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", "Yamal-401"
Document: 11. Total: 12
Create: 15.12.2014 15:54:41 (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 |
03:15:54.99 |
-5.01 |
Proton-M |
-5.01 |
0.00 |
2 |
SE1 ignition |
03:15:58.24 |
-1.76 |
Proton-M |
-1.77 |
0.01 |
3 |
Lift-off contact |
03:16:00.00 |
0.00 |
Proton-M |
0.00 |
0.00 |
4 |
SE2 ignition |
03:17:55.38 |
115.38 |
Proton-M |
114.98 |
0.40 |
5 |
Stage 1-2 separation |
03:17:59.63 |
119.63 |
Proton-M |
120.82 |
1.19 |
6 |
VE3 ignition |
03:21:23.78 |
323.78 |
Proton-M |
324.54 |
0.76 |
7 |
SE2 burnout |
03:21:26.48 |
326.48 |
Proton-M |
327.25 |
0.77 |
8 |
Stage 2-3 separation |
03:21:27.18 |
327.18 |
Proton-M |
327.98 |
0.80 |
9 |
SE3 ignition |
03:21:29.58 |
329.58 |
Proton-M |
330.40 |
0.82 |
10 |
HF jettison |
03:21:45.05 |
345.05 |
Proton-M |
345.80 |
0.75 |
11 |
Fairing jettison indication |
03:21:46.95 |
346.95 |
Proton-M |
345.90 |
1.05 |
12 |
Preliminary command |
03:25:30.13 |
570.13 |
Proton-M |
570.98 |
0.85 |
13 |
Main command |
03:25:42.06 |
582.06 |
Proton-M |
582.22 |
0.16 |
14 |
OU separation |
03:25:42.22 |
582.22 |
Proton-M |
582.35 |
0.13 |
15 |
US ICE 1- ignition |
03:27:02.22 |
662.22 |
Breeze-M |
662.63 |
0.41 |
16 |
US SE 1- ignition |
03:27:16.22 |
676.22 |
Breeze-M |
676.66 |
0.44 |
17 |
US ICE 1- burnout |
03:27:18.12 |
678.12 |
Breeze-M |
678.56 |
0.44 |
18 |
US SE 1- burnout |
03:31:22.20 |
922.20 |
Breeze-M |
917.70 |
4.50 |
19 |
US ICE 2- ignition |
04:23:08.00 |
4028.00 |
Breeze-M |
4028.04 |
0.04 |
20 |
US SE 2- ignition |
04:23:28.00 |
4048.00 |
Breeze-M |
4048.22 |
0.22 |
21 |
US ICE 2- burnout |
04:23:29.90 |
4049.90 |
Breeze-M |
4050.06 |
0.16 |
22 |
US SE 2- burnout |
04:41:22.75 |
5122.75 |
Breeze-M |
5108.86 |
13.89 |
23 |
US ICE 3- ignition |
06:44:33.00 |
12513.00 |
Breeze-M |
12513.12 |
0.12 |
24 |
US SE 3- ignition |
06:44:57.00 |
12537.00 |
Breeze-M |
12537.23 |
0.23 |
25 |
US ICE 3- burnout |
06:44:58.90 |
12538.90 |
Breeze-M |
12539.07 |
0.17 |
26 |
US SE 3- burnout |
07:02:58.18 |
13618.18 |
Breeze-M |
13607.30 |
10.88 |
27 |
US ICE 4- ignition |
07:04:13.38 |
13693.38 |
Breeze-M |
13682.54 |
10.84 |
28 |
APT separation |
07:04:19.18 |
13699.18 |
Breeze-M |
13688.41 |
10.77 |
29 |
US ICE 4- burnout |
07:04:21.38 |
13701.38 |
Breeze-M |
13690.41 |
10.97 |
30 |
US ICE 5- ignition |
12:02:49.00 |
31609.00 |
Breeze-M |
31609.19 |
0.19 |
31 |
US SE 4- ignition |
12:03:09.00 |
31629.00 |
Breeze-M |
31629.18 |
0.18 |
32 |
US ICE 5- burnout |
12:03:10.90 |
31630.90 |
Breeze-M |
31631.28 |
0.38 |
33 |
US SE 4- burnout |
12:16:13.84 |
32413.84 |
Breeze-M |
32403.29 |
10.55 |
34 |
"Yamal-401" SC separation |
12:17:23.84 |
32483.84 |
Breeze-M |
32472.30 |
11.54 |
35 |
US ICE 6- ignition |
14:26:00.00 |
40200.00 |
Breeze-M |
40200.24 |
0.24 |
36 |
US ICE 6- burnout |
14:26:12.00 |
40212.00 |
Breeze-M |
40212.30 |
0.30 |
37 |
US ICE 7- ignition |
15:31:30.00 |
44130.00 |
No date |
||
38 |
US ICE 7- burnout |
15:33:10.00 |
44230.00 |
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) - 15.12.2014 03:25:42 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:21:44.0 |
