Difference between revisions of "Sirius-7K IDS"
Jump to navigation
Jump to search
m |
|||
Line 174: | Line 174: | ||
|} | |} | ||
+ | ==Combined Electronic Indicator (CEI)== | ||
+ | |||
+ | ==Acronyms== | ||
;ДО | ;ДО | ||
:10N attitude control vernier thrusters. | :10N attitude control vernier thrusters. | ||
Line 182: | Line 185: | ||
;СКД | ;СКД | ||
:Main engine | :Main engine | ||
− | |||
− | |||
− | |||
==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 12:03, 8 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 |
БАКИ? ДО |
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 |
Feed SOUD | 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
- ДО
- 10N attitude control vernier thrusters.
- ДПО
- 100N attitude control and maneuvering thrusters.
- ЗСП
- Reserve parachute
- СКД
- Main engine