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", "Astra-2E"
Document: 11. Total: 12
Create: 30.09.2013 13:33:59 (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 |
00:38:04.99 |
-5.01 |
Proton-M |
-5.00 |
0.01 |
2 |
SE1 ignition |
00:38:08.24 |
-1.76 |
Proton-M |
-1.76 |
0.00 |
3 |
Lift-off contact |
00:38:10.00 |
0.00 |
Proton-M |
0.00 |
0.00 |
4 |
SE2 ignition |
00:40:05.38 |
115.38 |
Proton-M |
114.73 |
0.65 |
5 |
Stage 1-2 separation |
00:40:09.63 |
119.63 |
Proton-M |
118.93 |
0.70 |
6 |
VE3 ignition |
00:43:33.78 |
323.78 |
Proton-M |
323.96 |
0.18 |
7 |
SE2 burnout |
00:43:36.48 |
326.48 |
Proton-M |
326.68 |
0.20 |
8 |
Stage 2-3 separation |
00:43:37.18 |
327.18 |
Proton-M |
327.40 |
0.22 |
9 |
SE3 ignition |
00:43:39.58 |
329.58 |
Proton-M |
329.82 |
0.24 |
10 |
HF jettison |
00:43:54.98 |
344.98 |
Proton-M |
345.16 |
0.18 |
11 |
Fairing jettison indication |
00:43:56.88 |
346.88 |
Proton-M |
345.26 |
1.62 |
12 |
Preliminary command |
00:47:40.13 |
570.13 |
Proton-M |
570.86 |
0.73 |
13 |
Main command |
00:47:52.06 |
582.06 |
Proton-M |
582.30 |
0.24 |
14 |
OU separation |
00:47:52.22 |
582.22 |
Proton-M |
582.43 |
0.21 |
15 |
US ICE 1- ignition |
00:49:12.22 |
662.22 |
Breeze-M |
662.80 |
0.58 |
16 |
US SE 1- ignition |
00:49:26.22 |
676.22 |
Breeze-M |
676.95 |
0.73 |
17 |
US ICE 1- burnout |
00:49:28.12 |
678.12 |
Breeze-M |
678.79 |
0.67 |
18 |
US SE 1- burnout |
00:53:56.81 |
946.81 |
Breeze-M |
941.20 |
5.61 |
19 |
US ICE 2- ignition |
01:45:23.00 |
4033.00 |
Breeze-M |
4033.18 |
0.18 |
20 |
US SE 2- ignition |
01:45:43.00 |
4053.00 |
Breeze-M |
4053.37 |
0.37 |
21 |
US ICE 2- burnout |
01:45:44.90 |
4054.90 |
Breeze-M |
4055.20 |
0.30 |
22 |
US SE 2- burnout |
02:03:26.93 |
5116.93 |
Breeze-M |
5096.18 |
20.75 |
23 |
US ICE 3- ignition |
04:05:58.00 |
12468.00 |
Breeze-M |
12468.19 |
0.19 |
24 |
US SE 3- ignition |
04:06:22.00 |
12492.00 |
Breeze-M |
12492.31 |
0.31 |
25 |
US ICE 3- burnout |
04:06:23.90 |
12493.90 |
Breeze-M |
12494.14 |
0.24 |
26 |
US SE 3- burnout |
04:17:51.65 |
13181.65 |
Breeze-M |
13173.10 |
8.55 |
27 |
US ICE 4- ignition |
04:18:35.85 |
13225.85 |
Breeze-M |
13217.40 |
8.45 |
28 |
APT separation |
04:18:41.65 |
13231.65 |
Breeze-M |
13223.26 |
8.39 |
29 |
US ICE 4- burnout |
04:18:43.85 |
13233.85 |
Breeze-M |
13225.52 |
8.33 |
30 |
US ICE 5- ignition |
04:20:00.65 |
13310.65 |
Breeze-M |
13310.72 |
0.07 |
31 |
US SE 4- ignition |
04:20:08.65 |
13318.65 |
Breeze-M |
13318.85 |
0.20 |
32 |
US ICE 5- burnout |
04:20:10.55 |
13320.55 |
Breeze-M |
13320.95 |
0.40 |
33 |
US SE 4- burnout |
04:26:01.48 |
13671.48 |
Ball center |
13664.62 |
6.86 |
34 |
US ICE 6- ignition |
09:31:08.00 |
31978.00 |
Breeze-M |
31978.06 |
0.06 |
35 |
US SE 5- ignition |
09:31:18.00 |
31988.00 |
Breeze-M |
31988.09 |
0.09 |
36 |
US ICE 6- burnout |
09:31:19.90 |
31989.90 |
Breeze-M |
31990.05 |
0.15 |
37 |
US SE 5- burnout |
09:37:33.94 |
32363.94 |
Breeze-M |
32359.68 |
4.26 |
38 |
"Astra-2E" SC separation |
09:50:10.00 |
33120.00 |
Breeze-M |
33120.35 |
0.35 |
39 |
US ICE 7- ignition |
11:54:50.00 |
40600.00 |
Breeze-M |
40600.11 |
0.11 |
40 |
US ICE 7- burnout |
11:55:02.00 |
40612.00 |
Breeze-M |
40612.17 |
0.17 |
41 |
US ICE 8- ignition |
13:14:50.00 |
45400.00 |
Breeze-M |
45400.29 |
