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.] Exhibit B Use or disclosure of the data contained on this sheet is subject to the restriction on the title page. TerreStar Satellite Program – Technical Specifications
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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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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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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 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%).

  • Buyer Furnished Equipment 14.3.2.1 The Seller shall introduce data related to Buyer Furnished Equipment, for equipment that is installed on the Aircraft by the Seller (hereinafter “BFE Data”) into the customized Technical Data, at no additional charge to the Buyer for the initial issue of the Technical Data provided at first Aircraft Delivery, provided such BFE Data is provided in accordance with the conditions set forth in Clauses 14.3.2.2 through 14.3.2.6.

  • 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 in Paragraphs 2 and 3 below (the “Guarantees”) are applicable to the A321 Aircraft as described in the A321 Standard Specification ***** as amended by the following SCNs:

  • Airframe The Airbus A300F4-605R aircraft (excluding the Engines or engines from time to time installed thereon) to be leased by the Lessor to the Lessee pursuant to the Lease and the initial Lease Supplement and having the United States FAA Registration Number initially and manufacturer's serial number specified in the initial Lease Supplement, including (i) all Parts in respect thereof and (ii) any Replacement Airframe which may be substituted pursuant to Section 11.03

  • Aircraft The Airframe to be sold by AVSA to the Owner Trustee as provided in the Participation Agreement and to be leased under the Lease (or any permitted substitute airframe thereunder) together with two Engines (whether either is an initial Engine or a Replacement Engine) whether or not any of such initial or Replacement Engines may from time to time be installed on such Airframe or may be installed on any other airframe or on any other aircraft, including any aircraft substituted pursuant to Section 11.03

  • Specification The Airframe shall be manufactured in accordance with the Standard Specification, as modified or varied prior to the date of this Agreement by the Specification Change Notices listed in Appendix 1 to Exhibit A.

  • Succession; Subcontractors (a) As a condition to the succession to the Master Servicer and Special Servicer or to any Sub-Servicer (but only if such Sub-Servicer is a Servicing Function Participant and a servicer as contemplated by Item 1108(a)(2)) as servicer or sub-servicer under this Agreement by any Person (i) into which the Master Servicer and Special Servicer or such Sub-Servicer may be merged or consolidated, or (ii) which may be appointed as a successor to the Master Servicer and Special Servicer or to any such Sub-Servicer, the person removing and replacing the Master Servicer and Special Servicer shall provide to the Depositor and the Certificate Administrator, at least fifteen (15) calendar days prior to the effective date of such succession or appointment (or such shorter period as is agreed to by the Depositor), (x) written notice to the Depositor of such succession or appointment and (y) in writing and in form and substance reasonably satisfactory to the Depositor, all information relating to such successor reasonably requested by the Depositor in order to comply with its reporting obligation under Item 6.02 of Form 8-K pursuant to the Exchange Act (if such reports under the Exchange Act are required to be filed under the Exchange Act); provided, however that if disclosing such information prior to such effective date would violate any applicable law or confidentiality agreement, the Master Servicer, the Special Servicer or any Additional Servicer, as the case may be, shall submit such disclosure to the Depositor no later than the first Business Day after the effective date of such succession or appointment.

  • Aircraft Documents The following documentation and information is part of the Aircraft, and is the property of the Lessor. The documentation shall be in English, complete, current, accurate and include the latest revisions, in good condition, readable and capable of being reproduced using standard reproduction processes. All documentation shall have the necessary stamps, endorsements, certifications and signatures where appropriate. Bulk storage media (microfilm, CD, DVD) shall be in an industry standard format, requiring no proprietary or “fee added” software to access. One set of any such bulk storage media or one set of paper documentation shall be provided. All records listed in this Exhibit B shall be provided notwithstanding any policies of the Aviation Authority or the Reference Regulatory Agency that may allow the disposal of such records.

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