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 |