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Information message about launch progress
"Proton-M", "Breeze-M", "MSV-1"
Document: 11. Total: 12
Create: 15.11.2010 08:01:50 (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 |
114.852 |
0.525 |
5 |
Stage 1-2 separation |
00:01:59.627 |
119.627 |
Proton-M |
120.226 |
0.599 |
6 |
VE3 ignition |
00:05:23.781 |
323.781 |
Proton-M |
324.633 |
0.852 |
7 |
SE2 burnout |
00:05:26.481 |
326.481 |
Proton-M |
327.352 |
0.871 |
8 |
Stage 2-3 separation |
00:05:27.181 |
327.181 |
Proton-M |
328.073 |
0.892 |
9 |
SE3 ignition |
00:05:29.581 |
329.581 |
Proton-M |
330.498 |
0.917 |
10 |
HF jettison |
00:05:44.228 |
344.228 |
Proton-M |
345.080 |
0.852 |
11 |
Fairing jettison indication |
00:05:46.129 |
346.129 |
No date |
||
12 |
Preliminary command |
00:09:28.951 |
568.951 |
Proton-M |
570.360 |
1.409 |
13 |
Main command |
00:09:40.879 |
580.879 |
Proton-M |
581.075 |
0.196 |
14 |
OU separation |
00:09:41.043 |
581.043 |
Proton-M |
581.206 |
0.163 |
15 |
US ICE 1- ignition |
00:11:01.043 |
661.043 |
Breeze-M |
661.553 |
0.510 |
16 |
US SE 1- ignition |
00:11:15.043 |
675.043 |
Breeze-M |
675.578 |
0.535 |
17 |
US ICE 1- burnout |
00:11:16.943 |
676.943 |
Breeze-M |
677.478 |
0.535 |
18 |
US SE 1- burnout |
00:18:23.859 |
1103.859 |
Ball center |
1096.908 |
6.951 |
19 |
US ICE 2- ignition |
01:08:01.000 |
4081.000 |
Breeze-M |
4081.418 |
0.418 |
20 |
US SE 2- ignition |
01:08:21.000 |
4101.000 |
Breeze-M |
4101.341 |
0.341 |
21 |
US ICE 2- burnout |
01:08:22.900 |
4102.900 |
Breeze-M |
4103.438 |
0.538 |
22 |
US SE 2- burnout |
01:25:48.818 |
5148.818 |
Breeze-M |
5140.742 |
8.076 |
23 |
US ICE 3- ignition |
03:28:15.000 |
12495.000 |
Breeze-M |
12501.942 |
6.942 |
24 |
US SE 3- ignition |
03:28:39.000 |
12519.000 |
Ball center |
12519.309 |
0.309 |
25 |
US ICE 3- burnout |
03:28:40.900 |
12520.900 |
Breeze-M |
12521.144 |
0.244 |
26 |
US SE 3- burnout |
03:40:56.856 |
13256.856 |
Ball center |
13258.293 |
1.437 |
27 |
US ICE 4- ignition |
03:41:41.056 |
13301.056 |
Breeze-M |
13306.462 |
5.406 |
28 |
APT separation |
03:41:46.856 |
13306.856 |
Breeze-M |
13308.461 |
1.605 |
29 |
US ICE 4- burnout |
03:41:49.056 |
13309.056 |
Breeze-M |
13310.722 |
1.666 |
30 |
US ICE 5- ignition |
03:43:05.856 |
13385.856 |
Breeze-M |
13385.892 |
0.036 |
31 |
US SE 4- ignition |
03:43:13.856 |
13393.856 |
Ball center |
13394.083 |
0.227 |
32 |
US ICE 5- burnout |
03:43:15.756 |
13395.756 |
Breeze-M |
13395.919 |
0.163 |
33 |
US SE 4- burnout |
03:48:05.517 |
13685.517 |
Breeze-M |
13683.229 |
2.288 |
34 |
US ICE 6- ignition |
08:52:46.000 |
31966.000 |
Breeze-M |
31966.134 |
0.134 |
35 |
US SE 5- ignition |
08:53:06.000 |
31986.000 |
Breeze-M |
31986.123 |
0.123 |
36 |
US ICE 6- burnout |
08:53:07.900 |
31987.900 |
Breeze-M |
31988.154 |
0.254 |
37 |
US SE 5- burnout |
09:00:21.278 |
32421.278 |
Breeze-M |
32420.430 |
0.848 |
38 |
"MSV-1" SC separation |
09:14:00.000 |
33240.000 |
Breeze-M |
33240.154 |
0.154 |
39 |
US ICE 7- ignition |
11:23:20.000 |
41000.000 |
No date |
||
40 |
US ICE 7- burnout |
11:23:32.000 |
41012.000 |
