Russian

Sea Launch Project

Main Performances


Factor Name Value
The mass of spacecraft (in tons), that are put into:
  • geostationary orbit
  • GEO transfer orbit
    (Hapogee=36000 km) (i=0deg)
  • medium circular orbits
    (Hcircle=10000 km, i=45deg)
  • medium low Earth orbit
    (Hperigee=200 km Hapogee=36000 km) with inclinations
    i = 45deg
    i = 90deg


up to 2.9

up to 5.7

up to 3.75


4.75
3.6
Number of launches per year
6 - 8
Time between signing the contract with the SC Customer and the launch
12 - 18 months
Probability of failure-free operation of the launcher
no less than 0.95
Coordinates of the main launch site
0degS, 154degW

 

News Archive

March  2017
Mon Tue Wed Thu Fri Sat Sun
    1 2 3 4 5
6 7 8 9 10 11 12
13 14 15 16 17 18 19
20 21 22 23 24 25 26
27 28 29 30 31