K H R U N I C H E V T E L E C O M C o m p a n y Launch information processing and display center |
Information message about launch progress
"Proton-M", "Breeze-M", "Echostar-16"
Document: 11. Total: 12
Create: 21.11.2012 08:00:51 (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 |
0.000 |
0.000 |
4 |
SE2 ignition |
00:01:55.377 |
115.377 |
Proton-M |
114.636 |
0.741 |
5 |
Stage 1-2 separation |
00:01:59.627 |
119.627 |
Proton-M |
119.781 |
0.154 |
6 |
VE3 ignition |
00:05:23.781 |
323.781 |
Proton-M |
323.794 |
0.013 |
7 |
SE2 burnout |
00:05:26.481 |
326.481 |
Proton-M |
326.514 |
0.033 |
8 |
Stage 2-3 separation |
00:05:27.181 |
327.181 |
Proton-M |
327.235 |
0.054 |
9 |
SE3 ignition |
00:05:29.581 |
329.581 |
Proton-M |
329.660 |
0.079 |
10 |
HF jettison |
00:05:44.556 |
344.556 |
Proton-M |
344.569 |
0.013 |
11 |
Fairing jettison indication |
00:05:46.457 |
346.457 |
Proton-M |
344.667 |
1.790 |
12 |
Preliminary command |
00:09:30.131 |
570.131 |
Proton-M |
570.767 |
0.636 |
13 |
Main command |
00:09:42.058 |
582.058 |
Proton-M |
582.203 |
0.145 |
14 |
OU separation |
00:09:42.222 |
582.222 |
Proton-M |
582.334 |
0.112 |
15 |
US ICE 1- ignition |
00:11:02.222 |
662.222 |
Breeze-M |
662.635 |
0.413 |
16 |
US SE 1- ignition |
00:11:16.222 |
676.222 |
Ball center |
676.790 |
0.568 |
17 |
US ICE 1- burnout |
00:11:18.122 |
678.122 |
Breeze-M |
678.625 |
0.503 |
18 |
US SE 1- burnout |
00:18:52.071 |
1132.071 |
Ball center |
1121.910 |
10.161 |
19 |
US ICE 2- ignition |
01:07:20.000 |
4040.000 |
No date |
||
20 |
US SE 2- ignition |
01:07:43.000 |
4063.000 |
Ball center |
4063.400 |
0.400 |
21 |
US ICE 2- burnout |
01:07:44.900 |
4064.900 |
Breeze-M |
4065.264 |
0.364 |
22 |
US SE 2- burnout |
01:25:24.913 |
5124.913 |
Ball center |
5113.300 |
11.613 |
23 |
US ICE 3- ignition |
03:27:40.000 |
12460.000 |
No date |
||
24 |
US SE 3- ignition |
03:28:06.000 |
12486.000 |
Ball center |
12486.377 |
0.377 |
25 |
US ICE 3- burnout |
03:28:07.900 |
12487.900 |
Breeze-M |
12488.213 |
0.313 |
26 |
US SE 3- burnout |
03:37:43.972 |
13063.972 |
Ball center |
13063.356 |
0.616 |
27 |
US ICE 4- ignition |
03:38:28.172 |
13108.172 |
No date |
||
28 |
APT separation |
03:38:33.972 |
13113.972 |
Ball center |
13113.262 |
0.710 |
29 |
US ICE 4- burnout |
03:38:36.172 |
13116.172 |
Breeze-M |
13115.523 |
0.649 |
30 |
US ICE 5- ignition |
03:39:52.972 |
13192.972 |
No date |
||
31 |
US SE 4- ignition |
03:40:00.972 |
13200.972 |
Ball center |
13201.244 |
0.272 |
32 |
US ICE 5- burnout |
03:40:02.872 |
13202.872 |
Breeze-M |
13203.341 |
0.469 |
33 |
US SE 4- burnout |
03:47:36.816 |
13656.816 |
Ball center |
13653.180 |
3.636 |
34 |
US ICE 6- ignition |
08:54:00.000 |
32040.000 |
Breeze-M |
32040.157 |
0.157 |
35 |
US SE 5- ignition |
08:54:20.000 |
32060.000 |
Breeze-M |
32060.146 |
0.146 |
36 |
US ICE 6- burnout |
08:54:21.900 |
32061.900 |
Breeze-M |
32062.243 |
0.343 |
37 |
US SE 5- burnout |
08:58:56.124 |
32336.124 |
Breeze-M |
32335.135 |
0.989 |
38 |
"Echostar-16" SC separation |
09:12:00.000 |
33120.000 |
Breeze-M |
33105.904 |
14.096 |
39 |
US ICE 7- ignition |
09:51:40.000 |
35500.000 |
Breeze-M |
35500.065 |
0.065 |
40 |
US ICE 7- burnout |
09:51:52.000 |
35512.000 |
Breeze-M |
35512.189 |
0.189 |
41 |
US ICE 8- ignition |
10:26:40.000 |
37600.000 |
Breeze-M |
37600.428 |
0.428 |
42 |
US ICE 8- burnout |
10:28:20.000 |
37700.000 |
Breeze-M |
37700.502 |
0.502 |
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) - 20.11.2012 21:40:42 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:17:46.7 |
1:17:46.7 |
0:0:0.0 |
----------- |
------------------- |
2 |
a [km] |
6035.81 |
6035.77 |
0.04 |
----------- |
------------------- |
3 |
e |
0.0868478 |
0.0868057 |
0.0000422 |
----------- |
------------------- |
4 |
i |
51 °32 '41 " |
51 °32 '40 " |
0 °0 '1 " |
----------- |
------------------- |
5 |
Hp [km] |
-866.53 |
-866.31 |
0.22 |
----------- |
------------------- |
6 |
Ha [km] |
181.87 |
181.57 |
0.30 |
----------- |
------------------- |
Parking orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 20.11.2012 21:50:02 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:28:2.0 |
1:28:1.7 |
0:0:0.3 |
----------- |
------------------- |
2 |
a [km] |
6555.26 |
6555.00 |
0.26 |
----------- |
------------------- |
3 |
e |
0.0001097 |
0.0000002 |
0.0001094 |
----------- |
------------------- |
4 |
i |
51 °33 '8 " |
51 °33 '23 " |
0 °0 '15 " |
----------- |
------------------- |
5 |
Hp [km] |
176.41 |
176.86 |
0.46 |
----------- |
------------------- |
6 |
Ha [km] |
177.84 |
176.86 |
0.98 |
----------- |
------------------- |
Intermediate orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 20.11.2012 22:56:34 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:21:51.1 |
2:21:54.9 |
0:0:3.8 |
----------- |
------------------- |
2 |
a [km] |
9009.80 |
9012.50 |
2.70 |
----------- |
------------------- |
3 |
e |
0.2624316 |
0.2624685 |
0.0000369 |
----------- |
------------------- |
4 |
i |
50 °20 '10 " |
50 °17 '60 " |
0 °2 '10 " |
----------- |
------------------- |
5 |
Hp [km] |
267.21 |
268.87 |
1.66 |
----------- |
------------------- |
6 |
Ha [km] |
4996.12 |
4999.86 |
3.74 |
----------- |
------------------- |
Transfer orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 21.11.2012 01:18:46 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
10:35:35.4 |
10:36:2.2 |
0:0:26.7 |
----------- |
------------------- |
2 |
a [km] |
24487.54 |
24498.99 |
11.45 |
----------- |
------------------- |
3 |
e |
0.7220892 |
0.7221926 |
0.0001034 |
----------- |
------------------- |
4 |
i |
49 °7 '26 " |
49 °6 '0 " |
0 °1 '26 " |
----------- |
------------------- |
5 |
Hp [km] |
427.22 |
427.86 |
0.65 |
----------- |
------------------- |
6 |
Ha [km] |
35791.59 |
35813.84 |
22.25 |
----------- |
------------------- |
"Echostar-16" target orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 21.11.2012 06:30:06 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
11:14:48.0 |
11:14:57.1 |
0:0:9.1 |
----------- |
------------------- |
2 |
a [km] |
25484.55 |
25488.38 |
3.83 |
----------- |
------------------- |
3 |
e |
0.6543102 |
0.6542441 |
0.0000662 |
----------- |
------------------- |
4 |
i |
29 °28 '17 " |
29 °30 '11 " |
0 °1 '54 " |
----------- |
------------------- |
5 |
Hp [km] |
2431.61 |
2434.62 |
3.01 |
----------- |
------------------- |
6 |
Ha [km] |
35781.22 |
35785.86 |
4.64 |
----------- |
------------------- |
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:
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
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 |