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Information message about launch progress
"Proton-M", "Breeze-M", "NSS-14"
Document: 11. Total: 12
Create: 15.02.2012 10:19:55 (MDT)
Summary SC launch information
¹ |
Event of flight cyclogram |
Predicted flight time |
Data |
Measuring values |
||
[h:m:s from L-OC] |
[s from L-OC] |
time [s from L-OC] |
deviation [s] |
|||
1 |
Gyroplatform activation end |
-00:00:05.000 |
-5.000 |
Proton-M |
-5.000 |
0.000 |
2 |
SE1 ignition |
-00:00:01.750 |
-1.750 |
Proton-M |
-1.756 |
0.006 |
3 |
Lift-off contact |
00:00:00.000 |
0.000 |
Proton-M |
0.079 |
0.079 |
4 |
SE2 ignition |
00:01:55.377 |
115.377 |
Proton-M |
114.865 |
0.512 |
5 |
Stage 1-2 separation |
00:01:59.627 |
119.627 |
Proton-M |
120.305 |
0.678 |
6 |
VE3 ignition |
00:05:23.781 |
323.781 |
Proton-M |
325.367 |
1.586 |
7 |
SE2 burnout |
00:05:26.481 |
326.481 |
Proton-M |
328.087 |
1.606 |
8 |
Stage 2-3 separation |
00:05:27.181 |
327.181 |
Proton-M |
328.808 |
1.627 |
9 |
SE3 ignition |
00:05:29.581 |
329.581 |
Proton-M |
329.594 |
0.013 |
10 |
HF jettison |
00:05:44.982 |
344.982 |
Proton-M |
346.568 |
1.586 |
11 |
Fairing jettison indication |
00:05:46.883 |
346.883 |
Proton-M |
346.666 |
0.217 |
12 |
Preliminary command |
00:09:30.131 |
570.131 |
Proton-M |
572.339 |
2.208 |
13 |
Main command |
00:09:42.058 |
582.058 |
Proton-M |
582.989 |
0.931 |
14 |
OU separation |
00:09:42.222 |
582.222 |
Proton-M |
583.120 |
0.898 |
15 |
US ICE 1- ignition |
00:11:22.222 |
682.222 |
Breeze-M |
683.541 |
1.319 |
16 |
US SE 1- ignition |
00:11:36.222 |
696.222 |
Breeze-M |
697.696 |
1.474 |
17 |
US ICE 1- burnout |
00:11:38.122 |
698.122 |
Breeze-M |
699.531 |
1.409 |
18 |
US SE 1- burnout |
00:16:07.474 |
967.474 |
Breeze-M |
965.607 |
1.867 |
19 |
US ICE 2- ignition |
01:07:13.000 |
4033.000 |
Breeze-M |
4033.217 |
0.217 |
20 |
US SE 2- ignition |
01:07:33.000 |
4053.000 |
Ball center |
4053.139 |
0.139 |
21 |
US ICE 2- burnout |
01:07:34.900 |
4054.900 |
Breeze-M |
4055.237 |
0.337 |
22 |
US SE 2- burnout |
01:25:16.816 |
5116.816 |
Breeze-M |
5106.172 |
10.644 |
23 |
US ICE 3- ignition |
03:27:53.000 |
12473.000 |
Breeze-M |
12473.205 |
0.205 |
24 |
US SE 3- ignition |
03:28:07.000 |
12487.000 |
Ball center |
12497.321 |
10.321 |
25 |
US ICE 3- burnout |
03:28:18.900 |
12498.900 |
Breeze-M |
12499.157 |
0.257 |
26 |
US SE 3- burnout |
03:39:20.029 |
13160.029 |
Ball center |
13158.711 |
1.318 |
27 |
US ICE 4- ignition |
03:40:04.229 |
13204.229 |
Breeze-M |
13203.014 |
1.215 |
28 |
APT separation |
03:40:10.029 |
13210.029 |
Breeze-M |
13208.879 |
1.150 |
29 |
US ICE 4- burnout |
03:40:12.229 |
13212.229 |
Breeze-M |
13211.140 |
1.089 |
30 |
US ICE 5- ignition |
03:41:29.029 |
13289.029 |
Breeze-M |
13289.259 |
0.230 |
31 |
US SE 4- ignition |
03:41:37.029 |
13297.029 |
Ball center |
13297.385 |
0.356 |
32 |
US ICE 5- burnout |
03:41:38.929 |
13298.929 |
Breeze-M |
13299.221 |
0.292 |
33 |
US SE 4- burnout |
03:47:54.925 |
13674.925 |
Breeze-M |
13671.989 |
2.936 |
34 |
US ICE 6- ignition |
08:53:00.000 |
31980.000 |
Breeze-M |
31980.126 |
0.126 |
35 |
US SE 5- ignition |
08:53:20.000 |
32000.000 |
Breeze-M |
32000.311 |
0.311 |
36 |
US ICE 6- burnout |
08:53:21.900 |
32001.900 |
Breeze-M |
32002.146 |
0.246 |
37 |
US SE 5- burnout |
08:59:10.352 |
32350.352 |
Breeze-M |
32349.749 |
0.603 |
38 |
"NSS-14" SC separation |
09:12:00.000 |
33120.000 |
Breeze-M |
33105.314 |
14.686 |
39 |
US ICE 7- ignition |
11:16:40.000 |
40600.000 |
Breeze-M |
40600.207 |
0.207 |
40 |
US ICE 7- burnout |
11:16:52.000 |
40612.000 |
Breeze-M |
40612.266 |
0.266 |
41 |
US ICE 8- ignition |
12:36:40.000 |
45400.000 |
No date |
||
42 |
US ICE 8- burnout |
12:38:20.000 |
45500.000 |
No date |
||
Used abbreviations:
| APT | - Additional propellant tank | ETC | - Engine thrust control | ||
| F | - Fuel | GS | - Gyro Settings | ||
| GTSV | - Ground Tracking Stations Visibility | ||||
| HF | - Head fairing | ICE | - US impulse correction engine | ||
| L-OC | - Lift-Off contact | MC | - Main command | ||
| MDT | - Moscow Decree time | ND | - Nominal duty | ||
| NTL | - Nomihal thrust level | O | - Oxidant | ||
| ODCC | - Onboard digital computer complex | OU | - Orbital unit | ||