0.29 |
42 |
US ICE 8- burnout |
13:16:30.00 |
45500.00 |
Breeze-M |
45500.37 |
0.37 |
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) - 30.09.2013 00:47:52 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:21:16.5 |
1:21:16.8 |
0:0:0.3 |
----------- |
------------------- |
2 |
a [km] |
6215.31 |
6215.57 |
0.27 |
----------- |
------------------- |
3 |
e |
0.0536725 |
0.0535623 |
0.0001102 |
----------- |
------------------- |
4 |
i |
51 °33 '22 " |
51 °32 '52 " |
0 °0 '30 " |
----------- |
------------------- |
5 |
Hp [km] |
-496.42 |
-495.48 |
0.94 |
----------- |
------------------- |
6 |
Ha [km] |
170.76 |
170.36 |
0.40 |
----------- |
------------------- |
Parking orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 30.09.2013 00:54:06 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:27:59.2 |
1:27:59.2 |
0:0:0.1 |
----------- |
------------------- |
2 |
a [km] |
6552.95 |
6553.00 |
0.05 |
----------- |
------------------- |
3 |
e |
0.0000152 |
0.0000001 |
0.0000151 |
----------- |
------------------- |
4 |
i |
51 °33 '40 " |
51 °33 '10 " |
0 °0 '29 " |
----------- |
------------------- |
5 |
Hp [km] |
174.72 |
174.86 |
0.15 |
----------- |
------------------- |
6 |
Ha [km] |
174.92 |
174.86 |
0.05 |
----------- |
------------------- |
Intermediate orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 30.09.2013 02:03:36 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:21:55.5 |
2:21:55.6 |
0:0:0.1 |
----------- |
------------------- |
2 |
a [km] |
9012.92 |
9013.00 |
0.08 |
----------- |
------------------- |
3 |
e |
0.2623905 |
0.2623984 |
0.0000079 |
----------- |
------------------- |
4 |
i |
50 °19 '25 " |
50 °17 '60 " |
0 °1 '25 " |
----------- |
------------------- |
5 |
Hp [km] |
269.88 |
269.87 |
0.01 |
----------- |
------------------- |
6 |
Ha [km] |
4999.68 |
4999.86 |
0.17 |
----------- |
------------------- |
Transfer orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 30.09.2013 04:26:11 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
10:35:8.3 |
10:35:3.8 |
0:0:4.5 |
----------- |
------------------- |
2 |
a [km] |
24475.91 |
24473.99 |
1.92 |
----------- |
------------------- |
3 |
e |
0.7216473 |
0.7216227 |
0.0000246 |
----------- |
------------------- |
4 |
i |
49 °6 '18 " |
49 °5 '60 " |
0 °0 '18 " |
----------- |
------------------- |
5 |
Hp [km] |
434.80 |
434.87 |
0.07 |
----------- |
------------------- |
6 |
Ha [km] |
35760.75 |
35756.83 |
3.92 |
----------- |
------------------- |
"Astra-2E" target orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 30.09.2013 09:37:43 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
11:48:21.7 |
11:49:21.1 |
0:0:59.3 |
----------- |
------------------- |
2 |
a [km] |
26322.69 |
26347.19 |
24.50 |
----------- |
------------------- |
3 |
e |
0.5999332 |
0.5984199 |
0.0015134 |
----------- |
------------------- |
4 |
i |
22 °58 '15 " |
22 °59 '53 " |
0 °1 '39 " |
----------- |
------------------- |
5 |
Hp [km] |
4152.70 |
4202.37 |
49.67 |
----------- |
------------------- |
6 |
Ha [km] |
35736.41 |
35735.73 |
0.68 |
----------- |
------------------- |
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 |
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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 |