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) - 14.11.2010 20:39:01 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:18:11.6 |
1:18:11.0 |
0:0:0.6 |
----------- |
------------------- |
2 |
a [km] |
6057.23 |
6056.69 |
0.54 |
----------- |
------------------- |
3 |
e |
0.0825315 |
0.0825295 |
0.0000020 |
----------- |
------------------- |
4 |
i |
51 °31 '39 " |
51 °31 '16 " |
0 °0 '23 " |
----------- |
------------------- |
5 |
Hp [km] |
-820.82 |
-821.30 |
0.48 |
----------- |
------------------- |
6 |
Ha [km] |
179.00 |
178.41 |
0.59 |
----------- |
------------------- |
Parking orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 14.11.2010 20:47:53 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:28:2.2 |
1:28:1.7 |
0:0:0.6 |
----------- |
------------------- |
2 |
a [km] |
6555.48 |
6555.00 |
0.48 |
----------- |
------------------- |
3 |
e |
0.0000869 |
0.0000001 |
0.0000868 |
----------- |
------------------- |
4 |
i |
51 °32 '16 " |
51 °31 '55 " |
0 °0 '21 " |
----------- |
------------------- |
5 |
Hp [km] |
176.78 |
176.86 |
0.08 |
----------- |
------------------- |
6 |
Ha [km] |
177.92 |
176.86 |
1.05 |
----------- |
------------------- |
Intermediate orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 14.11.2010 21:55:18 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:21:51.8 |
2:21:52.1 |
0:0:0.2 |
----------- |
------------------- |
2 |
a [km] |
9010.34 |
9010.50 |
0.16 |
----------- |
------------------- |
3 |
e |
0.2627769 |
0.2627486 |
0.0000283 |
----------- |
------------------- |
4 |
i |
50 °18 '51 " |
50 °17 '60 " |
0 °0 '51 " |
----------- |
------------------- |
5 |
Hp [km] |
264.49 |
264.87 |
0.37 |
----------- |
------------------- |
6 |
Ha [km] |
4999.91 |
4999.86 |
0.05 |
----------- |
------------------- |
Transfer orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.11.2010 00:17:35 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
10:35:58.6 |
10:35:40.0 |
0:0:18.7 |
----------- |
------------------- |
2 |
a [km] |
24497.46 |
24489.48 |
7.99 |
----------- |
------------------- |
3 |
e |
0.7225880 |
0.7224930 |
0.0000950 |
----------- |
------------------- |
4 |
i |
49 °6 '37 " |
49 °5 '60 " |
0 °0 '37 " |
----------- |
------------------- |
5 |
Hp [km] |
417.75 |
417.87 |
0.11 |
----------- |
------------------- |
6 |
Ha [km] |
35820.90 |
35804.81 |
16.08 |
----------- |
------------------- |
Target orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.11.2010 05:29:51 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
12:28:13.4 |
12:27:45.1 |
0:0:28.3 |
----------- |
------------------- |
2 |
a [km] |
27301.16 |
27289.68 |
11.48 |
----------- |
------------------- |
3 |
e |
0.5450499 |
0.5450532 |
0.0000033 |
----------- |
------------------- |
4 |
i |
18 °57 '43 " |
18 °59 '60 " |
0 °2 '17 " |
----------- |
------------------- |
5 |
Hp [km] |
6042.53 |
6037.22 |
5.31 |
----------- |
------------------- |
6 |
Ha [km] |
35803.53 |
35785.88 |
17.65 |
----------- |
------------------- |
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 |
|
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 |