PROPULSION MODEL Sample Clauses

PROPULSION MODEL. 1.5.4 T&C SUBSYSTEM MODEL *
Sample 1
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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:
Sample 1
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
Sample 1

Related to PROPULSION MODEL

  • 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.

  • 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:

  • 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%).

  • Specification Changes (a) During the Term, GSK will accept a labeling change from Prometheus as contemplated by this Section 4.2 but otherwise the Parties acknowledge and agree that GSK does not intend to make any material changes (such as packaging design, manufacturing process or similar or related changes) to the existing Product during the Term.

  • Aircraft Information Table Table 1 consolidates information contained in Articles 1, 2, 3 and 4 with respect to (i) quantity of Aircraft, (ii) applicable Detail Specification, (iii) month and year of scheduled deliveries, (iv) Aircraft Basic Price, (v) applicable escalation factors and (vi) Advance Payment Base Prices and advance payments and their schedules.

  • Aircraft Description The Option Aircraft are described by Boeing Detail Specification D6-38808, Revision E, dated September 15, 1995, as amended and revised pursuant to the Agreement.

  • 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

  • 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.

  • 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.

  • 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.

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