.11.1 Qualification..........................................4-14 4.11.2 Protoflight and Acceptance Tests.......................4-14 4.12
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PROPULSION SUBSYSTEM. 6.1 FUNCTIONAL REQUIREMENTS 6.2 PROPELLANT BUDGETS
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PROPULSION SUBSYSTEM. The satellite propulsion subsystem shall include all components and assemblies associated with storing, conditioning, routing, controlling, and expelling propellant, as required to change the satellite’s attitude and angular or linear velocity. The propulsion subsystem includes all propulsion hardware and propellants required to achieve placement into geosynchronous orbit from the geo-transfer orbit existing at separation from the launch vehicle. Liquid bi-propellant thrusters shall be utilized during the various operational phases following separation from the launch vehicle until the end of mission life including all major velocity maneuvers, apogee injection, and final de-orbit maneuver. It shall be possible to restart and operate any thruster at any time required for the mission with no thermal constraints. [*] [*] CONFIDENTIAL TREATMENT REQUESTED BY ICO GLOBAL COMMUNICATIONS (HOLDINGS) LIMITED. Propellant and gas leaks shall be minimized consistent with the satellite orbit lifetime. It shall be possible to predict depletion of the propellant at 15 years after beginning of life to an accuracy of [*] [*]
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Related to PROPULSION SUBSYSTEM

  • Aircraft Basic Price The Aircraft Basic Price is listed in Table 1 and is subject to escalation in accordance with the terms of this Purchase Agreement.

  • Technical Specifications The Technical Specifications furnished on the CD are intended to establish the standards for quality, performance and technical requirements for all labor, workmanship, material, methods and equipment necessary to complete the Work. When specifications and drawings are provided or referenced by the County, these are to be considered part of the Scope of Work, and to be specifically documented in the Detailed Scope of Work. For convenience, the County supplied specifications, if any, and the Technical Specifications furnished on the CD.

  • Engines POSITION SERIAL NO. TOTAL HOURS TOTAL CYCLES HRS/CYCLES SINCE LAST SHOP VISIT Time Remaining to Next LIFE LIMITED PART REMOVAL PART NAME HOURS CYCLES MSN MSN

  • AIRCRAFT CONFIGURATION The guarantees defined below (the “Guarantees”) are applicable to the A319-100 Aircraft as described in the Standard Specification Ref. J 000 01000 Issue 6 dated 1st March 2007 equipped with:

  • Engine A. Any internal repairs or replacement of internal components, or replacement of engine assembly.

  • DAF Specifications Developer shall submit initial specifications for the DAF, including System Protection Facilities, to Connecting Transmission Owner and NYISO at least one hundred eighty (180) Calendar Days prior to the Initial Synchronization Date; and final specifications for review and comment at least ninety (90) Calendar Days prior to the Initial Synchronization Date. Connecting Transmission Owner and NYISO shall review such specifications to ensure that the DAF are compatible with the technical specifications, operational control, and safety requirements of the Connecting Transmission Owner and NYISO and comment on such specifications within thirty (30) Calendar Days of Developer’s submission. All specifications provided hereunder shall be deemed to be Confidential Information.

  • Loop Provisioning Involving Integrated Digital Loop Carriers 2.6.1 Where Xxxx has requested an Unbundled Loop and BellSouth uses IDLC systems to provide the local service to the End User and BellSouth has a suitable alternate facility available, BellSouth will make such alternative facilities available to Xxxx. If a suitable alternative facility is not available, then to the extent it is technically feasible, BellSouth will implement one of the following alternative arrangements for Xxxx (e.g. hairpinning): 1. Roll the circuit(s) from the IDLC to any spare copper that exists to the customer premises. 2. Roll the circuit(s) from the IDLC to an existing DLC that is not integrated. 3. If capacity exists, provide "side-door" porting through the switch. 4. If capacity exists, provide "Digital Access Cross Connect System (DACS)- door" porting (if the IDLC routes through a DACS prior to integration into the switch). 2.6.2 Arrangements 3 and 4 above require the use of a designed circuit. Therefore, non- designed Loops such as the SL1 voice grade and UCL-ND may not be ordered in these cases. 2.6.3 If no alternate facility is available, and upon request from Xxxx, and if agreed to by both Parties, BellSouth may utilize its Special Construction (SC) process to determine the additional costs required to provision facilities. Xxxx will then have the option of paying the one-time SC rates to place the Loop.

  • ODUF Packing Specifications 6.3.1 A pack will contain a minimum of one message record or a maximum of 99,999 message records plus a pack header record and a pack trailer record. One transmission can contain a maximum of 99 packs and a minimum of one pack.

  • Equipment Specifications All equipment must meet the contract specifications and all federal and State safety codes and regulations in effect at the date of manufacture. All equipment must be Original Equipment Manufacturer (OEM) equipment unless otherwise stated in the contract. All products, materials, supplies, replacement parts, and equipment offered and furnished must be new, of current manufacturer production, and must have been formally announced by the manufacturer as being commercially available, unless otherwise stated in this Contract.

  • Aircraft This peril includes self-propelled missiles and spacecraft.

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