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Additional info for Apollo-Soyuz Test Project : information for press

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To which are attached. a flange is a structural for attachment part, forming ring, to the space- a tunnel construction with a hatch from insideo Guide rin_ three guides member The base is the pressure-tight of a cylindrical is looked structural end of the base there end of the base has and consists which base is the main is installed Supporting rods the rods The guide hollow 45° to the longitudinal ring and roll of a ring, during ring for the guide three rods, attachconnec- ring lateral degrees capture and of the docking are the kinematic attenuation(three supports axis on six supporting attachments and provide in cross-section dis_ of freedom).

Rol can also be performed The monitoring of insertion flight. The DV regenerator DV panel. only at the phase from the automatically The regenerator cont- from the DV and OM panels. of the atmosphere facilities is performed - 60 - composition by maintained two gas analyzers D installed in the Descent Vehicle When gas analyzer and the Orbital Module. 02 and CO 2 contents produces warning exceed producing installed and leakage tank designed time required is more module, it may for module for the crew pressurization to don their mixture (40% oxygen) and automatically required for the spacecraft descent A pressare unit control the module Pressure pressure two inflight bags, ment and two headsets.

Attachment - antenna which with a thrust - the small vice, on TV camera. is intended required targets are located of intermediate, section On the intermediate control mode of sections. with tanks Module consists docking of the external and equipment The intermediate hicle control antennas equipment program-timlng power supply The infra-red on the instrument de- system are orientation section sen- outer surface. The assembly which is connected section is of a cylindrical with a conical - 38 - shell which shell ends with design the base mounting ring for the spacecraft installation on the latmch-ve- hicle.

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