| PC | - Preliminary command | PU | - Propulsion unit | ||
| SC | - Spacecraft | SHU | - Spacehead unit | ||
| SE | - Sustainer engine | SEU | - Sustainer engine unit | ||
| StE | - Stabilization engine | US | - Upper stage | ||
| UTC | - Universal Coordinated Time | VE | - Vernier engine |
Sub-orbital trajectory.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 14.02.2012 22:46:19 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:21:16.8 |
1:21:16.8 |
0:0:0.0 |
----------- |
------------------- |
2 |
a [km] |
6215.57 |
6215.57 |
0.00 |
----------- |
------------------- |
3 |
e |
0.0535669 |
0.0535623 |
0.0000046 |
----------- |
------------------- |
4 |
i |
51 °32 '31 " |
51 °32 '52 " |
0 °0 '22 " |
----------- |
------------------- |
5 |
Hp [km] |
-495.51 |
-495.48 |
0.03 |
----------- |
------------------- |
6 |
Ha [km] |
170.39 |
170.36 |
0.03 |
----------- |
------------------- |
Parking orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 14.02.2012 22:52:54 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:27:59.0 |
1:27:59.2 |
0:0:0.3 |
----------- |
------------------- |
2 |
a [km] |
6552.79 |
6553.00 |
0.21 |
----------- |
------------------- |
3 |
e |
0.0000685 |
0.0000001 |
0.0000684 |
----------- |
------------------- |
4 |
i |
51 °32 '50 " |
51 °33 '13 " |
0 °0 '23 " |
----------- |
------------------- |
5 |
Hp [km] |
174.21 |
174.86 |
0.66 |
----------- |
------------------- |
6 |
Ha [km] |
175.11 |
174.86 |
0.24 |
----------- |
------------------- |
Intermediate orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2012 00:02:03 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:21:53.9 |
2:21:55.6 |
0:0:1.7 |
----------- |
------------------- |
2 |
a [km] |
9011.81 |
9013.00 |
1.19 |
----------- |
------------------- |
3 |
e |
0.2623792 |
0.2623987 |
0.0000195 |
----------- |
------------------- |
4 |
i |
50 °19 '27 " |
50 °18 '0 " |
0 °1 '27 " |
----------- |
------------------- |
5 |
Hp [km] |
269.17 |
269.86 |
0.70 |
----------- |
------------------- |
6 |
Ha [km] |
4998.19 |
4999.86 |
1.67 |
----------- |
------------------- |
Transfer orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2012 02:24:41 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
10:35:11.9 |
10:35:56.3 |
0:0:44.4 |
----------- |
------------------- |
2 |
a [km] |
24477.48 |
24496.49 |
19.00 |
----------- |
------------------- |
3 |
e |
0.7218737 |
0.7220826 |
0.0002089 |
----------- |
------------------- |
4 |
i |
49 °5 '57 " |
49 °6 '0 " |
0 °0 '3 " |
----------- |
------------------- |
5 |
Hp [km] |
429.70 |
429.86 |
0.17 |
----------- |
------------------- |
6 |
Ha [km] |
35769.00 |
35806.84 |
37.84 |
----------- |
------------------- |
"NSS-14" target orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2012 07:35:57 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
11:38:30.4 |
11:40:31.8 |
0:2:1.4 |
----------- |
------------------- |
2 |
a [km] |
26077.98 |
26128.31 |
50.33 |
----------- |
------------------- |
3 |
e |
0.6154007 |
0.6137287 |
0.0016720 |
----------- |
------------------- |
4 |
i |
24 °32 '14 " |
24 °36 '11 " |
0 °3 '57 " |
----------- |
------------------- |
5 |
Hp [km] |
3651.44 |
3714.48 |
63.04 |
----------- |
------------------- |
6 |
Ha [km] |
35748.25 |
35785.86 |
37.61 |
----------- |
------------------- |
Used abbreviations and notation:
| MBC - Main Ballistic Center |
| SDO MEI - Special Design Office MEI |
| SSC - Space Surveillance Center |
| T - orbital period |
| a - semi-major axis |
| e - eccentricity |
| i - inclination |
| Hp - perigee altitude |
| Ha - apogee altitude |
Screen shots:
|
1-st stage separation |
|
First stage impact area |
|
2-nd stage separation |
|
HF jettison |
|
Second stage and HF impact area |
|
US separation |
|
End of booster phase |
|
End of booster phase |
|
End of booster phase |
|
End of booster phase |
|
US main engine action 1-st ign. (ICE) |
|
US main engine action (1-st ign.) |
|
US main engine action (2-nd ign.) |
|
US main engine action (3-rd ign.) |
|
APT separation |
|
US main engine action (4-th ign.) |
|
US main engine action (5-th ign.) |
|
SC separation |
|
SC separation |
|
SC separation |
|
US withdrawel |