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The security procedures specified in this Agreement supplement the procedures detailed in the technology control plans in the contracts regarding the launch of the Aussat and Asiasat satellites between the consignee and China Great Wall Industry Corporation (CGWIC) (hereinafter the "Hughes - CGWIC Plan"). Compliance with both this government-to-government Agreement and the Hughes-CGWIC plan is required. Any conflict between the provisions of this Agreement and the provisions of the Hughes-CGWIC Plan will be resolved in favor of this Agreement. If the Government of the United States of America determines that there is clear evidence that any provisions of either this Agreement or the technology control plan between Hughes and CGWIC have been violated, it may suspend or revoke the export license(s). Furthermore, nothing in this Agreement should be construed το I can that the Government of the United States of America will be constrained from taking any action on the license(s) consistent with United States laws and regulations. Nevertheless, the Government of the United States of America will do its utmost to assure
continuity transaction covered by the license(s). In the event the license(s) are revoked, the Government of the People's Republic of China agrees to cooperate in the return of any equipment and technical data that was transferred prior to revocation.
of the license(s) and completion of the
II.
AUTHORIZED TECHNICAL DATA
public domain
Disclosure of technical data by the consignee will be limited to
information,
information essential to the fulfillment of contractually designated tasks, and will be limited, additionally, to the interface information specified below.
Disclosure of technical data controlled by the Government of the United States of America will be limited only to the interface information specified below. No additional controlled technical data or other information will be disclosed without thre prior written approval of the Government of the United States of America. Only the following interface form, fit, and function data that describes mechanical and electrical mating requirements for attaching the spacecraft to the launch vehicle is authorized for ' release:
orbit requirements; launch window; weight; center of gravity; envelope; dynamic loading; power usage/conditioning; interface adaptor requirements; environmental requirements; propellant requirements; frequency plans, including telemetry, tracking & control (TT&C); safety plans; test flows; separation
characteristics;
handling/te:
ground
equipment; and test/flight event sequences.
leesy