|
Accuracy of SC Launches to Geostationary
Transfer Orbit and High Elliptical Orbit Using DM Type Upper
Stage For a Period Since 1996.
Controlled parameters of target orbits:
| р - SC orbital period; |
w - argument of perigee; |
Ha - apogee
altitude; |
| Е - eccentricity of orbit; |
W - longitude of
ascending node; |
мp - perigee
altitude. |
i - inclination of orbit to
the
equator plane; |
l - geographical
longitude of injection point; |
|
|
SC Type and Launch Date |
Parameters |
| Dр, Я |
De |
Di,ang. Min. |
Dw,ang. Min. |
DW,ang. Min. |
Dl,ang. Min. |
DHa,
km |
Dмp,
km |
| |
Customer
Requirements of 3 sigma |
| ±550 |
±0.009 |
±45 |
±60 |
±60 |
±60 |
±150 |
±392 |
|
Astra 1F
09.04.96
|
- |
- |
3.7 |
21.3 |
- |
-
|
3.6 |
-22.7 |
Telstar-5
24.05.97 |
- |
- |
-0.7 |
0.6 |
- |
- |
11.5 |
16.2 |
PanAmSat 5
(PAS-5)
28.08.97 |
-13.8 |
-0.0003 |
1.9 |
2.9 |
-3.9 |
- |
-16.2 |
2.5 |
Astra 1G
03.12.97 |
26.6 |
0.0002 |
-2.5 |
-1.8 |
4.2 |
- |
20 |
-2 |
EchoStar IV
08.05.98 |
- |
- |
-1.4 |
1.8 |
- |
6.0 |
-36 |
-32 |
Astra 2ю
30.08.98 |
27 |
-0.0003 |
2.5 |
5.5 |
-2.4 |
- |
7 |
11 |
PanAmSat 8 (PAS-8)
04.11.98 |
- |
- |
-0.58 |
-18.5 |
- |
- |
120 |
33 |
Telstar-6
15.02.99 |
- |
- |
6.4 |
1.49 |
- |
- |
-16 |
1.0 |
AsiaSat 3я
21.03.99 |
-11 |
0 |
4.0 |
-0.4 |
0.4 |
- |
-6.4 |
-6.0 |
Nimiq
21.05.99 |
- |
- |
-0.5 |
-3.2 |
- |
- |
2.0 |
-20.0 |
Astra 1м
18.06.99 |
34 |
-0.0004 |
0.7 |
-4.3 |
5.2 |
- |
10.0 |
15.0 |
LMI
27.09.99 |
- |
- |
-7.3 |
7.9 |
- |
3.3 |
-4.0 |
-17.0 |
Garuda
12.02.00 |
- |
- |
-0.4 |
-2.3 |
-0.5 |
-3.4 |
7.0 |
8.0 |
Sirius-1
01.07.00 |
- |
- |
-0.7 |
-0.3 |
- |
1.5 |
-27.0 |
0.9 |
Sirius-2
05.09.00 |
- |
- |
2.0 |
0.1 |
- |
0.3 |
-69.2 |
0.1 |
GE-1A
02.10.00 |
- |
- |
-4.2 |
-11.8 |
- |
0.4 |
-2.4 |
-38.4 |
GE-6
| |
