TNAG-2109-FCO40-3008-Outer-Space-Act-1986-extension-to-Hong-Kong-1990 — Page 87

Ľ

The

detailed dimensions of the adaptor are defined the LM-3 Users Manual, Revision 1, Section III.

in

The locations of the cable plug supports on the adapter

of on the basis

the will be determined

spacecraft orientation necessary to provide satisfactory access to the required areas using the standard access doors the fairing.

in

1

-L.

2.1.2

The

Spacecraft Volume

physical

dimensions

of the Spacecraft

compatible with the inner volume of the LM-3 See Fig. Al.1.

shall fairing.

be

encap-

LM-3 Users

The standard access doors on the fairing to the sulated

are described in the Spacecraft Manual. If non-standard doors are required, they shall be indicated in the Application to use the will be determined through negotiation prior months before launch.

LM-3 and to 13.5

......

7.

-L.

2.2

Electrical Interface

The

Spacecraft/Launch Vehicle electrical interface and

Spacecraft/Ground Checkout Facility electrical tions are specified in LM-3 Users Manual.

connec-

Two umbilical connectors are located at the aft end of the Spacecraft at 45 deg. and 225 deg. Both connectors are used to interconnect the Spacecraft with the block-

house.

Two quick disconnect connectors will be provided by the Client. The Client will provide the connectors for both the Spacecraft and Launch Vehicle sides of the inter- face.

2.3

Others

2.3.1

RF Interface

t...

The nose cone and the bicone section of the fairing are radio-transparent in the Spacecraft command and teleme- by try frequency bands with a transparency of 90% (TBD CGWIC based on RF frequency data to be AsiaSat).

2.3.2

Spacecraft Destruct System

provided

A destruct system for the Spacecraft is not required.

by

-L

ANNEX I

4