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

Sample text

And made docking function control system designs, pro- possible° and structure is to provide control. This is: build-up control for capture upon principles The Soyuz attitude nance in- systems. it that the Soyuz and motion attitude systems electromechanic Attitude the spacecraft elements. 3 system autonomous for redundant However, of different of docking ring ex- connection. essential has electric on previous structural and guide docking with based differences system the Soyuz have considerable and utilization in manufacturing those in attenuation designs are primarily of each side specialists structural volve system of orientation specific hold with - correcting the spacecraft modes; orientation the generation propulsion rendezvous.

Radially to compen- of the structural mode, the guide ring. pin is auto- position. is also and sensors equipped indicating with docking interface the interface seal com- pression. Spri_ vide thrusters spacecraft separation Dockin_ the docking centric rubber rings to close The manhole by means chanism by means P interface of closed fails, pressure The sealing tunnel of the docking is manually being connection. connected which with In case the cover or even all hooks the mission can be opened and subsequent the Soy-am d_cking - 45 - and is performed by the has eight each other sealir_ me- or closed assembling.

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.

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