Spacecraft Reconfiguration Sample Clauses

Spacecraft Reconfiguration. Some spacecraft have the capability to be reconfigured for different input attenuation, operation in LINEAR or LIMITER mode and/or downlink beam switching. The procedure for spacecraft reconfiguration is as follows:
Sample 1
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Spacecraft Reconfiguration. Some spacecraft have the capability to be reconfigured for different input attenuation, operation in LINEAR or LIMITER mode and/or downlink beam switching. The procedure for spacecraft reconfiguration is as follows: - The customer shall supply to the TOC a written list of the persons in their organization authorized to request the reconfigurations allowed in their contract. - These persons may contact the TOC and request a reconfiguration. The TOC will validate the request and pass it on to the TT&C controlling the spacecraft. Depending on other critical operations in progress, the TT&C will accomplish the reconfiguration as soon as possible and notify the TOC who will in turn notify the customer. - Changes from LINEAR to LIMITER or vice versa or changes to input attenuators may be requested. Switching input attenuators to 3 dB or less requires approval from GE Americom's Manager, Customer and Technical Services.
Sample 1

Related to Spacecraft Reconfiguration

  • 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.

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  • 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

  • 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 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.

  • 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%).

  • 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.

  • Spares Boeing will revise, as applicable, the customized Recommended Spares Parts List (RSPL) and Illustrated Parts Catalog (IPC).

  • Hardware and Software Requirements In order to access and retain Disclosures electronically, you must satisfy the following computer hardware and software requirements: access to the Internet; an email account and related software capable of receiving email through the Internet; a web browser which is SSL-compliant and supports secure sessions, and hardware capable of running this software.

  • Delivery Location The Aircraft shall be located at the agreed Delivery Location;

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