PROPULSION MODEL Sample Clauses

PROPULSION MODEL. The bipropellant model includes the twelve 22-N attitude control thrusters, the Main Satellite Thruster (MST), and the Stationary Plasma Thrusters (SPTs) if provided on the spacecraft. This model: 1. Calculates the forces and torques on the spacecraft created by the thruster firings 2. Models the pressures in both propellant tanks and the helium tank, and modifies the Specific Impulse (Isp) accordingly 3. Maintains the status of the propulsion system valves and their effect on the propulsion system 4. Models the thruster plume impingement forces and adjusts them as the solar array rotates 5. Updates the force/torque table as a function of thruster position and alignment and as the center of mass and solar array position changes 6. Changes the spacecraft mass properties as the propellant is consumed 7. Models behavior of the SPT gimbals and changing thrust vectors 8. Models leaky/blocked thrusters with a user-selected leak rate and blocked percentage
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PROPULSION MODEL. 4-2 4.4 T&C SUBSYSTEM MODEL.............................................4-2 4.4.1 Caribou Decryptor Modeling...........................4-3 4.5 ORBIT & EPHEMERIS MODEL.........................................4-3 4.6 EMULATION OF THE SECOND SPACECRAFT SCE PROCESSOR................4-4 4.7 DYNAMIC POWER MODEL.............................................4-4 4.8 DYNAMIC THERMAL MODEL...........................................4-4 4.9 COMMUNICATIONS PAYLOAD MODEL....................................4-5 4.10 FAILURE MODELS.................................................4-5 5 --FAST MODE SIMULATION.....................................................5-1 6 --SIMULATOR USER INTERFACE.................................................6-1 7 --POST-PROCESSING PLOTTING.................................................7-1 8 --DESIGN REVIEWS...........................................................8-1 9 --SIMULATOR TEST AND VALIDATION............................................9-1 10 --DOCUMENTATION..........................................................10-1 11 --DELIVERY AND INSTALLATION..............................................11-1 12 --TRAINING...............................................................12-1 13 --WARRANTY & MAINTENANCE.................................................13-1
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PROPULSION MODEL. T&C SUBSYSTEM MODEL *
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Related to PROPULSION MODEL

  • Model List your model number of the product you are bidding.

  • 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 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:

  • Alternate Work Schedule An alternate work schedule is any work schedule where an employee is regularly scheduled to work five (5) days per week, but the employee’s regularly scheduled two (2) days off are NOT Saturday and Sunday.

  • 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: