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", "TurkSat-4A"
Document: 11. Total: 12
Create: 15.02.2014 12:42:11 (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 |
00:08:57.99 |
-5.01 |
Proton-M |
-5.00 |
0.01 |
2 |
SE1 ignition |
00:09:01.24 |
-1.76 |
Proton-M |
-1.76 |
0.00 |
3 |
Lift-off contact |
00:09:03.00 |
0.00 |
Ball center |
0.02 |
0.02 |
4 |
SE2 ignition |
00:10:58.38 |
115.38 |
Proton-M |
114.90 |
0.48 |
5 |
Stage 1-2 separation |
00:11:02.63 |
119.63 |
Proton-M |
120.30 |
0.67 |
6 |
VE3 ignition |
00:14:26.78 |
323.78 |
Proton-M |
324.38 |
0.60 |
7 |
SE2 burnout |
00:14:29.48 |
326.48 |
Proton-M |
327.10 |
0.62 |
8 |
Stage 2-3 separation |
00:14:30.18 |
327.18 |
Proton-M |
327.82 |
0.64 |
9 |
SE3 ignition |
00:14:32.58 |
329.58 |
Proton-M |
330.25 |
0.67 |
10 |
HF jettison |
00:14:47.98 |
344.98 |
Proton-M |
345.58 |
0.60 |
11 |
Fairing jettison indication |
00:14:49.62 |
346.62 |
Proton-M |
345.68 |
0.94 |
12 |
Preliminary command |
00:18:32.74 |
569.74 |
Proton-M |
570.60 |
0.86 |
13 |
Main command |
00:18:44.70 |
581.70 |
Proton-M |
581.38 |
0.32 |
14 |
OU separation |
00:18:44.86 |
581.86 |
Proton-M |
581.51 |
0.35 |
15 |
US ICE 1- ignition |
00:20:34.86 |
691.86 |
Breeze-M |
692.09 |
0.23 |
16 |
US SE 1- ignition |
00:20:48.86 |
705.86 |
Breeze-M |
705.99 |
0.13 |
17 |
US ICE 1- burnout |
00:20:50.76 |
707.76 |
Breeze-M |
707.82 |
0.06 |
18 |
US SE 1- burnout |
00:25:15.57 |
972.57 |
Breeze-M |
965.77 |
6.80 |
19 |
US ICE 2- ignition |
01:16:16.00 |
4033.00 |
Breeze-M |
4033.12 |
0.12 |
20 |
US SE 2- ignition |
01:16:36.00 |
4053.00 |
Breeze-M |
4053.30 |
0.30 |
21 |
US ICE 2- burnout |
01:16:37.90 |
4054.90 |
Breeze-M |
4055.14 |
0.24 |
22 |
US SE 2- burnout |
01:34:22.04 |
5119.04 |
Breeze-M |
5099.78 |
19.26 |
23 |
US ICE 3- ignition |
03:37:09.00 |
12486.00 |
Breeze-M |
12486.21 |
0.21 |
24 |
US SE 3- ignition |
03:37:33.00 |
12510.00 |
Ball center |
12510.30 |
0.30 |
25 |
US ICE 3- burnout |
03:37:34.90 |
12511.90 |
Breeze-M |
12512.17 |
0.27 |
26 |
US SE 3- burnout |
03:52:11.83 |
13388.83 |
Ball center |
13380.40 |
8.43 |
27 |
US ICE 4- ignition |
03:52:56.02 |
13433.02 |
Breeze-M |
13424.43 |
8.59 |
28 |
APT separation |
03:53:01.83 |
13438.83 |
Ball center |
13430.30 |
8.53 |
29 |
US ICE 4- burnout |
03:53:04.02 |
13441.02 |
Breeze-M |
13432.55 |
8.47 |
30 |
US ICE 5- ignition |
03:54:20.83 |
13517.83 |
Breeze-M |
13518.01 |
0.18 |
31 |
US SE 4- ignition |
03:54:28.83 |
13525.83 |
Ball center |
13526.10 |
0.27 |
32 |
US ICE 5- burnout |
03:54:30.73 |
13527.73 |
Breeze-M |
13528.24 |
0.51 |
33 |
US SE 4- burnout |
03:57:26.74 |
13703.74 |
Ball center |
13700.20 |
3.54 |
34 |
US ICE 6- ignition |
09:00:28.00 |
31885.00 |
Breeze-M |
31885.13 |
0.13 |
35 |
US SE 5- ignition |
09:00:38.00 |
31895.00 |
Breeze-M |
31895.35 |
0.35 |
36 |
US ICE 6- burnout |
09:00:39.90 |
31896.90 |
Breeze-M |
31897.19 |
0.29 |
37 |
US SE 5- burnout |
09:09:46.02 |
32443.02 |
Breeze-M |
32437.73 |
5.29 |
38 |
"TurkSat-4A" SC separation |
09:22:03.00 |
33180.00 |
Breeze-M |
33160.53 |
19.47 |
39 |
US ICE 7- ignition |
11:25:43.00 |
40600.00 |
Breeze-M |
40600.18 |
0.18 |
40 |
US ICE 7- burnout |
11:25:55.00 |
40612.00 |
Breeze-M |
40612.23 |
0.23 |
41 |
US ICE 8- ignition |
12:34:03.00 |
44700.00 |
Breeze-M |
44700.30 |
0.30 |
42 |
US ICE 8- burnout |
12:35:43.00 |
44800.00 |
