Difference between revisions of "Sirius-7K IDS"

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;СКД
 
;СКД
 
:Main engine
 
:Main engine
 +
;СОУД
 +
:Attitude and motion control system
  
 
==References==
 
==References==
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/soyuz7.pdf Системы отображения информации типа "Сириус" космических аппаратов "Союз-7К","Союз-А8","Союз-М",станций "ДОС-17К"]
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/soyuz7.pdf Системы отображения информации типа "Сириус" космических аппаратов "Союз-7К","Союз-А8","Союз-М",станций "ДОС-17К"]
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/analiz.pdf Анализ и синтез подсистем СОИ ПКА]
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/analiz.pdf Анализ и синтез подсистем СОИ ПКА]

Revision as of 17:44, 9 October 2010

Command/Signal instrument (CSI)

CSI - a first type of an integrated control panel. It controls guidance systems and subsystems of spacecraft 7K-OK, signalizes executed commands, monitors the state of complex systems. In the IDS Sirius-7K are two CSIs: A left CSI and a right CSI.

Command/Signal matrix (English translation)

A Б B Г Д Е Ж И К Л М Н П Р С Т
Backup
Radio
Radio D/L Landing ECLSS
DM
ECLSS
OM, PM
Airlock Docking Prepare
Reentry
Guidance
Attitude
Control
System
Navigation Program Propellant
Supply
System
Back-up
System
RTS, RKO
KM, SEP
CEI
1 2 Prepare
UHF XMTR
I
Modulation
HF and UHF
АСП Light I Guide
from DM
Prepare
RDZ
Select
ДПО
Cancel
Mode
Manual
Control
Cancel
program
RCS
tanks
Habitat
Systems
RTS, RKO CEI
3 4 Prepare
UHF XMTR
II
Back-up UHF
antenna
Air supply
Valve
Light II Dryer Supply
interface
Retract
Probe (?)
Select
ДО
DU Orbit
maneuver
ДО nozzle Propulsion
System
Back-up
Antenna I
Air
assembly
5 6 UHF RVR
Simplex
Dynamic
OM
XMTR mode
Voice / Recorder
Transfer
light
Reduce
Press. in
OM
Manual docking Indicator
mode
RO βс Approach "IE" Supply ДО Sealed
Enclosure
A / B
Antenna II
7 8 UHF RCVR
Duplex
Microphone Transmit ??????
Light Ctrl.
PO Valve Egress
Hatch
open
Lateral
offset
connection
ИД разг.тор Pulsed RO γс Automated
deorbit
Pressurize
ДО
PTD
P gr
Matrix I Off Fast pitch
9 10 Prepare
HF XMTR II
Pyro-String I Gas analysis AC
OM
Basic
press.
open
TV Camera
A
Pitch
forward
IO αх Deorbit
by RO
Supply
ДПО
Television Matrix II Off Peroxide
ДПО
11 12 Prepare
HF XMTR I
Pyro-String II Dehumidify Inner Pump Tank
press.
open
TV Camera
B
Pitch
backward
Sun
tracking
СКД
impulse
Automatic
Maneuver
Pressurize
ДПО
Power СОУД VKIP off
13 14 Frequency
HF XMTR I
Telegraph Pyro-String
ЗСП
Dryer Outer Pump I TV Camera OM TV scale
Fluid/Manual
Visor
attitude
Manual
input
Maneuver
with RO
Engine Generator
setting
Solar battery
off

Combined Electronic Indicator (CEI)

Acronyms

АСП
Automatic landing program
ДО
10N attitude control vernier thrusters.
ДПО
100N attitude control and maneuvering thrusters.
ЗСП
Reserve parachute
СКД
Main engine
СОУД
Attitude and motion control system

References