TNAG-2109-FCO40-3008-Outer-Space-Act-1986-extension-to-Hong-Kong-1990 — Page 93

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1.3

1.4

1.3.1

1.3.2

Mission Analysis

Trajectories up to injection

Separation analysis

1.3.3

Orbit characteristics and dispersion

1.3.4

Dynamic coupled analysis

NOTE:

1.3.5

NOTE:

1.3.6

It may be required that the Client perform the dynamic dynamic coupled analysis or that the coupled analysis be performed in part by Client and in part by CGWIC.

the The Client and

cooperate

as

that they will agree CGWIC necessary to ensure that the analysis verifies that the LM-3 flight environment satisfies the environmental limits to which the Spacecraft for responsibility has been verifying that the flight environment will be suitable for the Spacecraft shall remain with

CGWIC.

The designed.

Thermal coupled analysis

environment

It may be required that the Client perform the thermal analysis or that the thermal analysis be performed in part by the Client and in part by CGWIC. The Client and CGWIC agree that they that ensure will cooperate as necessary to

satisfies the the LM-3 flight environmental limits to which the Spacecraft for The responsibility been designed.

that the flight environment will be suitable for the Spacecraft shall remain CGWIC.

has

verifying

Radio frequency compatibility analysis

with

Transport

t

1

!

1.4.1

Launch

shipment to Xichang.

and Vehicle

its support equipment

without inspection

1.4.2 Obtaining customs clearance and asistance with arranging transportation between the port of entry and the Xichang airport for the Space- and between the port craft and its support equipment;

entry and XSLC for the spacecraft propellants return).

(and

f

ANNEX II

2

B $