Amos 2
Launch originally planned on Ariane but it couldn't wait till a launch slot was
available. It was therefore transfered on Soyuz-Fregat.
Begin
|
End
|
Position
|
L:
Jan 2004
|
Oct
2016
|
4°W
|
Oct
2016
|
Apr
2017
|
4°W,
inclined
|
Out
of service
|
April
2017
|
Cause
|
Sent
to junk orbit
|
sat-index articles
Lyngsat
transponder loading
Central Europe & Middle East
US
Prime
contractor
|
Israel
Aircraft Industries (IAI)
|
Platform
|
AMOS
|
Mass
at launch
|
1370
kg
|
Dry
mass
|
646
kg
|
Dimension
|
2.7
x 2.06 x 2.38 m
|
Solar
array
|
11.03
m
|
Stabilization
|
3-axis
|
DC
power
|
EOL:
1900 W
|
Design
lifetime
|
12
years
|
Payload built by Alenia Spazio.
Main
transponders
|
11
|
Backup
transponders
|
3 |
Power
|
75
W
|
Bandwidth
|
72
MHz
|
Coverage
& EIRP max
|
Central Europe:
57 dBW
Middle East:
57 dBW
US:
52 dBW
|
G/T
max
|
Europe:
14.5 dB/K
Middle East: 15 dB/K
US: 9 dB/K
|
Polarization
|
linear
H/V crossed
|
Vertical
Downlink
|
Transponder
|
Horizontal
Downlink
|
Uplink
from
|
|
28
|
11.45-11.7
|
19
|
|
29
|
11.45-11.7
|
20
|
|
30
|
11.45-11.7
|
21
|
Vertical
Downlink
|
Transponder
|
Horizontal
Downlink
|
Uplink
from
|
|
22
|
10.7-10.95
|
22
or 122
|
|
23
|
10.7-10.95
|
23
or 123
|
|
24
|
10.7-10.95
|
24
or 124
|
|
25
|
11.45-11.7
|
25
or 125
|
|
26
|
11.45-11.7
|
26
or 126
|
|
27
|
11.45-11.7
|
27
or 127
|
Vertical
Downlink
|
Transponder
|
Horizontal
Downlink
|
Uplink
from
|
10.7-10.95
|
11
|
|
11
or 111
|
10.7-10.95
|
12
|
|
12
or 112
|
10.7-10.95
|
13
|
|
13
or 113
|
10.95-11.2
|
14'
|
10.95-11.2
|
14'
(dual polarisation)
|
10.95-11.2
|
15'
|
10.95-11.2
|
15'
(dual polarisation)
|
11.2-11.45
|
16
|
|
16
|
11.2-11.45
|
17
|
|
17
or 117
|
11.2-11.45
|
18
|
|
18
or 118
|
|
19
|
11.45-11.7
|
19
or 119
|
|
20
|
11.45-11.7
|
20
or 120
|
|
21
|
11.45-11.7
|
21
or 121
|