1:21:44.2 |
0:0:0.2 |
----------- |
------------------- |
2 |
a [km] |
6238.72 |
6238.85 |
0.13 |
----------- |
------------------- |
3 |
e |
0.0496677 |
0.0496453 |
0.0000223 |
----------- |
------------------- |
4 |
i |
51 °33 '16 " |
51 °33 '14 " |
0 °0 '2 " |
----------- |
------------------- |
5 |
Hp [km] |
-449.27 |
-449.01 |
0.26 |
----------- |
------------------- |
6 |
Ha [km] |
170.45 |
170.45 |
0.00 |
----------- |
------------------- |
Parking orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.12.2014 03:31:32 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:27:55.7 |
1:27:56.8 |
0:0:1.1 |
----------- |
------------------- |
2 |
a [km] |
6550.10 |
6551.00 |
0.90 |
----------- |
------------------- |
3 |
e |
0.0001374 |
0.0000001 |
0.0001373 |
----------- |
------------------- |
4 |
i |
51 °33 '29 " |
51 °33 '29 " |
0 °0 '1 " |
----------- |
------------------- |
5 |
Hp [km] |
171.07 |
172.86 |
1.79 |
----------- |
------------------- |
6 |
Ha [km] |
172.87 |
172.86 |
0.00 |
----------- |
------------------- |
Intermediate orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.12.2014 04:41:32 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:21:49.1 |
2:21:52.1 |
0:0:2.9 |
----------- |
------------------- |
2 |
a [km] |
9008.45 |
9010.50 |
2.05 |
----------- |
------------------- |
3 |
e |
0.2626577 |
0.2627489 |
0.0000912 |
----------- |
------------------- |
4 |
i |
49 °58 '33 " |
49 °54 '0 " |
0 °4 '33 " |
----------- |
------------------- |
5 |
Hp [km] |
264.17 |
264.86 |
0.69 |
----------- |
------------------- |
6 |
Ha [km] |
4996.45 |
4999.86 |
3.41 |
----------- |
------------------- |
Transfer orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.12.2014 07:03:08 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
10:32:4.5 |
10:31:26.9 |
0:0:37.6 |
----------- |
------------------- |
2 |
a [km] |
24397.17 |
24381.03 |
16.14 |
----------- |
------------------- |
3 |
e |
0.7228561 |
0.7227020 |
0.0001541 |
----------- |
------------------- |
4 |
i |
47 °40 '5 " |
47 °36 '11 " |
0 °3 '54 " |
----------- |
------------------- |
5 |
Hp [km] |
383.39 |
382.67 |
0.72 |
----------- |
------------------- |
6 |
Ha [km] |
35654.68 |
35623.11 |
31.57 |
----------- |
------------------- |
"Yamal-401" target orbit.Final orbit parameter estimation per MBC
MDT of orbit.parameters ( day.month.year hour:min:sec) - 15.12.2014 12:16:23 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
23:41:26.8 |
23:49:29.0 |
0:8:2.1 |
----------- |
------------------- |
2 |
a [km] |
41877.49 |
42035.16 |
157.68 |
----------- |
------------------- |
3 |
e |
0.0032353 |
0.0002719 |
0.0029635 |
----------- |
------------------- |
4 |
i |
0 °3 '25 " |
0 °0 '8 " |
0 °3 '17 " |
----------- |
------------------- |
5 |
Hp [km] |
35363.87 |
35645.60 |
281.73 |
----------- |
------------------- |
6 |
Ha [km] |
35634.84 |
35668.46 |
33.62 |
----------- |
------------------- |
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.) |
|
SC separation |
|
SC separation |
|
SC separation |
|
US withdrawel |