PROPULSION SUBSYSTEM Clause Samples

The Propulsion Subsystem clause defines the requirements, specifications, and responsibilities related to the design, manufacture, integration, and performance of the propulsion system within a larger project or contract, such as a spacecraft or satellite. This clause typically outlines the technical standards the propulsion subsystem must meet, the testing and acceptance procedures, and the division of tasks between the contracting parties. By clearly delineating these aspects, the clause ensures that the propulsion subsystem will function as intended and that accountability for its performance is established, thereby reducing the risk of disputes or failures related to this critical component.
PROPULSION SUBSYSTEM. [***] [The remaining 3 pages (pages 8-1 through 8-3) of this section have been omitted and filed separately with the Commission.]
View SourceView Similar (2)
PROPULSION SUBSYSTEM. 6.1 FUNCTIONAL REQUIREMENTS 6.2 PROPELLANT BUDGETS
View Source
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
View Source
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 [*] [*]
View Source

Related to PROPULSION SUBSYSTEM

  • Technical Specifications The purpose of the Technical Specifications (TS), is to define the technical characteristics of the Goods and Related Services required by the Procuring Entity. The Procuring Entity shall prepare the detailed TS consider that:

  • 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 A330-200 Aircraft as described in the Technical Specification ***, as amended by the Specification Change Notices ("SCN's") for:

  • 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.