Breeze-M |
44800.31 |
0.31 |
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) - 15.02.2014 00:18:44 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:21:16.2 |
1:21:16.6 |
0:0:0.4 |
----------- |
------------------- |
2 |
a [km] |
6215.12 |
6215.44 |
0.31 |
----------- |
------------------- |
3 |
e |
0.0538008 |
0.0536432 |
0.0001576 |
----------- |
------------------- |
4 |
i |
51 °34 '11 " |
51 °33 '16 " |
0 °0 '55 " |
----------- |
------------------- |
5 |
Hp [km] |
-497.39 |
-496.12 |
1.27 |
----------- |
------------------- |
6 |
Ha [km] |
171.37 |
170.72 |
0.65 |
----------- |
------------------- |
Parking orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2014 00:25:25 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:27:55.9 |
1:27:56.8 |
0:0:0.9 |
----------- |
------------------- |
2 |
a [km] |
6550.23 |
6551.00 |
0.77 |
----------- |
------------------- |
3 |
e |
0.0001029 |
0.0000001 |
0.0001028 |
----------- |
------------------- |
4 |
i |
51 °34 '28 " |
51 °33 '38 " |
0 °0 '50 " |
----------- |
------------------- |
5 |
Hp [km] |
171.42 |
172.86 |
1.44 |
----------- |
------------------- |
6 |
Ha [km] |
172.77 |
172.86 |
0.09 |
----------- |
------------------- |
Intermediate orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2014 01:34:32 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:21:53.7 |
2:21:55.6 |
0:0:1.9 |
----------- |
------------------- |
2 |
a [km] |
9011.69 |
9013.00 |
1.31 |
----------- |
------------------- |
3 |
e |
0.2623822 |
0.2623984 |
0.0000162 |
----------- |
------------------- |
4 |
i |
50 °22 '29 " |
50 °17 '60 " |
0 °4 '29 " |
----------- |
------------------- |
5 |
Hp [km] |
269.04 |
269.87 |
0.82 |
----------- |
------------------- |
6 |
Ha [km] |
4998.06 |
4999.86 |
1.80 |
----------- |
------------------- |
Transfer orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2014 03:57:36 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
10:35:57.2 |
10:35:41.1 |
0:0:16.1 |
----------- |
------------------- |
2 |
a [km] |
24496.86 |
24489.98 |
6.87 |
----------- |
------------------- |
3 |
e |
0.7223263 |
0.7222129 |
0.0001134 |
----------- |
------------------- |
4 |
i |
49 °10 '35 " |
49 °6 '0 " |
0 °4 '35 " |
----------- |
------------------- |
5 |
Hp [km] |
424.00 |
424.87 |
0.87 |
----------- |
------------------- |
6 |
Ha [km] |
35813.45 |
35798.83 |
14.62 |
----------- |
------------------- |
"TurkSat-4A" target orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.02.2014 09:09:56 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
13:43:49.4 |
13:43:40.6 |
0:0:8.8 |
----------- |
------------------- |
2 |
a [km] |
29110.51 |
29107.03 |
3.47 |
----------- |
------------------- |
3 |
e |
0.4485958 |
0.4485783 |
0.0000175 |
----------- |
------------------- |
4 |
i |
12 °42 '38 " |
12 °41 '60 " |
0 °0 '38 " |
----------- |
------------------- |
5 |
Hp [km] |
9673.52 |
9672.11 |
1.41 |
----------- |
------------------- |
6 |
Ha [km] |
35791.22 |
35785.68 |
5.54 |
----------- |
------------------- |
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:
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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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 |
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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 |