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Дата изменения: Unknown
Дата индексирования: Tue Oct 2 10:34:30 2012
Кодировка:

Поисковые слова: mercury program
S.P.Korolev RSC Energia - UNIVERSAL SPACE PLATFORM



 
homepage
UNIVERSAL SPACE PLATFORM

Russian
   
MAIN CHARACTERISTICS

Working orbits

Low (including SSO),
middle, HEO,
GEO

Dry space platform (SP) mass 950…1200 kg

Payload (PL) mass:

for low, middle, high-elliptical orbits
for GEO

 

500…1000 kg
250…300 kg

PL electric power:

for low, middle, high-elliptical orbits
for GEO

 

up to 3000 W
2200 W

Attitude control Three-axial
SP attitude control accuracy 3…6 min of arc

Stabilization accuracy:

- in angle
- in angular rate

 

1 min of arc
0.001...0.002 deg of arc/s

Nominal voltage 28.5 V

Flight service life

for low, middle, high-elliptical orbits
for GEO

 

at least 7 years
up to 12.5 years

SSO - Sun-synchronous orbit
HEO - High-elliptical orbit
GEO - geostationary orbit

 

 

 

 

 

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E-mail:mail@rsce.ru